Nothing Special   »   [go: up one dir, main page]

CN110043412A - A kind of energy recycle device for being mounted on airbome pulse formula fog machine - Google Patents

A kind of energy recycle device for being mounted on airbome pulse formula fog machine Download PDF

Info

Publication number
CN110043412A
CN110043412A CN201910363913.2A CN201910363913A CN110043412A CN 110043412 A CN110043412 A CN 110043412A CN 201910363913 A CN201910363913 A CN 201910363913A CN 110043412 A CN110043412 A CN 110043412A
Authority
CN
China
Prior art keywords
impeller
airbome
fog machine
pulse formula
mounting rack
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201910363913.2A
Other languages
Chinese (zh)
Inventor
姜涛
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zheng Yunlin
Original Assignee
Chengdu Huimei Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Chengdu Huimei Technology Co Ltd filed Critical Chengdu Huimei Technology Co Ltd
Priority to CN201910363913.2A priority Critical patent/CN110043412A/en
Publication of CN110043412A publication Critical patent/CN110043412A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B1/00Engines of impulse type, i.e. turbines with jets of high-velocity liquid impinging on blades or like rotors, e.g. Pelton wheels; Parts or details peculiar thereto
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B3/00Machines or engines of reaction type; Parts or details peculiar thereto
    • F03B3/12Blades; Blade-carrying rotors
    • F03B3/121Blades, their form or construction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B3/00Machines or engines of reaction type; Parts or details peculiar thereto
    • F03B3/12Blades; Blade-carrying rotors
    • F03B3/126Rotors for essentially axial flow, e.g. for propeller turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B3/00Machines or engines of reaction type; Parts or details peculiar thereto
    • F03B3/16Stators
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The present invention relates to field of generating equipment, disclose a kind of energy recycle device for being mounted on airbome pulse formula fog machine.The energy recycle device includes mounting rack, impeller, gear drive and generator, wherein the mounting rack is used to be fixed on the nozzle of airbome pulse formula fog machine;The impeller, the gear drive and the generator are separately mounted on the mounting rack, wherein, the impeller can be located at the inlet zone of the airbome pulse formula fog machine by the mounting rack, and the impeller shaft of the impeller is sequentially connected the armature spindle of the generator by the gear drive.It is possible thereby to utilize the composite structure of impeller, gear drive and generator, the part ejecta kinetic energy discharged through gasoline combustion is captured in the nozzle of existing airbome pulse formula fog machine, and capture kinetic energy recycling is converted into electric energy, and then the power consumption of aircraft can be compensated, conducive to the continuation of the journey path for extending aircraft.

