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CN202828088U - Airtight booster-type hot air floating platform - Google Patents

Airtight booster-type hot air floating platform Download PDF

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Publication number
CN202828088U
CN202828088U CN 201220491299 CN201220491299U CN202828088U CN 202828088 U CN202828088 U CN 202828088U CN 201220491299 CN201220491299 CN 201220491299 CN 201220491299 U CN201220491299 U CN 201220491299U CN 202828088 U CN202828088 U CN 202828088U
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CN
China
Prior art keywords
utricule
booster
control system
hot gas
hollow panel
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.)
Expired - Fee Related
Application number
CN 201220491299
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Chinese (zh)
Inventor
贺应平
薛富利
郭海军
盛光喜
陈勇
祝远程
王冰
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.)
Xiangyang Hongwei Aircraft Co Ltd
Original Assignee
Xiangyang Hongwei Aircraft 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 Xiangyang Hongwei Aircraft Co Ltd filed Critical Xiangyang Hongwei Aircraft Co Ltd
Priority to CN 201220491299 priority Critical patent/CN202828088U/en
Application granted granted Critical
Publication of CN202828088U publication Critical patent/CN202828088U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model provides an airtight booster-type hot air floating platform comprising a lift force system (1), hang ropes (2), a nacelle (3), a mooring rope (4), a positioning disk (5), a hydraulic winch (6), a mooring car (7) and a control system. The lift force system is connected with the nacelle through hang ropes. The upper end of the mooring rope is connected with a meeting point of the lower ends of the hang roles. The lower end of the mooring rope is installed on the positioning disk. The positioning disk and the hydraulic winch are fixed on the mooring car in sequence. The lift force system (1) comprises a capsule body (11), a one-way decompression valve (12), a booster fan (14), a heater (15) and a booster constructional element (16). Compared with the prior art, the airtight booster-type hot air floating platform has the advantages that the capsule body is high in rigidity, strong in anti-wind ability and stable in working, the manufacture cost is low, the operation is easy and the maintenance is simple. Moreover, the airtight booster-type hot air floating platform is safe, reliable and low in accident occurrence rate. When an emergency circumstance such as a natural disaster occurs, the emergency response is quick and the maneuverability is strong.

