CN112758327A - Novel manned unmanned aerial vehicle - Google Patents
Novel manned unmanned aerial vehicle Download PDFInfo
- Publication number
- CN112758327A CN112758327A CN202110279027.9A CN202110279027A CN112758327A CN 112758327 A CN112758327 A CN 112758327A CN 202110279027 A CN202110279027 A CN 202110279027A CN 112758327 A CN112758327 A CN 112758327A
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- Prior art keywords
- unmanned aerial
- aerial vehicle
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- machine body
- spraying device
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- 238000005507 spraying Methods 0.000 claims abstract description 29
- 230000001681 protective effect Effects 0.000 claims abstract description 14
- 230000003139 buffering effect Effects 0.000 claims abstract description 9
- 238000013016 damping Methods 0.000 claims description 24
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 7
- 239000004917 carbon fiber Substances 0.000 claims description 7
- 239000002131 composite material Substances 0.000 claims description 7
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 7
- 230000035939 shock Effects 0.000 claims description 4
- 239000011521 glass Substances 0.000 claims description 3
- 238000010521 absorption reaction Methods 0.000 claims 3
- 230000000694 effects Effects 0.000 description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 239000006096 absorbing agent Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 description 1
- 238000004146 energy storage Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 230000000638 stimulation Effects 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
- B64C1/063—Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0647—Seats characterised by special upholstery or cushioning features
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention discloses a novel manned unmanned aerial vehicle which comprises a machine body, a pump spraying device, a cabin, a rotor, a motor and a stator, wherein the pump spraying device is arranged on the periphery of the machine body, the cabin is arranged above the machine body, the bottom of the pump spraying device is connected with a foldable rod frame, one end, far away from the pump spraying device, of the foldable rod frame is connected with the machine body, the stator and the rotor are arranged inside the pump spraying device, an outer protective shell is arranged outside the stator and the rotor, the motor is hermetically arranged inside the machine body, a buffering moving device is arranged at the bottom of the machine body, a foldable foot rest is connected to the bottom of the buffering moving device, and a connecting bottom wheel is arranged below the foldable foot rest. This novel manned unmanned aerial vehicle, collapsible rack and pump spout the device and be connected to make this unmanned aerial vehicle's power device can fold, realize practicing thrift the purpose of interior space through folding collapsible rack when not using, also improved this unmanned aerial vehicle's practicality.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a novel manned unmanned aerial vehicle.
Background
With the continuous progress of science and technology, the living standard of people is also continuously improved, so people have higher pursuit for the quality of leisure life, and the film is taken as a part of the leisure life of people, so that people can better understand the development of society and bring visual enjoyment to people, so people have higher pursuit for the image quality and the shooting effect of the film, however, aerial photographing lenses appear in commercial films at higher and higher frequency, sometimes the aerial photographing lenses are intensively inserted in the most important war, pursuit and fighting scenes in the film in a fierce dazzling mode, the wonderful aerial photographing lenses can bring extraordinary visual stimulation to audiences, and in the aerial photographing process of the film, the use of an unmanned aerial vehicle is indispensable;
manned machine aerial photography always is the final branch that will in the aerial photography, however the cost ratio of this kind of mode of taking photo by plane is higher, the noise of aircraft is also very big when taking some splendid fragments simultaneously, the quality of shooing has been influenced, it is supplementary each other with the unmanned aerial vehicle cooperation in the function also to have man-machine now, but such shooting is with high costs, the controllability is low, the danger coefficient is high, and current manned machine type is big, area is big, thereby reduced the availability factor to unmanned aerial vehicle, the shooting quality and effect have also been reduced.
We therefore propose a novel manned drone in order to solve the problems set out above.
Disclosure of Invention
The invention aims to provide a novel manned unmanned aerial vehicle, which aims to solve the problems that the cost of the existing aerial photography mode in the market proposed by the background technology is higher, the noise of an airplane is very high when some wonderful segments are photographed, the photographing quality is influenced, and the manned unmanned aerial vehicle and the unmanned aerial vehicle are matched and supplemented with each other in function, but the photographing cost is high, the controllability is low, the danger coefficient is high, the existing manned unmanned aerial vehicle is large in size and large in occupied area, so that the use efficiency of the unmanned aerial vehicle is reduced, and the photographing quality and effect are also reduced.
In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides a novel manned unmanned aerial vehicle, spouts device, cabin, rotor, motor and stator including organism, pump, be provided with the pump all around of organism and spout the device, and the top of organism is provided with the cabin, the bottom and the collapsible rod frame that the device was spouted to the pump are connected, and collapsible rod frame keeps away from the one end that the device was spouted to the pump and the organism is connected, the inside that the device was spouted to the pump is provided with stator and rotor, and the externally mounted of stator and rotor has outer protective housing, motor seal installs in the inside of organism, the buffering mobile device is installed to the bottom of organism, and the bottom of buffering mobile device is connected with collapsible foot rest to the below of collapsible foot rest is equipped with the connection return pulley, collapsible foot rest and control system are connected, the inside in cabin is provided with built-in seat, and damping.