Description

A kind of energy recycle device for being mounted on airbome pulse formula fog machine
Technical field
The invention belongs to field of generating equipment, and in particular to a kind of energy for being mounted on airbome pulse formula fog machine Recyclable device.
Background technique
Pulsejet type fogger is a kind of novel application, fertilising and Pesticidal and sterilizing manufactured and designed based on pulse jet principle The farm machine of equal applications, due to none rotatable parts of full machine, there is no mechanical wears in any case, can be durable, There are fabulous penetrability and diffusivity, adhesion is good, and anti-rain drop erosion is strong, smoke-like can be made in drug and fertilizer, had It is easy to operate, drug dose is greatly reduced, work efficiency is high, and brake worm sterilizes, and is conducive to the outstanding features such as environmental protection.
The ejecta of existing pulsejet type fogger initial velocity all with higher, to realize that large area sprays purpose.But When pulsejet type fogger by carry on the aircraft such as unmanned plane in use, since its spout mean level is arranged backwards, Belong to high-altitude sprinkling and aircraft inherently have the characteristics that it is removable, be able to achieve large area sprinkling purpose, ejecta at this time Without compared with high initial speed, but the ejecta initial velocity of existing pulsejet type fogger can not flexible modulation, so for ejecta Kinetic energy will cause certain waste.
Summary of the invention
In order to solve the problems, such as that the ejecta kinetic energy of existing airbome pulse formula fog machine has certain waste, the object of the invention It is to provide a kind of energy recycle device for being mounted on airbome pulse formula fog machine, the progress of ejecta kinetic energy can be recycled Power generation, conducive to the cruising ability for promoting unmanned plane.
The technical scheme adopted by the invention is as follows:
A kind of energy recycle device for being mounted on airbome pulse formula fog machine, including mounting rack, impeller, gear pass Motivation structure and generator, wherein the mounting rack is used to be fixed on the nozzle of airbome pulse formula fog machine;
The impeller, the gear drive and the generator are separately mounted on the mounting rack, wherein described Impeller can be located at the inlet zone of the airbome pulse formula fog machine by the mounting rack, and the impeller shaft of the impeller passes through described Gear drive is sequentially connected the armature spindle of the generator.
Optimization, the mounting rack includes impeller support plate and motor mounting plate, wherein the number of the impeller support plate It is vertically arranged in the injection direction two sides of the airbome pulse formula fog machine for two pieces and respectively;
The first end of the impeller support plate is used to be fixed on the nozzle of the airbome pulse formula fog machine, the leaf The both ends of wheel shaft are respectively perpendicular the second end that ground activity passes through respective side impeller support plate, so that the radial blade of the impeller It can be rotated between two impeller support plates;
The motor mounting plate vertically connects the first end of a wherein impeller support plate, the generator sheet of the generator Body is mounted on the motor mounting plate.
Optimization, further include the smog extension being obliquely installed, wherein the first end of the smog extension is for connecting Lead to the spout of the airbome pulse formula fog machine;
The shortest distance of radial blade of the second end of the smog extension to the impeller between 5~10cm it Between.
It advanced optimizes, when the mounting rack includes two impeller support plates, the smog extension is located at two leaves It takes turns between support plate;
The mounting rack further includes several floors, and the floor is between two impeller support plates and vertical connection impeller branch Fagging, the second end of the smog extension is after being secured across all floors towards the radial blade.
Optimize in detail, the mounting rack further includes the hurricane globe having for surrounding the impeller, wherein the smog prolongs The second end for stretching pipe is inserted into the hurricane globe, and offers outlet in the bottom of the hurricane globe 106.
It advanced optimizes, the tilt angle of the smog extension is between 35~40 degree.
It advanced optimizes, the mounting rack further includes having several otic placodes, wherein the otic placode vertically connects the impeller Support plate;
Vertically activity passes through the otic placode at the middle part of the armature spindle.
It advanced optimizes, several through-holes is provided on the motor mounting plate;And/or the radial direction of the radial blade is hung down Straightforward face is in the arc structure towards emission direction evagination, and the crooked radian of the arc structure is between 0.12~0.24rad.
Optimization, the gear drive includes first bevel gear and the second bevel gear with vertical-transmission relationship, Wherein, first angular wheel shaft connects the impeller shaft, and second angular wheel shaft connects the armature spindle;
The gear ratio of first bevel gear and second bevel gear is less than 1.
Optimization, further include having AC/DC converter and super capacitor, wherein the super capacitor is airborne for being electrically connected Receiving end or on-board batteries;
