CN111361724A - Hybrid rotor relay unmanned aerial vehicle - Google Patents
Hybrid rotor relay unmanned aerial vehicle Download PDFInfo
- Publication number
- CN111361724A CN111361724A CN202010233939.8A CN202010233939A CN111361724A CN 111361724 A CN111361724 A CN 111361724A CN 202010233939 A CN202010233939 A CN 202010233939A CN 111361724 A CN111361724 A CN 111361724A
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- Prior art keywords
- fixedly connected
- unmanned aerial
- oil
- aerial vehicle
- oil tank
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- Pending
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- 238000002955 isolation Methods 0.000 claims abstract description 19
- 239000000446 fuel Substances 0.000 claims abstract description 16
- 238000005086 pumping Methods 0.000 claims description 12
- 230000002457 bidirectional effect Effects 0.000 claims description 6
- 238000001914 filtration Methods 0.000 claims description 5
- 230000000149 penetrating effect Effects 0.000 claims 1
- 238000004891 communication Methods 0.000 abstract description 6
- 230000005611 electricity Effects 0.000 abstract description 4
- 238000005516 engineering process Methods 0.000 abstract description 3
- 230000005540 biological transmission Effects 0.000 abstract description 2
- 239000003921 oil Substances 0.000 description 54
- 239000000295 fuel oil Substances 0.000 description 13
- 238000000034 method Methods 0.000 description 6
- 239000002828 fuel tank Substances 0.000 description 3
- 238000005192 partition Methods 0.000 description 3
- 230000005574 cross-species transmission Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 241000883990 Flabellum Species 0.000 description 1
- 241001465754 Metazoa Species 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
-
- 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
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/04—Arrangement thereof in or on aircraft
-
- 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/06—Constructional adaptations thereof
- B64D37/08—Internal partitioning
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
- G08C17/02—Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
Abstract
The invention discloses a hybrid rotor relay unmanned aerial vehicle, which comprises a body, wherein two sides of the body are fixedly connected with rotors, the bottoms of the rotors are fixedly connected with supporting legs, the center of the bottom of an inner cavity of the body is fixedly connected with a small fuel generator, the bottom of the inner cavity of the body and the outer part of the small fuel generator are fixedly connected with an annular oil tank, the bottom of the inner surface of the annular oil tank is fixedly connected with an isolation frame, and a gap is reserved between the top of the isolation frame and the top of the inner surface of the annular oil tank. This hybrid rotor relay unmanned aerial vehicle of oil electricity through taking relay technology on unmanned aerial vehicle, utilizes signal transceiver receiving and dispatching signal, and unmanned aerial vehicle machine provides command platform as relay base station or communication node, increases communication distance, and extension coverage can solve no picture number transmission in remote area or 4G signal, uses this kind of relay, can shelter from the area for signal blind area, mountain forest and provide the signal guarantee.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a hybrid rotor relay unmanned aerial vehicle.
Background
An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
Present unmanned aerial vehicle all is rotor all around and blows downwards basically, controls unmanned aerial vehicle's removal through the rotational speed of control rotor flabellum all around, and when removing, obvious rocking can appear in the unmanned aerial vehicle body, to some fuel driven unmanned aerial vehicle, oil is to one side shifting, and its focus can obvious skew, and the difficult control of holistic balance.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides an oil-electricity hybrid rotor relay unmanned aerial vehicle, which solves the problems that the existing unmanned aerial vehicle basically blows air downwards through surrounding rotors, and for some oil-electricity hybrid driven unmanned aerial vehicles, the unmanned aerial vehicle body obviously shakes when moving, oil moves to one side, the gravity center of the unmanned aerial vehicle obviously shifts, and the whole balance is difficult to control.
In order to achieve the purpose, the invention is realized by the following technical scheme: the utility model provides an oil-electricity hybrid rotor relay unmanned aerial vehicle, includes the organism, the equal fixedly connected with rotor in both sides of organism, and the bottom fixedly connected with landing leg of rotor, the small-size fuel oil generator of center fixedly connected with of internal cavity bottom of the organism, the bottom of internal cavity of the organism and the outside fixedly connected with annular oil tank that is located small-size fuel oil generator, and the bottom fixedly connected with of annular oil tank internal surface keeps apart the frame, the top of keeping apart the frame leaves the space with the top of annular oil tank internal surface, the top of annular oil tank and each cavity that is located the isolation frame all run through there is the oil pumping branch pipe, the intercommunication has an oil collecting pipe between the top of oil pumping branch pipe, and the intercommunication has the oil feeding pipe between the rear side at oil collecting pipe top and the.
Preferably, the front side intercommunication at annular oil tank top has the oil filling pipe, the top of oil filling pipe runs through the organism and extends to the top of organism, and the top joint of oil filling pipe has the gas cap of straining.
Preferably, the outside fixedly connected with baffle that just is located small-size fuel generator between the top of organism internal surface and the lateral wall, and the top of baffle from left to right fixedly connected with battery and circuit board in proper order, the left side joint at organism top has the battery cover.
Preferably, the center of the bottom of the machine body is fixedly connected with a signal transceiver, and the front of the machine body is fixedly connected with a camera.
