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CN107972857A - A kind of five rotor crafts - Google Patents

A kind of five rotor crafts Download PDF

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Publication number
CN107972857A
CN107972857A CN201711256638.1A CN201711256638A CN107972857A CN 107972857 A CN107972857 A CN 107972857A CN 201711256638 A CN201711256638 A CN 201711256638A CN 107972857 A CN107972857 A CN 107972857A
Authority
CN
China
Prior art keywords
rotor
fuselage
jack
motor
post
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
CN201711256638.1A
Other languages
Chinese (zh)
Inventor
王志成
王鹏飞
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.)
Foshan Shenfeng Aviation Technology Co Ltd
Original Assignee
Foshan Shenfeng Aviation 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 Foshan Shenfeng Aviation Technology Co Ltd filed Critical Foshan Shenfeng Aviation Technology Co Ltd
Priority to CN201711256638.1A priority Critical patent/CN107972857A/en
Publication of CN107972857A publication Critical patent/CN107972857A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • B64D47/08Arrangements of cameras

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)

Abstract

A kind of five rotor crafts, belong to vehicle technology field, more particularly to a kind of five rotor crafts, including video camera, remote controler, fuselage, rack, jack-post, big rotor, supporting rod, motor, ring protection shell, small rotor and support wheel.It is furnished with control system and airborne equipment in fuselage.Video camera is embedded in fore-body and energy 360 rotates freely exploration.Big rotor fin is symmetrical and is mutually 15 degree of angles of attack.Small rotor fin is symmetrical and is mutually 15 degree of angles of attack.Supporting bar structure formed objects are equally symmetrically distributed in fuselage both sides.Motor is separately fixed on respective supporting rod.Small rotor is placed on motor.Interior smooth recessed structure can place small rotor wing tip wherein ring protection shell marginal center in a ring.Big rotor agree with jack-post can on jack-post opening and closing.Jack-post can on fuselage free vertical telescopic.Support wheel it is scalable go out rack.Five rotor craft of one kind of the present invention, safety and stability is full-featured, can carry out operation with land in the air, save production cost.