The electric energy output end of the generator, the AC/DC converter and the super capacitor are sequentially connected electrically.
The invention has the benefit that
(1) the invention provides one kind can carry out recycling power generation to the ejecta kinetic energy of airbome pulse formula fog machine Novel energy recyclable device, it can using the composite structure of impeller, gear drive and generator, in existing airbome pulse The nozzle of formula fog machine captures the part ejecta kinetic energy discharged through gasoline combustion, and capture kinetic energy recycling is converted to electricity Can, and then the power consumption of aircraft can be compensated, conducive to the continuation of the journey path for extending aircraft;
(2) spray can also be changed although ejecta can be made to slow down since impeller can also generate inhibition to ejecta Direction out diffuses away ejecta downward, and ejecta is prevented to be attached to the abdomen of aircraft, avoids the occurrence of material waste and asks Topic;
(3) energy recycle device has the characteristics that installation is firm, does not influence flight, structure is simple and is easily achieved, Convenient for practical application and popularization.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this Some embodiments of invention for those of ordinary skill in the art without creative efforts, can be with It obtains other drawings based on these drawings.
Fig. 1 is the three-dimensional assembling structure schematic diagram of airbome pulse formula fog machine and energy recycle device provided by the invention.
Fig. 2 is the section view assembling structure schematic diagram of airbome pulse formula fog machine and energy recycle device provided by the invention.
Fig. 3 is the circuit system structure schematic diagram of energy recycle device provided by the invention.
Fig. 4 is the structural schematic diagram of the radial vertical cross-section of radial blade provided by the invention.
In above-mentioned attached drawing: 1- mounting rack;101- impeller support plate;102- motor mounting plate;103- floor;104- otic placode; 105- through-hole;106- hurricane globe;The outlet 107-;2- impeller;201- impeller shaft;202- radial blade;3- gear drive; The first bevel gear of 301-;The second bevel gear of 302-;4- generator;401- armature spindle;402- engine block;5- smog extends Pipe;20- airbome pulse formula fog machine.
Specific embodiment
With reference to the accompanying drawing and specific embodiment come the present invention is further elaborated.It should be noted that for Although the explanation of these way of example is to be used to help understand the present invention, but and do not constitute a limitation of the invention.It is public herein The specific structure and function detail opened are only used for description example embodiments of the present invention.However, can with many alternative forms come The present invention is embodied, and is not construed as limiting the invention in embodiment set forth herein.
It will be appreciated that though various units may be described herein using term first, second etc., but these units It should not be limited by these terms.These terms are only used to distinguish a unit and another unit.Such as it can be by Unit one is referred to as second unit, and similarly second unit can be referred to as first unit, shows without departing from of the invention The range of example embodiment.
It should be appreciated that being only a kind of pass for describing affiliated partner to the term "and/or" being likely to occur in this article Connection relationship indicates may exist three kinds of relationships, for example, A and/or B, can indicate: individualism A, individualism B are deposited simultaneously In tri- kinds of situations of A and B;To the term "/and " being likely to occur in this article, it is to describe another affiliated partner relationship, indicates There may be two kinds of relationships, for example, A/ and B, can indicate: two kinds of situations of individualism A, individualism A and B;In addition, for The character "/" being likely to occur herein, typicallying represent forward-backward correlation object is a kind of "or" relationship.
If should be appreciated that, it can when unit being referred to as with another unit " connection ", " connected " or " coupling " herein To be directly connected with another unit or couple or temporary location may exist.Relatively, if herein by unit be referred to as with When another unit " being connected directly " or " direct-coupling ", indicate that temporary location is not present.Additionally, it should solve in a similar manner Release for describing the relationship between unit other words (for example, " ... between " to " between directly existing ... ", " adjacent " To " direct neighbor " etc.).
It should be appreciated that terms used herein are only used for description specific embodiment, it is not intended to limit example of the invention Embodiment.If used herein, singular "a", "an" and "the" is intended to include plural form, unless context Contrary is explicitly indicated.If being also understood that, term " includes ", " including ", "comprising" and/or " containing " are herein When being used, specify stated feature, integer, step, operation, unit and/or component existence, and be not excluded for one Or other multiple features, quantity, step, operation, unit, component and/or their combination existence or increase.