Preferably, the machine body is made of carbon fiber composite materials and is of a cylindrical structure, and a hemispherical aviation organic glass window is arranged on the machine body.
Preferably, the pump spraying device is fixedly installed on a shaft of the motor, the motor is connected with a power supply through an electric wire in sealing connection with the carbon-fiber composite main machine body, the number of the pump spraying devices is 4, and meanwhile, the motor is a waterproof motor.
Preferably, the outer protective shell is in a circular truncated cone shape, a gap exists between the outer protective shell and the stator, and the stators are distributed at equal angles.
Preferably, the stator does not rotate in the flying state of the machine body, and the direction of the stator is upward.
Preferably, the damping device is composed of a damping spring and a damping pad, and the damping device is arranged below the built-in seat.
Preferably, the foldable foot rest is made of carbon fiber composite materials, 4 foldable foot rests are arranged, and the foldable foot rest and the connecting bottom wheel are connected through a shaft.
Preferably, the control system is composed of a control terminal, a lighting device, a GPS, a Beidou positioning device and a cabin environment control system.
Compared with the prior art, the invention has the beneficial effects that: the novel manned unmanned aerial vehicle is provided with a vehicle body,
(1) the unmanned aerial vehicle is provided with 4 pump spraying devices which are connected with the foldable rod frame, so that the power device of the unmanned aerial vehicle adopts a pump spraying type structure, the flying speed of the unmanned aerial vehicle can be improved, the maneuverability of the unmanned aerial vehicle is also improved, meanwhile, the flying noise of the unmanned aerial vehicle is small during aerial photography, and the aerial photography quality and the working efficiency are improved;
(2) the foldable rod frame is connected with the pump spraying device, so that the power device of the unmanned aerial vehicle can be folded, the purpose of saving indoor space is realized by folding the foldable rod frame when the unmanned aerial vehicle is not used, and the practicability of the unmanned aerial vehicle is also improved;
(3) the unmanned aerial vehicle has better controllability and maneuverability due to the structural property, can flexibly reach a shooting lens for shooting, has high safety performance, can ensure the safety of personnel in the unmanned aerial vehicle, and improves the safety performance of the unmanned aerial vehicle when in use;
(4) the unmanned aerial vehicle is provided with a control system, and the control system consists of a control terminal, a lighting device, a GPS (global positioning system), a Beidou positioning device and a cabin environment control system, so that when an operator drives the unmanned aerial vehicle, the direction can be accurately controlled, and the environment condition can be accurately mastered, so that the operator can better carry out aerial photography work, the aerial photography effect is ensured, and the use efficiency of the unmanned aerial vehicle is ensured;
(5) be provided with damping device, and damping device installs in the below of built-in seat to damping device comprises damping spring and damping pad, and operating personnel can effectively slow down the vibrations dynamics like this when driving this unmanned aerial vehicle, lets operating personnel more comfortable, and then lets the better operation of taking photo by plane of operating personnel, has also improved this unmanned aerial vehicle's practicality.
Drawings
FIG. 1 is a schematic overall front view of the present invention;
FIG. 2 is a front view of the shock absorber of the present invention;
FIG. 3 is a schematic top view of the inboard seat of the present invention;
FIG. 4 is a schematic bottom view of the buffer moving device of the present invention;
FIG. 5 is a schematic view of the pump-spraying apparatus of the present invention;
FIG. 6 is a schematic top view of the motor and rotor connection of the present invention;
fig. 7 is a schematic top view of the motor and stator connection of the present invention.
In the figure: 1. a body; 2. a pump spray device; 3. a nacelle; 4. a collapsible pole stand; 5. a rotor; 6. a motor; 7. an outer protective shell; 8. a stator; 9. a buffer moving device; 10. connecting a bottom wheel; 11. a damping device; 12. a built-in seat; 13. a foldable foot rest; 14. and (5) controlling the system.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-7, the present invention provides a technical solution: a novel manned unmanned aerial vehicle comprises a machine body 1, a pump spraying device 2, a machine room 3, a foldable rod frame 4, a rotor 5, a motor 6, an outer protective shell 7, a stator 8, a buffering moving device 9, a connecting bottom wheel 10, a damping device 11, a machine seat 12, a foldable foot stool 13 and a control system 14, wherein the pump spraying device 2 is arranged around the machine body 1, the machine room 3 is arranged above the machine body 1, the bottom of the pump spraying device 2 is connected with the foldable rod frame 4, one end, far away from the pump spraying device 2, of the foldable rod frame 4 is connected with the machine body 1, the stator 8 and the rotor 5 are arranged inside the pump spraying device 2, the outer protective shell 7 is arranged outside the stator 8 and the rotor 5, the motor 6 is hermetically arranged inside the machine body 1, the buffering moving device 9 is arranged at the bottom of the machine body 1, and the bottom of the buffering moving device 9 is connected, and a connecting bottom wheel 10 is arranged below the foldable foot rest 13, the foldable foot rest 13 is connected with a control system 14, an internal seat 12 is arranged inside the engine room 3, and a damping device 11 is arranged below the internal seat 12.