Description

A kind of five rotor crafts
Technical field
A kind of five rotor crafts, belong to vehicle technology field, more particularly to a kind of five rotor crafts.
Background technology
Aircraft has come into the sight of people gradually with advances in technology, thus be widely used in exploration, agricultural, People need the place of operation in the air in military, postal delivery, rescue and relief work and daily life, but traditional aircraft can only Working at height is carried out, but is difficult to save oneself and aircraft is recycled, stability and safety in the event of unexpected run out of steam Property it is poor moreover, and unmanned plane can only working at height once occur emergency need land work can not realize at all.
The content of the invention
The purpose of the present invention is overcoming the above-mentioned deficiency of traditional aircraft, it is simple to invent a kind of structure of convenient control Five higher rotor crafts of efficiency.
A kind of five rotor crafts, including video camera, remote controler, fuselage, rack, jack-post, big rotor, supporting rod, motor, Ring protection shell, small rotor and support wheel.
It is furnished with control system and airborne equipment in the fuselage.The video camera is embedded in fore-body and can 360 ° of freedom Rotation exploration.The big rotor fin is symmetrical and is mutually 15 degree of angles of attack.The small rotor fin is symmetrical and is mutually 15 degree and meets Angle.The supporting bar structure formed objects are equally symmetrically distributed in fuselage both sides.The motor is separately fixed at each self-supporting On bar.The small rotor is placed on motor.Interior smooth recessed structure can be by small rotation in a ring for the ring protection shell marginal center Cautiously point is placed wherein.The big rotor agree with jack-post can on jack-post opening and closing.The jack-post can be on fuselage certainly By vertical telescopic.The support wheel it is scalable go out rack.
The working method of five rotor craft is:It can be moved to during five rotor craft standby for takeoff by support wheel Solution space, is gone up to the air operation by the small rotor of remote control control electric motor starting afterwards, go up to the air operation when video camera be actuated for entirely The prospecting in orientation carries out relevant work, causes five rotors to fly if running into harsh climate and burst factor in operation process The small rotor of row device is damaged, and jack-post will be stretched out out of fuselage at this time, and the big rotor agreed with it, which will open, carries out spiraling, together When small rotor stop rotating, reach specify ground after five rotor crafts land, and be moved to safety area.When need not be into Also operation can be carried out during row aerial work on ground.
Five rotor craft of one kind of the present invention, safety and stability is full-featured, can carry out operation, section with land in the air About production cost.
Brief description of the drawings
Fig. 1 is the schematic perspective view of five rotor crafts;Fig. 2 is the schematic side view of five rotor crafts;Fig. 3 is five rotations The schematic top plan view of rotor aircraft.
In figure, 1- video cameras, 2- remote controlers, 3- fuselages, 4- racks, 5- jack-posts, the big rotors of 6-, 7- supporting rods, 8- motors, 9- ring protection shells, the small rotors of 10-, 11- support wheels.
Embodiment
The present invention is illustrated in conjunction with attached drawing, a kind of five rotor crafts, including video camera 1, remote controler 2, Fuselage 3, rack 4, jack-post 5, big rotor 6, supporting rod 7, motor 8, ring protection shell 9, small rotor 10 and support wheel 11.
It is furnished with control system and airborne equipment in the fuselage 3.The video camera 1 be embedded in fuselage 3 it is anterior and can 360 from Surveyed by rotation.6 fin of big rotor is symmetrical and is mutually 15 degree of angles of attack.10 fin of small rotor is symmetrical and is mutually 15 Spend the angle of attack.The 7 structure formed objects of supporting rod are equally symmetrically distributed in 3 both sides of fuselage.The motor 8 is separately fixed at respectively On self-supporting bar 7.The small rotor 10 is placed on motor 8.9 marginal center of ring protection shell interior smooth recessed knot in a ring Structure can place small 10 wing tip of rotor wherein.The big rotor 6 agree with jack-post 5 can on jack-post 5 opening and closing.The axis Column 5 can on fuselage 3 free vertical telescopic.The support wheel 11 it is scalable go out rack 4.
The working method of five rotor craft is:It can be moved during five rotor craft standby for takeoff by support wheel 11 To solution space, control motor 8 to start small rotor 10 by remote controler 2 afterwards and go up to the air operation, go up to the air operation when video camera 1 start Carry out comprehensive prospecting and carry out relevant work, if harsh climate and burst factor are run into operation process causes five The small rotor 10 of rotor craft is impaired, and jack-post 5 will be stretched out out of fuselage 3 at this time, and the big rotor 6 agreed with it, which will open, to carry out Spiraling, while small rotor 10 stops rotating, five rotor crafts land after specified ground is reached, and are moved to safely Band.Also operation can be carried out when aerial work need not be carried out on ground.
Five rotor craft of one kind of the present invention, safety and stability is full-featured, can carry out operation, section with land in the air About production cost.

Claims (5)