It should be appreciated that it will be further noted that the function action occurred may go out with attached drawing in some alternative embodiments Existing sequence is different.Such as related function action is depended on, it can actually substantially be executed concurrently, or sometimes Two figures continuously shown can be executed in reverse order.
It should be appreciated that providing specific details, in the following description in order to which example embodiment is understood completely. However those of ordinary skill in the art are it is to be understood that implementation example embodiment without these specific details. Such as system can be shown in block diagrams, to avoid with unnecessary details come so that example is unclear.In other instances, may be used Or not show well-known process, structure and technology unnecessary details, to avoid making example embodiment unclear.
Embodiment one
As shown in figures 1-4, the energy regenerating for being mounted on airbome pulse formula fog machine provided in this embodiment Device, including mounting rack 1, impeller 2, gear drive 3 and generator 4, wherein the mounting rack 1 is airborne for being fixed on The nozzle of pulsejet type fogger 20;The impeller 2, the gear drive 3 and the generator 4 are separately mounted to described On mounting rack 1, wherein the impeller 2 can be located at the inlet zone of the airbome pulse formula fog machine 20 by the mounting rack 1, The impeller shaft 201 of the impeller 2 is sequentially connected the armature spindle 401 of the generator 4 by the gear drive 3.
As shown in Fig. 1~2, in the specific structure of the energy recycle device, the airbome pulse formula fog machine 20 is used It on having the aircraft such as man-machine or unmanned plane, to reach various agriculture application purposes, such as applies fertilizer or spills in by carry Pesticide;The airbome pulse formula fog machine 20 can directly apply existing pulsejet type fogger, and (it mainly uses gasoline combustion Mode drives work);Since the quality of aircraft is much larger than the quality of carry fog machine, and the ejecta kinetic energy of fog machine spout It is again limited, therefore ejecta can be ignored the repulsion of entire aircraft.The mounting rack 1 is for carrying the leaf Wheel 2, the gear drive 3 and the generator 4, and them is made to may be mounted at the spray of the airbome pulse formula fog machine 20 At mouthful;In addition, in order to mitigate flight burden, the mounting rack 1 is preferably made of aluminum alloy material or light aircraft aluminium material.
The impeller 2 can be located at the spray of the airbome pulse formula fog machine 20 by then passing through the design of the mounting rack 1 Penetrate area, therefore when the airbome pulse formula fog machine 20 ejects smog, can capture ejecta kinetic energy (it can be appreciated that Shock wave kinetic energy) and rotate the impeller shaft 201;The impeller 2 can be, but not limited to using as shown in Figure 1 by impeller shaft 201 and several radial blades 202 being equally spaced around 201 circumferential direction of impeller shaft composed by structure, can so mention It is exported for maximized torsion;Further for maximum speed and peak torque is guaranteed, weight can be installed additional in the impeller shaft 201 Power flywheel, so that revolving speed be made to be getting faster;In addition, the impeller 2 is it is also preferred that using aluminum alloy material in order to mitigate flight burden Or light aircraft aluminium material is made.
The gear drive 3 for realizing from the impeller shaft 201 to the rotary drive of the armature spindle 401, into And realize that kinetic energy transmits, and enables the generator 4 that the kinetic energy of capture is converted to electric energy.As shown in Figure 1, specifically, described Gear drive 3 can be, but not limited to include first bevel gear 301 and the second bevel gear 302 with vertical-transmission relationship, Wherein, impeller shaft 201 described in 301 axis connection of the first bevel gear, armature spindle described in 402 axis connection of the second bevel gear 401;The gear ratio of first bevel gear 301 and second bevel gear 302 is less than 1.In aforesaid gears transmission mechanism 3 Specific structure in,, can be revolving speed so that the gear drive 3 is to drive up mechanism since gear ratio is less than 1 Promote most fast state, it is ensured that the efficiency that kinetic energy converts electric energy maximizes.In addition, in order to mitigate flight burden, the gear is passed Motivation structure 3 of aluminum alloy material or light aircraft aluminium material it is also preferred that be made.
The generator 4 is converted to electric energy for realizing kinetic energy, can use the knot similar with existing wind-driven generator Structure realizes power generation purpose.During practical flight, the spout direction mean level of the airbome pulse formula fog machine 20 is backwards Setting, so that the airbome pulse formula fog machine 20 and the impeller 2 are front and back setting, the airbome pulse formula fog machine of front 20 can play the role of effectively keeping out the wind to subsequent impeller 2, therefore the impeller 2 only will receive ejecta kinetic energy and turn It is dynamic, it realizes the purpose for driving the generator 4 to generate electricity, moving ahead for aircraft will not be hindered because of the design of the impeller 2 (it is contemplated herein that ejecta to whole aircraft it is counter push away acceleration can be carried out with impeller by the repulsion of ejecta it is most of Ground is cancelled out each other, they influence the flight of aircraft negligible).In addition, as shown in Figure 1, the generator 4 it is also preferred that The front of the impeller 2 is set, certain keep out the wind can also be played the role of to the subsequent impeller 2.