Description

Airtight pressure charged hot gas floats hollow panel
Technical field
The utility model relates to floating hollow panel field, particularly, relates to the floating hollow panel of a kind of airtight pressure charged hot gas.
Background technology
Dirigible is a kind of aircraft, and the dirigible at initial stage utilizes the lighter-than-air fire gases such as hydrogen as lift-off power, and the seventies in last century, dirigible is used helium instead, and safety is improved greatly.At present, the field that is widely used in various countries of dirigible comprise take photo by plane, advertisement, patrol, military surveillance, exploration, transportation, the disaster relief, communication broadcast etc.Vast in area, with a varied topography, climate difference is large, the country that disaster takes place frequently, and for example Chinese, people extraordinarily pay close attention to for the application of disaster relief aspect.
If can carry communication apparatus at dirigible, become the platform of mooring aloft, just can occur in disaster, the ground communication base station is destroyed, the disaster area is in emergency circumstances in confused situation, the high-altitude that its rising is tethered in about two kms forms air base station, be used for substituting ground because of the base station of disaster damage, just can greatly reduce the loss in disaster area, even can save the thousands of victims of the disaster's life, therefore be significant.
But, use helium to have the manufacturing cost height, operate and control the shortcomings such as complicated and difficult in maintenance as the captive platform of rising power.The applicant in first to file " floating platform for mooring hot airship " (Chinese patent application open CN102092471A), the characteristics of dirigible are combined with the principle of work of captive fire balloon, adopt the mode of utricule internal-combustion device heating to produce lift, solved the problems referred to above.But the disclosed structure of this utility model is perfect not enough.
The utility model content
Technical problem to be solved in the utility model is: further improve the deficiency that captive hot air airship floating platform of the prior art exists, a kind of increase utricule rigidity, raising wind resistance, low cost of manufacture, processing ease, the floating hollow panel of the simple airtight pressure charged hot gas of maintenance are provided.
The first technical scheme of the present utility model is:
A kind of airtight pressure charged hot gas floats hollow panel, it is characterized in that, comprises lift system, hanging rope, gondola, tether cable, positioning disk, hydraulic windlass, anchoring car and control system,
Lift system is connected with gondola by hanging rope, and the upper end of tether cable is connected with the lower end joint of hanging rope, and the lower end of tether cable is installed on the positioning disk, and positioning disk and hydraulic windlass are fixed on the anchoring car successively;
Lift system comprises utricule, unidirectional blowdown valve, booster fan, temperature booster and supercharging member;
Heater cartridge fits over the upper face of supercharging member, is in utricule inside, and booster fan is assemblied in the lower lattice of supercharging member, is in the utricule outside;
Fire proof seal section is arranged between supercharging member and the utricule;
Unidirectional blowdown valve is installed on the lower part wall of utricule.
The second technical scheme of the present utility model is that in the first technical scheme, said tether cable is wrapped on the cylinder of hydraulic windlass via positioning disk.
The 3rd technical scheme of the present utility model is in the first technical scheme, to be equipped with communication base station equipment and generating set in the said gondola.
The 4th technical scheme of the present utility model is, in the first technical scheme, utricule be shaped as stream line pattern, and have the Y shape empennage.
The 5th technical scheme of the present utility model is, in the first technical scheme, said control system comprises ground control system and aerial control system and the communication radio station for the telecommand of sending the ground artificial maneuvering device, reception aerial platform monitor data;
Ground control system comprises manual operation, display equipment;
Aerial control system comprises the monitored control system that the temperature sensor, anemoscope, baroceptor, the GPS orientator that are loaded on the utricule consist of, aerial control system also comprises telecommand, the collection monitoring system information of accepting the ground artificial operating equipment, carries out the A/D conversion, gps data receives, and sends signal that the control heater main valve opens and closes, sends the central controller of control command to booster fan control setup, unidirectional blowdown valve control setup to control circuit for heater.
Preferably, fire proof seal section between supercharging member and the utricule is made of tubular fire proofing and tether, the upper end of tubular fire proofing is connected with utricule in the mode of making, and the lower end utilizes tether to be connected with the supercharging member, forms seal cavity between utricule and supercharging member.
Preferably, the quantity of unidirectional blowdown valve (12), fire proof seal section (13), booster fan (14) and temperature booster (15) is respectively two.
The utility model is the floating hollow panel of airtight pressure charged hot gas that a kind of Operation and Maintenance is simple, operating costs is cheap, safe and reliable, has realized the emergency communication in the major natural disasters situation.Cause in disaster under the emergency state of fixed telecommunication and mobile communication facility destruction, the floating hollow panel of airtight pressure charged hot gas of the present utility model can carry communication base station and rise to the overhead high-altitude about two kms, unimpeded with the signal of keeping in communication, enforcement of the present utility model involves the thousands of disaster area common people's safety, this for the country of frequent natural calamity for example China have earth shaking meaning.In addition, the floating hollow panel of airtight pressure charged hot gas of the present utility model also has the function that surface state is monitored investigation.
Airtight pressure charged hot gas of the present utility model floats hollow panel, and the upper end of its tether cable is connected with the lower end joint of many hanging ropes of fan-shaped distribution, and the other end of tether cable is loaded on the car that movably anchors, but is a kind of device of vehicle-mounted mobile.Need to prove: the floating hollow panel of airtight pressure charged hot gas of the present utility model is not to move with the anchoring car under the state that hangs on high-altitude, the two km left and right sides, but after the task of finishing the work, it is recovered to vehicle-mounted mobile on the anchoring car.In addition, during the aloft work of the floating hollow panel of airtight pressure charged hot gas of the present utility model about two kms, only in the circular scope of setting radius, move, do not fly, utricule made stream line pattern and with empennage, be to facing the wind in order to control its head, to reduce the impact of wind-force.