  1. A kind of 1. five rotor crafts, it is characterised in that:Including video camera(1), remote controler(2), fuselage(3), rack(4), axis Column(5), big rotor(6), supporting rod(7), motor(8), ring protection shell(9), small rotor(10)And support wheel(11);The machine Body(3)It is interior to be furnished with control system and airborne equipment;The video camera(1)It is embedded in fuselage(3)Anterior and 360 ° of energy rotates freely Exploration;The big rotor(6)Fin is symmetrical and is mutually 15 ° of angles of attack;The small rotor(10)Fin is symmetrical and is mutually 15 degree The angle of attack;The supporting rod(7)Structure formed objects are equally symmetrically distributed in fuselage(3)Both sides;The motor(8)Fix respectively In respective supporting rod(7)On;The small rotor(10)It is placed on motor(8)On;The ring protection shell(9)Marginal center is in ring Smooth recessed structure can be by small rotor in shape(10)Wing tip is placed wherein;The big rotor(6)Agree with jack-post(5)On can be in jack-post (5)Upper opening and closing;The jack-post(5)Can be in fuselage(3)Upper free vertical telescopic;The support wheel(7)It is scalable go out rack (4).
  2. A kind of 2. five rotor craft according to claim 1, it is characterised in that:Its working method is:Five rotors fly It can pass through support wheel during row device standby for takeoff(11)Solution space is moved to, passes through remote controler afterwards(2)Control motor(8)Start Small rotor(10)Go up to the air operation, go up to the air operation when video camera(1)It is actuated for comprehensive prospecting and carries out relevant work, if Harsh climate and burst factor are run into operation process causes the small rotor of five rotor crafts(10)It is damaged, at this time jack-post (5)Will be from fuselage(3)Interior stretching, agrees with big rotor on it(6)It will open and carry out spiraling, while small rotor(10)Stop Spin-ended turn, five rotor crafts land after specified ground is reached, and are moved to safety area.
  3. 3. also operation can be carried out on ground when aerial work need not be carried out.
  4. A kind of 4. five rotor craft according to claim 1 or 2, it is characterised in that:There is big motor in airborne equipment(8) Drive jack-post(5)Rotation is so as to drive big rotor(6)Rotation.
  5. A kind of 5. five rotor craft according to claim 1 or 2, it is characterised in that:The aircraft can lean on greatly in the air Motor(8)Drive big rotor(6)And motor(8)Drive small rotor(10)Operation, on land secure support wheel(11)Operation.
CN201711256638.1A 2017-12-03 2017-12-03 A kind of five rotor crafts Pending CN107972857A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711256638.1A CN107972857A (en) 2017-12-03 2017-12-03 A kind of five rotor crafts

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711256638.1A CN107972857A (en) 2017-12-03 2017-12-03 A kind of five rotor crafts

Publications (1)

Publication Number Publication Date
CN107972857A true CN107972857A (en) 2018-05-01

Family

ID=62009012

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711256638.1A Pending CN107972857A (en) 2017-12-03 2017-12-03 A kind of five rotor crafts

Country Status (1)

Country Link
CN (1) CN107972857A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112078784A (en) * 2020-09-30 2020-12-15 福州大学 Omnidirectional five-rotor aircraft and control method
CN114889378A (en) * 2022-06-01 2022-08-12 佛山市神风航空科技有限公司 Air-ground dual-purpose aerocar

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150102175A1 (en) * 2012-11-15 2015-04-16 Aviron Consulting Developmentand Manufacture For Advanced Aviation Fixed winged aircraft with foldable auto-rotation rotor
CN105366046A (en) * 2015-12-15 2016-03-02 江苏艾锐泰克无人飞行器科技有限公司 Fixed-wing air vehicle and control method in vertical posture
CN205891232U (en) * 2016-07-08 2017-01-18 上海工程技术大学 Urgent safe launching appliance of four rotor unmanned aerial vehicle

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150102175A1 (en) * 2012-11-15 2015-04-16 Aviron Consulting Developmentand Manufacture For Advanced Aviation Fixed winged aircraft with foldable auto-rotation rotor
CN105366046A (en) * 2015-12-15 2016-03-02 江苏艾锐泰克无人飞行器科技有限公司 Fixed-wing air vehicle and control method in vertical posture
CN205891232U (en) * 2016-07-08 2017-01-18 上海工程技术大学 Urgent safe launching appliance of four rotor unmanned aerial vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112078784A (en) * 2020-09-30 2020-12-15 福州大学 Omnidirectional five-rotor aircraft and control method
CN114889378A (en) * 2022-06-01 2022-08-12 佛山市神风航空科技有限公司 Air-ground dual-purpose aerocar

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Legal Events

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PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20180501

RJ01 Rejection of invention patent application after publication