Organism 1 constitutes for carbon borer dimension combined material, and organism 1 is cylindrical structure to be provided with hemispherical aviation organic glass window on the organism 1, can make organism 1 firmer when using like this, thereby can reduce and damage the probability, improve organism 1's live time, guarantee operating personnel's normal driving simultaneously.
2 fixed mounting of device are spouted to the pump is epaxial at motor 6, and motor 6 is connected with the power through the electric wire with 1 sealing connection of carbon borer dimension combined material host computer body, and the pump spouts device 2 to be provided with 4, motor 6 is waterproof motor simultaneously, can guarantee motor 6's normal use like this, effectively prevent the phenomenon that motor 6 from weing from appearing, thereby guarantee this unmanned aerial vehicle power device's normal use, wherein the setting of pump spout device 2, not only can improve this unmanned aerial vehicle's flight speed, can also improve this unmanned aerial vehicle's mobility, increase the flexibility in the use, provide the advantage for the work of taking photo by plane.
Outer protective housing 7 is the round platform shape, and has the interval between outer protective housing 7 and the stator 8 to angular distribution such as stator 8 through outer protective housing 7, can effectively protect stator 8, reduces the impaired probability of stator 8, and when stator 8 was rotatory, the normal rotation that does not influence stator 8 simultaneously.
Collapsible foot rest 13 is carbon borer dimension combined material, and collapsible foot rest 13 is provided with 4 to collapsible foot rest 13 with connect for the hub connection between the return pulley 10, like this when this unmanned aerial vehicle contacts with ground, can slide on ground through connecting return pulley 10, when not using, be convenient for fold collapsible foot rest 13 and accomodate, reduce occupation space, further improved this unmanned aerial vehicle's flexibility.
The working principle of the embodiment is as follows: when the novel manned unmanned aerial vehicle is used, as shown in fig. 1-7, firstly, a worker checks the performance of the unmanned aerial vehicle, after safety is ensured, the unmanned aerial vehicle can sit in the cabin 3, then the motor 6 is started, and the pump spraying device 2 is driven to operate when the motor 6 is started, and the pump spraying device 2 is internally provided with the stator 8 and the rotor 5, wherein the stator 8 and the rotor 5 are externally provided with the outer protective shell 7, so that the stator 8 and the rotor 5 can be effectively protected, and the pump spraying device 2 operates along with the operation of the pump spraying device 2 and serves as a power structure of the unmanned aerial vehicle, and the stator 8 does not rotate in the flying state of the unmanned aerial vehicle and is upward in direction, so that noise can be greatly reduced during flying, the flying speed can be effectively improved, and the maneuverability of the unmanned aerial vehicle is also improved;
the pump-spraying device 2 can change the power direction during flying or navigating through the foldable rod frame 4 or rotate, and realize the purpose of controlling the driving direction, thereby enabling operators to better carry out the aerial photography work and ensuring the normal operation of the aerial photography work, because the buffer moving device 9 is positioned at the bottom of the machine body 1, and the bottom of the buffer moving device 9 is provided with a foldable foot rest 13 made of 4 carbon fiber composite materials, and a connecting bottom wheel 10 is arranged below the foldable foot rest 13, the unmanned aerial vehicle can slide on the ground, the use performance of the unmanned aerial vehicle is further improved, meanwhile, the foldable foot rest 13 is convenient to fold and store when not in use, further the occupied space can be effectively reduced, the flexibility of the unmanned aerial vehicle is increased, because the control system 14 comprises a control terminal, a lighting device, a GPS, a Beidou positioning device and a cabin environment control system, so control direction of flight that can be accurate, also can carry out better control to this unmanned aerial vehicle, accuracy when guaranteeing the flight, the bottom of seat 12 is provided with damping device 11 in the aircraft simultaneously, and damping device 11 comprises damping spring and damping pad, therefore operating personnel can let operating personnel more comfortable when the flight, play the absorbing effect, above just be the working process of whole device, the content of not making detailed description in this description all belongs to the prior art that technical personnel publicly know in the field.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that various changes in the embodiments and/or modifications of the invention can be made, and equivalents and modifications of some features of the invention can be made without departing from the spirit and scope of the invention.