From there through the specific design of preceding energy recyclable device, impeller, gear drive and generator can use Composite structure, it is dynamic in the part ejecta that is discharged through gasoline combustion of nozzle capture of existing airbome pulse formula fog machine Can, and capture kinetic energy recycling is converted into electric energy, and then the power consumption of aircraft can be compensated, conducive to the continuous of aircraft is extended Bit path.The essence of the invention is that the part of gasoline of airbome pulse formula fog machine releases energy recycling is transferred to aircraft Use, found by test, the airbome pulse formula fog machine for being 4000W for operating power, if install additional quality between 1~ The preceding energy recyclable device (quality is negligible to the increase of flight burden for entire aircraft) of 2Kg, Power generation output power can be made to reach 1100W, it can 27% or so gasoline releases energy and supplies aircraft use, not Perpetua mobilia scheme with practicability.In addition, since the impeller 2 can also generate inhibition to ejecta, although can make to spray Object slows down out, but can also change emission direction, diffuses away ejecta downward, ejecta is prevented to be attached to the abdomen of aircraft Portion avoids the occurrence of material waste problem.
Optimization, the mounting rack 1 includes impeller support plate 101 and motor mounting plate 102, wherein the impeller support The number of plate 101 is two pieces and is vertically arranged in the injection direction two sides of the airbome pulse formula fog machine 20 respectively;The leaf The first end of wheel support plate 101 is used to be fixed on the nozzle of the airbome pulse formula fog machine 20, the impeller shaft 201 Both ends are respectively perpendicular ground activity and pass through (activity herein passes through mode and can be, but not limited to using bearing arrangement) respective side impeller The second end of support plate 101, so that the radial blade 202 of the impeller 2 can rotate between two impeller support plates 101;Institute State the first end that motor mounting plate 102 vertically connects a wherein impeller support plate 101, the engine block of the generator 4 402 are mounted on the motor mounting plate 102.As shown in Figure 1, not only may insure by the way that the impeller support plate 101 is arranged The impeller 2 can be located at the inlet zone of the airbome pulse formula fog machine 20, the effect of keeping out the wind can also be further functioned as, to keep away Exempt from outer gas stream and interference is generated to the rotation of the impeller 2.In addition, in order to further mitigate the burden of the mounting rack 1, it is described Several through-holes 105 are provided on motor mounting plate 102;And driven to most preferably be ejected object air-flow, make kinetic energy capture rate It maximizes, from aerodynamic angle and referring to the structure of existing waterwheel impeller, by the radial direction of the radial blade 202 Vertical cross-section decision design is in the arc structure towards emission direction evagination, and the crooked radian of the arc structure is preferably between 0.12 Between~0.24rad.As shown in figure 4, the radial direction vertical cross-section refers to and radial perpendicular section, crooked radian θ citing For 0.18rad.
It advanced optimizes, further includes the smog extension 5 being obliquely installed, wherein the first end of the smog extension 5 Portion is used to be connected to the spout of the airbome pulse formula fog machine 20;The second end of the smog extension 5 is to the impeller 2 The shortest distance of radial blade 202 is between 5~10cm.As illustrated in fig. 1 and 2, consider that region to be sprayed is located at aircraft Underface, and the injection direction of existing airbome pulse formula fog machine be it is horizontal backwards, needing spout to transfer after 90 degree could be to Lower sprinkling, but jet impact wave in this way can be lost when through 90 degree of bends, while not allow that there are larger in exhaust duct Obstruction because may cause flame-out.Therefore on the one hand to the smog extension 5 using being obliquely installed, impact can be ensured Wave does not have too many loss when through turnover bend, is especially preferably between 35 in the tilt angle of the smog extension 5 Between~40 degree when (as shown in Fig. 2, tilt angle is exemplified as θ=36 °);On the other hand due to the of the smog extension 5 Two ends to the impeller 2 radial blade 202 the shortest distance between 5~10cm (as shown in Fig. 2, the shortest distance lift Example is D=7cm), it can not only make full use of the maximum impulse force of ejecta shock wave, but also can be to avoid allowing cigarette because reason is stopped There is flame-out risk in mist machine.