The utility model compared with prior art has following beneficial effect:
1. the utricule rigidity is high, wind resistance is strong, working stability;
2. low cost of manufacture, processing ease, maintenance are simple;
3. safe and reliable, accident rate is low;
4. when the emergency situations such as generation disaster, emergency response is fast, mobility strong.
Description of drawings
Fig. 1 is the scheme drawing of the floating embodiment of hollow panel of airtight pressure charged hot gas of the present utility model
Fig. 2 is the lift system scheme drawing of the floating embodiment of hollow panel of airtight pressure charged hot gas of the present utility model
Fig. 3 is the control system block diagram of the floating embodiment of hollow panel of airtight pressure charged hot gas of the present utility model
Fig. 4 is the scheme drawing of the fire proof seal section (13) of the floating embodiment of hollow panel of airtight pressure charged hot gas of the present utility model
Fig. 5 is the partial schematic diagram of fire proof seal section (13) connection mode of the floating embodiment of hollow panel of explanation airtight pressure charged hot gas of the present utility model
Among the figure:
The 1-lift system, 2-hanging rope, 3-gondola, 4-tether cable, 5-positioning disk, 6-hydraulic windlass, the 7-car that anchors, 11-utricule, the unidirectional blowdown valve of 12-, 13-fire proof seal section, the 14-booster fan, 15-temperature booster, 16-supercharging member, 131-tubular leakproofing material, 132-tether.
The specific embodiment
Further specify by the following examples the utility model.Fig. 1 is the scheme drawing of the floating hollow panel of airtight pressure charged hot gas of present embodiment; Fig. 2 is the lift system scheme drawing of the floating hollow panel of airtight pressure charged hot gas of present embodiment, and Fig. 3 is the control system block diagram of the floating hollow panel of airtight pressure charged hot gas of present embodiment.
Can be found out that by Fig. 1, Fig. 2 and Fig. 3 the floating hollow panel of the airtight pressure charged hot gas of present embodiment has lift system 1, hanging rope 2, gondola 3, tether cable 4, positioning disk 5, hydraulic windlass 6, anchoring car 7 and control system.
Lift system 1 is connected with gondola 3 by hanging rope 2, and the upper end of tether cable 4 is connected with the lower end joint of hanging rope 2, and the lower end of tether cable 4 is installed on the positioning disk 5, and positioning disk 5 and hydraulic windlass 6 are fixed on the anchoring car 7 successively.
Lift system comprises utricule 11, unidirectional blowdown valve 12, booster fan 14, temperature booster 15 and supercharging member 16.
Temperature booster 5 has two, be assemblied in respectively supercharging member 16 upper face about two places, be in utricule 11 inside, booster fan 14 also has two, is assemblied in respectively in the lower lattice of supercharging member 16, is in utricule 11 outsides.
Between supercharging member 16 and the utricule 11 fire proof seal section 13 is arranged, Fig. 4 is the scheme drawing of the fire proof seal section 13 of present embodiment, as seen from Figure 4, fire proof seal section 13 is made of tubular fire proofing 131 and tether 132, Fig. 5 is the partial schematic diagram of fire proof seal section 13 connection modes of explanation present embodiment, as seen from Figure 5, under assembled state, the upper end of two tubular fire proofings 131 is connected with utricule 11 in the mode of making, the lower end utilizes tether 132 to be connected with supercharging member 16, forms seal cavity between utricule 11 and supercharging member 16.Like this, during 14 pairs of utricule 11 interior pressure blastings of booster fan in being assemblied in supercharging member 16 lower lattice, air can be from not overflowing between supercharging member 16 and the utricule 11, thereby reach the effect of sealing.
Two unidirectional blowdown valves 12 are installed on the lower part wall of utricule 11, can be from utricule 11 inner unidirectional discharge air, booster fan 14 can feed utricule 11 with the cold air pressurization of utricule outside, and the cold air that feeds to utricule 11 inside can be heated to the temperature that needs by temperature booster 5 on the way.
The aperture of the unidirectional blowdown valve 11 of comprehensive adjustment, the impressed power of booster fan 14 and temperature booster add heat, just can change the pressure and temperature of the air in the utricule 11, the rigidity that keeps as required utricule 11 is implemented under the mooring suspended state and improves wind resistance; Perhaps realize rising, decline, the recovery of the floating hollow panel of airtight pressure charged hot gas.
Tether cable 4 is wrapped in by positioning disk 5 on the cylinder of hydraulic windlass 6, makes as required the platform operating altitude of going up to the air, and carries out the recovery of platform after finishing the work.
Be equipped with communication base station equipment and generating set in the gondola 3, promptly substitute the communication base station of ground damage.
Utricule 11 be shaped as stream line pattern, and have the Y shape empennage, adjust in case of necessity utricule 11 heads it facingd the wind, to reduce the impact of air-flow.
Fig. 3 is the block scheme of the control system of present embodiment, as seen from Figure 3, the airtight pressure charged hot gas of present embodiment floats the hollow panel control system, has ground control system 26 and aerial control system 27 and the communication radio station for the telecommand of sending the ground artificial maneuvering device, reception aerial platform monitor data;
Ground control system 26 comprises manual handling, display equipment;
Aerial control system 27 comprises the monitored control system that the temperature sensor, anemoscope, baroceptor, the GPS orientator that are loaded on the utricule 11 consist of, aerial control system 27 also comprises telecommand, the collection monitoring system information of accepting the ground artificial maneuvering device, carries out the A/D conversion, gps data receives, and sends signal that control heater 5 main valves open and close, sends the central controller of control command to booster fan 14 control setups, unidirectional blowdown valve 12 control setups to temperature booster 5 control circuits.
Be noted that protection domain of the present utility model is not subjected to the restriction of present embodiment, protection domain of the present utility model is documented in claims.