Claims (8)
1. The utility model provides a novel manned unmanned aerial vehicle, includes organism (1), pump spraying device (2), cabin (3), rotor (5), motor (6) and stator (8), its characterized in that: the pump spraying device is characterized in that a pump spraying device (2) is arranged on the periphery of the machine body (1), a cabin (3) is arranged above the machine body (1), the bottom of the pump spraying device (2) is connected with a foldable rod frame (4), one end, far away from the pump spraying device (2), of the foldable rod frame (4) is connected with the machine body (1), a stator (8) and a rotor (5) are arranged inside the pump spraying device (2), an outer protective shell (7) is arranged outside the stator (8) and the rotor (5), a motor (6) is hermetically installed inside the machine body (1), a buffering moving device (9) is installed at the bottom of the machine body (1), a foldable foot rest (13) is connected to the bottom of the buffering moving device (9), a connecting bottom wheel (10) is arranged below the foldable foot rest (13), and the foldable foot rest (13) is connected with a control system (14), an inner seat (12) is arranged in the cabin (3), and a damping device (11) is arranged below the inner seat (12).
2. The novel manned unmanned aerial vehicle of claim 1, wherein: the aircraft engine body (1) is made of carbon fiber composite materials, the engine body (1) is of a cylindrical structure, and a hemispherical aviation organic glass window is arranged on the engine body (1).
3. The novel manned unmanned aerial vehicle of claim 1, wherein: the pump spraying device (2) is fixedly installed on a shaft of the motor (6), the motor (6) is connected with a power supply through an electric wire which is hermetically connected with the carbon-fiber composite material main machine body (1), 4 pump spraying devices (2) are arranged, and meanwhile the motor (6) is a waterproof motor.
4. The novel manned unmanned aerial vehicle of claim 1, wherein: the outer protective shell (7) is in a circular truncated cone shape, an interval exists between the outer protective shell (7) and the stator (8), and the stator (8) is distributed in an equal angle.
5. The novel manned unmanned aerial vehicle of claim 1, wherein: the stator (8) does not rotate in the flying state of the machine body (1), and the direction of the stator (8) faces upwards.
6. The novel manned unmanned aerial vehicle of claim 1, wherein: the shock absorption device (11) is composed of a shock absorption spring and a damping pad, and the shock absorption device (11) is arranged below the built-in seat (12).
7. The novel manned unmanned aerial vehicle of claim 1, wherein: the foldable foot rest (13) is made of carbon fiber composite materials, 4 foldable foot rests (13) are arranged, and the foldable foot rest (13) is connected with the connecting bottom wheel (10) through a shaft.
8. The novel manned unmanned aerial vehicle of claim 1, wherein: the control system (14) is composed of a control terminal, a lighting device, a GPS, a Beidou positioning device and an engine room environment control system.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110279027.9A CN112758327A (en) | 2021-03-16 | 2021-03-16 | Novel manned unmanned aerial vehicle |
| CN202110719487.9A CN113212758A (en) | 2021-03-16 | 2021-06-28 | Novel unmanned aerial vehicle that security performance is high |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110279027.9A CN112758327A (en) | 2021-03-16 | 2021-03-16 | Novel manned unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN112758327A true CN112758327A (en) | 2021-05-07 |
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Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110279027.9A Pending CN112758327A (en) | 2021-03-16 | 2021-03-16 | Novel manned unmanned aerial vehicle |
| CN202110719487.9A Pending CN113212758A (en) | 2021-03-16 | 2021-06-28 | Novel unmanned aerial vehicle that security performance is high |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110719487.9A Pending CN113212758A (en) | 2021-03-16 | 2021-06-28 | Novel unmanned aerial vehicle that security performance is high |
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| CN (2) | CN112758327A (en) |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2557421Y (en) * | 2002-07-23 | 2003-06-25 | 武舟山 | Inner wing for helicopter |
| CN101367435A (en) * | 2008-09-16 | 2009-02-18 | 广州伟韬电子科技有限公司 | Novel air injection aerial vehicle |
| CN106741876B (en) * | 2016-12-28 | 2022-07-29 | 深圳市道通智能航空技术股份有限公司 | Unmanned aerial vehicle |
| CN207106875U (en) * | 2017-08-21 | 2018-03-16 | 杭州木书科技有限公司 | A kind of dual-purpose shooting unmanned plane in vacant lot |
| CN207985195U (en) * | 2018-03-13 | 2018-10-19 | 清远市巨劲科技有限公司 | A kind of folding unmanned plane of taking photo by plane |
| CN111591438A (en) * | 2020-06-01 | 2020-08-28 | 北京理工大学重庆创新中心 | Air-ground dual-purpose unmanned vehicle |
-
2021
- 2021-03-16 CN CN202110279027.9A patent/CN112758327A/en active Pending
- 2021-06-28 CN CN202110719487.9A patent/CN113212758A/en active Pending
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| CN113212758A (en) | 2021-08-06 |
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Application publication date: 20210507 |