Preferably, the signal transceiver is connected with the master base station in a bidirectional manner through a wireless signal, the signal transceiver is connected with the circuit board in a bidirectional manner, and an output end of the signal transceiver is connected with an input end of the sub base station through a wireless signal.
Preferably, the output of camera and battery all passes through the input electric connection of wire and circuit board, the output of circuit board passes through the input electric connection of wire and rotor motor.
Advantageous effects
The invention provides an oil-electricity hybrid rotor relay unmanned aerial vehicle. Compared with the prior art, the method has the following beneficial effects:
(1) the oil-electricity hybrid rotor relay unmanned aerial vehicle is characterized in that a small fuel oil generator is fixedly connected to the center of the bottom of an inner cavity of a vehicle body, an annular oil tank is fixedly connected to the bottom of the inner cavity of the vehicle body and located outside the small fuel oil generator, an isolation frame is fixedly connected to the bottom of the inner surface of the annular oil tank, a gap is reserved between the top of the isolation frame and the top of the inner surface of the annular oil tank, oil pumping branch pipes penetrate through the top of the annular oil tank and located in each cavity of the isolation frame, an oil collecting pipe is communicated between the top ends of the oil pumping branch pipes, an oil supply pipe is communicated between the rear side of the top of the oil collecting pipe and an oil inlet of the small fuel oil generator, the isolation frame is arranged in the annular oil tank, fuel oil cannot be completely deflected to one side in the moving process of the unmanned aerial vehicle, the gravity center deflection, and gather through the collection oil pipe, make the isolation frame not influence the use of fuel, and synchronous extraction, more can keep centrobaric balance throughout, convenient to use, and the clearance that leaves at the isolation frame top makes the fuel accessible overflow the mode of adding spill over in each cavity, convenient to use.
(2) This hybrid rotor relay unmanned aerial vehicle of oil electricity, through passing through radio signal and total base station realization both way junction at signal transceiver, signal transceiver realizes both way junction with the treater, signal transceiver's output passes through radio signal and is connected with sub-base station's input, through taking relay technology on unmanned aerial vehicle, utilize signal transceiver send-receiver signal, unmanned aerial vehicle is as relay base station or communication node, provide command platform, increase communication distance, the extension coverage, can solve the no picture number of remote area and pass or 4G signal, use this kind to relay, can be the signal blind area, mountain midlyre shelters from the area and provides the signal guarantee.
Drawings
FIG. 1 is a front view of the structure of the present invention
FIG. 2 is a cross-sectional view of the housing of the present invention;
FIG. 3 is a top view of the internal structure of the annular fuel tank of the present invention;
FIG. 4 is a top view of the outer structure of the annular fuel tank of the present invention;
FIG. 5 is a top view of the housing of the present invention;
fig. 6 is a schematic block diagram of the system of the present invention.
In the figure: 1-machine body, 2-supporting legs, 3-rotor wing, 4-signal transceiver, 5-camera, 6-total base station, 7-rotor wing motor, 8-small fuel generator, 9-sub base station, 10-annular fuel tank, 11-isolation frame, 12-oil pumping branch pipe, 13-oil collecting pipe, 14-oil supplying pipe, 15-oil supplying pipe, 16-gas filtering cover, 17-partition board, 18-storage battery, 19-circuit board and 20-storage battery cover.
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. 1-6, the present invention provides a technical solution: an oil-electricity hybrid rotor relay unmanned aerial vehicle comprises a machine body 1, a partition plate 17 is fixedly connected between the top of the inner surface of the machine body 1 and the side wall and positioned outside a small fuel generator 8, a storage battery 18 and a circuit board 19 are fixedly connected to the top of the partition plate 17 from left to right in sequence, a storage battery cover 20 is clamped on the left side of the top of the machine body 1, a signal transceiver 4 is fixedly connected to the center of the bottom of the machine body 1, the signal transceiver 4 is a GV-CDT01 type wireless signal transceiver module, a camera 5 is fixedly connected to the front of the machine body 1, the signal transceiver 4 is in bidirectional connection with a master base station 6 through wireless signals, the signal transceiver 4 is in bidirectional connection with the circuit board 19, the output end of the signal transceiver 4 is connected with the input end of a slave base station 9 through wireless signals, signals are transmitted and received by the signal transceiver, the unmanned aerial vehicle is used as a relay base station or a communication node, a command platform is provided, the communication distance is increased, the coverage range is expanded, the problem that a remote area has no image data transmission or 4G signals can be solved, the relay can be used for providing signal guarantee for a signal blind area and a mountain and dense forest sheltered area, a data link between the unmanned aerial vehicles is divided into an uplink and a downlink, the uplink controls the unmanned aerial vehicle through an instruction, the downlink is a telemetering link, telemetering information on the unmanned aerial vehicle is transmitted to a ground station, the output ends of the camera 5 and the storage battery 18 are electrically connected with the input end of the circuit board 19 through wires, the output end of the circuit board 19 is electrically connected with the input end of the rotor motor 7 through wires, the two sides of the machine body 1 are fixedly connected with the rotors 3, the bottom of the rotors 3 is fixedly connected with, an annular oil tank 10 is fixedly connected to the bottom of an inner cavity of a machine body 1 and positioned outside a small-sized fuel generator 8, an isolation frame 11 is fixedly connected to the bottom of the inner surface of the annular oil tank 10, an oil filling pipe 15 is communicated with the front side of the top of the annular oil tank 10, the top end of the oil filling pipe 15 penetrates through the machine body 1 and extends to the upper portion of the machine body 1, an air filtering cover 16 is clamped at the top end of the oil filling pipe 15, a gap is reserved between the top of the isolation frame 11 and the top of the inner surface of the annular oil tank 10, oil pumping branch pipes 12 penetrate through the top of the annular oil tank 10 and positioned in each cavity of the isolation frame 11, an oil collecting pipe 13 is communicated between the top ends of the oil pumping branch pipes 12, an oil supply pipe 14 is communicated between the rear side of the top of the oil collecting pipe 13 and an oil inlet of the small-sized fuel generator 8, further improved stability, set up the oil pumping branch pipe and draw the fuel in step from each cavity that the isolation frame was separated to assemble through the collection oil pipe, make the isolation frame not influence the use of fuel, and draw in step, more can keep centrobaric balance all the time, convenient to use, and the space that the isolation frame top was left makes the fuel accessible overflow the mode of interpolation spill over in each cavity, convenient to use.