Claims (7)

1. an airtight pressure charged hot gas floats hollow panel, it is characterized in that, comprise lift system (1), hanging rope (2), gondola (3), tether cable (4), positioning disk (5), hydraulic windlass (6), anchoring car (7) and control system
Lift system (1) is connected with gondola (3) by hanging rope (2), the upper end of tether cable (4) is connected with the lower end joint of hanging rope (2), the lower end of tether cable (4) is installed on the positioning disk (5), and positioning disk (5) and hydraulic windlass (6) are fixed on the anchoring car (7) successively;
Lift system comprises utricule (11), unidirectional blowdown valve (12), booster fan (14), temperature booster (15) and supercharging member (16);
Temperature booster (5) is assemblied in the upper face of supercharging member (16), is in utricule (11) inside, and booster fan (14) is assemblied in the lower lattice of supercharging member (16), is in utricule (11) outside;
Between supercharging member (16) and the utricule (11) fire proof seal section (13) is arranged;
Unidirectional blowdown valve (12) is installed on the lower part wall of utricule (11).
2. the floating hollow panel of airtight pressure charged hot gas according to claim 1 is characterized in that said tether cable (4) is wrapped on the cylinder of hydraulic windlass (6) via positioning disk (5).
3. the floating hollow panel of airtight pressure charged hot gas according to claim 1 is characterized in that said gondola is equipped with communication base station equipment and generating set in (3).
4. the floating hollow panel of airtight pressure charged hot gas according to claim 1 is characterized in that, utricule (11) be shaped as stream line pattern, and have the Y shape empennage.
5. airtight pressure charged hot gas according to claim 1 floats hollow panel, it is characterized in that said control system comprises ground control system (26) and aerial control system (27) and the communication radio station for the telecommand of sending the ground artificial maneuvering device, reception aerial platform monitor data;
Ground control system (26) comprises manual operation, display equipment;
Aerial control system (27) comprises the temperature sensor that is loaded on the utricule (11), anemoscope, baroceptor, the monitored control system that the GPS orientator consists of, aerial control system (27) also comprises the telecommand of accepting the ground artificial operating equipment, collection monitoring system information, carry out the A/D conversion, gps data receives, and sends the signal that control heater (15) main valve opens and closes to temperature booster (5) control circuit, to booster fan (14) control setup, unidirectional blowdown valve (12) control setup sends the central controller of control command.
6. each described airtight pressure charged hot gas floats hollow panel according to claim 1~5, it is characterized in that, fire proof seal section (13) between said supercharging member (16) and the utricule (11) is made of tubular fire proofing (131) and tether (132), the upper end of tubular fire proofing (131) is connected with utricule (11) in the mode of making, the lower end utilizes tether (132) to be connected with supercharging member (16), forms seal cavity between utricule (11) and supercharging member (16).
7. each described airtight pressure charged hot gas floats hollow panel according to claim 1~5, it is characterized in that the quantity of said unidirectional blowdown valve (12), fire proof seal section (13), booster fan (14) and temperature booster (15) is respectively two.
CN 201220491299 2012-09-25 2012-09-25 Airtight booster-type hot air floating platform Expired - Fee Related CN202828088U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220491299 CN202828088U (en) 2012-09-25 2012-09-25 Airtight booster-type hot air floating platform

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220491299 CN202828088U (en) 2012-09-25 2012-09-25 Airtight booster-type hot air floating platform

Publications (1)

Publication Number Publication Date
CN202828088U true CN202828088U (en) 2013-03-27

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220491299 Expired - Fee Related CN202828088U (en) 2012-09-25 2012-09-25 Airtight booster-type hot air floating platform

Country Status (1)

Country Link
CN (1) CN202828088U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102874402A (en) * 2012-09-25 2013-01-16 襄阳宏伟航空器有限责任公司 Airtight pressure-charged hot-gas floating platform
CN106428506A (en) * 2016-11-02 2017-02-22 上海钧希新能源科技有限公司 Hot-air balloon based on methanol fuel battery
CN107433046A (en) * 2017-09-28 2017-12-05 中国特种飞行器研究所 Travel aircraft and floating type is ridden aircraft
CN110228579A (en) * 2018-03-05 2019-09-13 东莞前沿技术研究院 Floating transport device

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102874402A (en) * 2012-09-25 2013-01-16 襄阳宏伟航空器有限责任公司 Airtight pressure-charged hot-gas floating platform
CN102874402B (en) * 2012-09-25 2015-06-03 襄阳宏伟航空器有限责任公司 Airtight pressure-charged hot-gas floating platform
CN106428506A (en) * 2016-11-02 2017-02-22 上海钧希新能源科技有限公司 Hot-air balloon based on methanol fuel battery
CN107433046A (en) * 2017-09-28 2017-12-05 中国特种飞行器研究所 Travel aircraft and floating type is ridden aircraft
CN110228579A (en) * 2018-03-05 2019-09-13 东莞前沿技术研究院 Floating transport device

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Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130327

Termination date: 20190925

CF01 Termination of patent right due to non-payment of annual fee