It advanced optimizes, the smog extension 5 is between two impeller support plates 101;The mounting rack 1 further includes Several floors 103, the floor 103 is between two impeller support plates 101 and vertical connection impeller support plate 101, the cigarette The second end of mist extension 5 is after being secured across all floors 103 towards the radial blade 202.As illustrated in fig. 1 and 2, The floor 103 consolidates the smog extension 5 for reinforcing the mounting rack 1, prevents from occurring because of frequent impulse wave The loosening of connected relation.Optimizing in detail, the mounting rack 1 further includes the hurricane globe 106 having for surrounding the impeller 2, In, the second end of the smog extension 5 is inserted into the hurricane globe 106, and is offered in the bottom of the hurricane globe 106 Outlet 107.As illustrated in fig. 1 and 2, the hurricane globe 106 can be fixedly mounted in the impeller support plate 101 of two sides, for complete Outer gas stream is avoided to generate interference to the rotation of the impeller 2;In addition, can make to change ejection side by the way that the outlet 107 is arranged To ejecta normally spray downward.In addition, for the ease of observing the internal structure of the hurricane globe 106, the hurricane globe 106 are preferably made of transparent and high temperature resistant material.
It advanced optimizes, the mounting rack 1 further includes having several otic placodes 104, wherein the vertically connection of otic placode 104 The impeller support plate 101;Vertically activity passes through the otic placode 104 at the middle part of the armature spindle 401.As shown in Figure 1, passing through The otic placode 104 is set, the middle part of the armature spindle 401 can be supported, consolidates the installation relation of the generator 4.In addition, this The activity at place passes through mode and equally can be, but not limited to using bearing arrangement.
Optimization, further include having AC/DC converter and super capacitor, wherein the super capacitor is airborne for being electrically connected Receiving end or on-board batteries;The electric energy output end of the generator 4, the AC/DC converter and the super capacitor are successively electric Connection.As shown in figure 3, since super capacitor is in circuit not counting acting loads, so the electric energy that generator 4 issues can be first Super capacitor is supplied, the airborne receiving end (power end of i.e. airborne power-consuming component) or on-board batteries of unmanned plane are then resupplied, The access and disconnection of such circuit load do not interfere with the revolving speed of generator, realize and steadily carry out power compensation purpose.
To sum up, using provided by the present embodiment for the energy recycle device that is mounted on airbome pulse formula fog machine, It has the following technical effect that
(1) the new of recycling power generation can be carried out to the ejecta kinetic energy of airbome pulse formula fog machine by present embodiments providing one kind Type energy recycle device, it can using the composite structure of impeller, gear drive and generator, in existing airbome pulse formula The nozzle of fog machine captures the part ejecta kinetic energy discharged through gasoline combustion, and capture kinetic energy recycling is converted to electricity Can, and then the power consumption of aircraft can be compensated, conducive to the continuation of the journey path for extending aircraft;
(2) spray can also be changed although ejecta can be made to slow down since impeller can also generate inhibition to ejecta Direction out diffuses away ejecta downward, and ejecta is prevented to be attached to the abdomen of aircraft, avoids the occurrence of material waste and asks Topic;
(3) energy recycle device has the characteristics that installation is firm, does not influence flight, structure is simple and is easily achieved, Convenient for practical application and popularization.
Multiple embodiments described above are only schematical, if being related to unit as illustrated by the separation member, It may or may not be physically separated;If being related to component shown as a unit, can be or It can not be physical unit, it can it is in one place, or may be distributed over multiple network units.It can be according to reality Some or all of the units may be selected to achieve the purpose of the solution of this embodiment for the needs on border.Those of ordinary skill in the art Without paying creative labor, it can understand and implement.
The above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations;Although with reference to the foregoing embodiments Invention is explained in detail, those skilled in the art should understand that: it still can be to aforementioned each implementation Technical solution documented by example is modified or equivalent replacement of some of the technical features.And these modification or Replacement, the spirit and scope for technical solution of various embodiments of the present invention that it does not separate the essence of the corresponding technical solution.
Finally it should be noted that the present invention is not limited to above-mentioned optional embodiment, anyone is in enlightenment of the invention Under can all obtain other various forms of products.Above-mentioned specific embodiment should not be understood the limit of pairs of protection scope of the present invention System, protection scope of the present invention should be subject to be defined in claims, and specification can be used for explaining that right is wanted Seek book.

Claims (10)

1. a kind of energy recycle device for being mounted on airbome pulse formula fog machine, it is characterised in that: including mounting rack (1), impeller (2), gear drive (3) and generator (4), wherein the mounting rack (1) is for being fixed on airbome pulse formula The nozzle of fog machine (20);
The impeller (2), the gear drive (3) and the generator (4) are separately mounted on the mounting rack (1), Wherein, the impeller (2) can be located at the inlet zone of the airbome pulse formula fog machine (20) by the mounting rack (1), described The armature spindle that the impeller shaft (201) of impeller (2) passes through the gear drive (3) transmission connection generator (4) (401)。
2. a kind of energy recycle device for being mounted on airbome pulse formula fog machine as described in claim 1, feature Be: the mounting rack (1) includes impeller support plate (101) and motor mounting plate (102), wherein the impeller support plate (101) number is two pieces and is vertically arranged in the injection direction two sides of the airbome pulse formula fog machine (20) respectively;
The first end of the impeller support plate (101) is used to be fixed on the nozzle of the airbome pulse formula fog machine (20), The both ends of the impeller shaft (201) are respectively perpendicular the second end that ground activity passes through respective side impeller support plate (101), so that institute The radial blade (202) for stating impeller (2) can rotate between two impeller support plates (101);
The motor mounting plate (102) vertically connects the first end of a wherein impeller support plate (101), the generator (4) Engine block (402) be mounted on the motor mounting plate (102).
3. a kind of energy recycle device for being mounted on airbome pulse formula fog machine as claimed in claim 1 or 2, special Sign is: further including the smog extension (5) being obliquely installed, wherein the first end of the smog extension (5) is for being connected to The spout of the airbome pulse formula fog machine (20);
The second end of the smog extension (5) to the impeller (2) radial blade (202) the shortest distance between 5~ Between 10cm.
4. a kind of energy recycle device for being mounted on airbome pulse formula fog machine as claimed in claim 3, feature Be: when the mounting rack (1) includes two impeller support plate (101), the smog extension (5) is located at the support of two impellers Between plate (101);
The mounting rack (1) further includes several floors (103), the floor (103) between two impeller support plates (101) and Vertical connection impeller support plate (101), the second end of the smog extension (5) are being secured across all floors (103) Afterwards towards the radial blade (202).
5. a kind of energy recycle device for being mounted on airbome pulse formula fog machine as claimed in claim 4, feature Be: the mounting rack (1) further includes the hurricane globe (106) having for surrounding the impeller (2), wherein the smog extends The second end for managing (5) is inserted into the hurricane globe (106), and offers outlet (107) in the bottom of the hurricane globe 106.
6. a kind of energy recycle device for being mounted on airbome pulse formula fog machine as claimed in claim 3, feature Be: the tilt angle of the smog extension (5) is between 35~40 degree.
7. a kind of energy recycle device for being mounted on airbome pulse formula fog machine as claimed in claim 2, feature Be: the mounting rack (1) further includes having several otic placodes (104), wherein the otic placode (104) vertically connects the impeller branch Fagging (101);
Vertically activity passes through the otic placode (104) at the middle part of the armature spindle (401).
8. a kind of energy recycle device for being mounted on airbome pulse formula fog machine as claimed in claim 2, feature It is: is provided with several through-holes (105) on the motor mounting plate (102);
And/or the radial vertical cross-section of the radial blade (202) is in the arc structure towards emission direction evagination, the arcuation knot The crooked radian of structure is between 0.12~0.24rad.
9. a kind of energy recycle device for being mounted on airbome pulse formula fog machine as claimed in claim 1 or 2, special Sign is: the gear drive (3) includes first bevel gear (301) and the second bevel gear with vertical-transmission relationship (302), wherein impeller shaft (201) described in the first bevel gear (301) axis connection, the second bevel gear (402) axis connection The armature spindle (401);
The gear ratio of first bevel gear (301) and second bevel gear (302) is less than 1.
10. a kind of energy recycle device for being mounted on airbome pulse formula fog machine as described in claim 1, feature It is: further includes having AC/DC converter and super capacitor, wherein the super capacitor is for being electrically connected airborne receiving end or machine Carry battery;
Electric energy output end, the AC/DC converter and the super capacitor of the generator (4) are sequentially connected electrically.
CN201910363913.2A 2019-04-30 2019-04-30 A kind of energy recycle device for being mounted on airbome pulse formula fog machine Pending CN110043412A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910363913.2A CN110043412A (en) 2019-04-30 2019-04-30 A kind of energy recycle device for being mounted on airbome pulse formula fog machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910363913.2A CN110043412A (en) 2019-04-30 2019-04-30 A kind of energy recycle device for being mounted on airbome pulse formula fog machine

Publications (1)

Publication Number Publication Date
CN110043412A true CN110043412A (en) 2019-07-23

Family

ID=67280664

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910363913.2A Pending CN110043412A (en) 2019-04-30 2019-04-30 A kind of energy recycle device for being mounted on airbome pulse formula fog machine

Country Status (1)

Country Link
CN (1) CN110043412A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112907882A (en) * 2021-03-05 2021-06-04 苏康平 Electrical fire early warning system and operation method thereof

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2232084Y (en) * 1994-12-20 1996-07-31 李红江 Counter-force external combustion jet engine
CN2321954Y (en) * 1998-01-24 1999-06-02 陈俊山 Simple type electricity generator
JP2006052718A (en) * 2004-08-13 2006-02-23 Cel:Kk Impulse-turbine complex motor
US20120080882A1 (en) * 2010-10-04 2012-04-05 Kenneth Tyrone Newburn Electric generator utilizing high pressure fluid spray to rotate power generating
CN102418594A (en) * 2011-08-12 2012-04-18 北京理工大学 Pre-vortex water spray waste gas energy recovery system and control method
CN102834183A (en) * 2010-03-31 2012-12-19 杜尔系统有限责任公司 Axial turbine for a rotary atomizer
CN104747351A (en) * 2013-12-28 2015-07-01 哈尔滨工大金涛科技股份有限公司 Steam power device
CN108617620A (en) * 2017-11-24 2018-10-09 吴李海 A kind of pulsed spraying machine
CN209761608U (en) * 2019-04-30 2019-12-10 成都德慧美科技有限公司 Energy recovery device for being mounted on airborne pulse smoke machine

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2232084Y (en) * 1994-12-20 1996-07-31 李红江 Counter-force external combustion jet engine
CN2321954Y (en) * 1998-01-24 1999-06-02 陈俊山 Simple type electricity generator
JP2006052718A (en) * 2004-08-13 2006-02-23 Cel:Kk Impulse-turbine complex motor
CN102834183A (en) * 2010-03-31 2012-12-19 杜尔系统有限责任公司 Axial turbine for a rotary atomizer
US20120080882A1 (en) * 2010-10-04 2012-04-05 Kenneth Tyrone Newburn Electric generator utilizing high pressure fluid spray to rotate power generating
CN102418594A (en) * 2011-08-12 2012-04-18 北京理工大学 Pre-vortex water spray waste gas energy recovery system and control method
CN104747351A (en) * 2013-12-28 2015-07-01 哈尔滨工大金涛科技股份有限公司 Steam power device
CN108617620A (en) * 2017-11-24 2018-10-09 吴李海 A kind of pulsed spraying machine
CN209761608U (en) * 2019-04-30 2019-12-10 成都德慧美科技有限公司 Energy recovery device for being mounted on airborne pulse smoke machine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112907882A (en) * 2021-03-05 2021-06-04 苏康平 Electrical fire early warning system and operation method thereof

Similar Documents

Publication Publication Date Title
CN100359161C (en) Anti-icing system for wind turbines
WO2012075566A1 (en) Turbine assembly, and kit with components for assembling the same
AU2009301600A1 (en) Wind powered apparatus having counter rotating blades
CN107905941B (en) A kind of horizontal-shaft wind turbine and its application method
CN209680365U (en) A kind of rotary air-assisted sprayer unit
CN110043412A (en) A kind of energy recycle device for being mounted on airbome pulse formula fog machine
CN207242047U (en) A kind of new unmanned plane using wireless remote control technology for agricultural seeder
CN106224181A (en) A kind of wind-driven generator
CN104912740A (en) Barrel type wind power generator with multiple impeller units
CN209581876U (en) It can VTOL fixed-wing fog machine
CN114070129B (en) Rotary-driven composite energy capture device
JP2010209786A (en) On-vehicle wind turbine generator
CN201433856Y (en) Combined wind driven generator
CN102269121A (en) Vertical-axis wind driven rotating power generation system
CN209761608U (en) Energy recovery device for being mounted on airborne pulse smoke machine
CN101994653B (en) Round through vertical shaft pneumatic wind power generator set
WO2019105517A1 (en) Wind turbine blade
CN201723380U (en) Automobile-used wind power generation device
KR102152359B1 (en) Wind power air cleaner
CN116745518A (en) Wind power generation device capable of being mounted on mobile body
CN106499574A (en) The small-sized solar power generation windmill of wind light mutual complementing
US20140175801A1 (en) Wind turbine power generator
RU49584U1 (en) ROTARY WIND ENGINE
CN201835983U (en) Multi-layered sail for wind power generation
CN112167214A (en) Portable multi-point vortex air-assisted high-clearance boom sprayer

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
TA01 Transfer of patent application right

Effective date of registration: 20231031

Address after: No. 34, Group 5, Longquan, Ganxi Town, Pujiang County, Chengdu City, Sichuan Province, 611600

Applicant after: Zheng Yunlin

Address before: 3 / F, block B, area a, building 6, 200 Tianfu 5th Street, hi tech Zone, Chengdu, Sichuan 610000

Applicant before: CHENGDU DEHUIMEI TECHNOLOGY CO.,LTD.

TA01 Transfer of patent application right