When the unmanned aerial vehicle is used, the gas filtering cover 16 is firstly screwed off, fuel oil is injected into the annular oil tank 10 through the oil filling pipe 15, the fuel oil in one cavity can stretch to the surrounding cavity after being filled with the fuel oil until the cavity is filled with the fuel oil, the gas filtering cover 16 is then covered, the unmanned aerial vehicle is remotely controlled to fly up, the small fuel oil generator 8 extracts the fuel oil in the annular oil tank 10 through the oil supply pipe 14, the oil collection pipe 13 and the oil pumping branch pipe 12, then the fuel oil is operated to generate electricity, the electricity is stored in the storage battery 18 and is provided to enable the rotor motor 7 to rotate, the upward power is provided to drive the device to ascend, during signal transmission, the master base station 6 sends an instruction and a signal to be transmitted to the unmanned aerial vehicle, after the signal is received by the signal transceiver 4 of the unmanned aerial vehicle and is identified and processed by the processor on the circuit board 19, the signal is sent to the appointed base, and sends the video data to the overall base station 6 via the signal transceiver 4 for position determination.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an unmanned aerial vehicle is relayed to hybrid rotor, includes organism (1), the equal fixedly connected with rotor (3) in both sides of organism (1), and the bottom fixedly connected with landing leg (2) of rotor (3), its characterized in that: the oil pumping device is characterized in that a small fuel generator (8) is fixedly connected to the center of the bottom of an inner cavity of the engine body (1), the bottom of the inner cavity of the engine body (1) is located on an annular oil tank (10) fixedly connected to the outer portion of the small fuel generator (8), an isolation frame (11) is fixedly connected to the bottom of the inner surface of the annular oil tank (10), a gap is reserved between the top of the isolation frame (11) and the top of the inner surface of the annular oil tank (10), oil pumping branch pipes (12) are arranged in the top of the annular oil tank (10) and located in each cavity of the isolation frame (11) in a penetrating mode, oil collecting pipes (13) are communicated between the top ends of the oil pumping branch pipes (12), and oil supply pipes (14) are communicated between the rear side of the top of the.
2. The hybrid rotor relay drone of claim 1, characterized in that: the front side at the top of the annular oil tank (10) is communicated with an oil filling pipe (15), the top end of the oil filling pipe (15) penetrates through the machine body (1) and extends to the upper part of the machine body (1), and the top end of the oil filling pipe (15) is clamped with an air filtering cover (16).
3. The hybrid rotor relay drone of claim 2, characterized in that: the external fixedly connected with baffle (17) that just is located small-size fuel generator (8) between the top of organism (1) internal surface and the lateral wall, and the top of baffle (17) from left to right fixedly connected with battery (18) and circuit board (19) in proper order, the left side joint at organism (1) top has battery cover (20).
4. The hybrid rotor relay drone of claim 1, characterized in that: the center of organism (1) bottom fixedly connected with signal transceiver (4), the front fixedly connected with camera (5) of organism (1).
5. The hybrid rotor relay drone of claim 1, characterized in that: the signal transceiver (4) is in bidirectional connection with the main base station (6) through wireless signals, the signal transceiver (4) is in bidirectional connection with the circuit board (19), and the output end of the signal transceiver (4) is connected with the input end of the sub base station (9) through the wireless signals.
6. The hybrid rotor relay drone of claim 3, characterized in that: the output of camera (5) and battery (18) all passes through the input electric connection of wire and circuit board (19), the output of circuit board (19) passes through the input electric connection of wire and rotor motor (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010233939.8A CN111361724A (en) | 2020-03-28 | 2020-03-28 | Hybrid rotor relay unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010233939.8A CN111361724A (en) | 2020-03-28 | 2020-03-28 | Hybrid rotor relay unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN111361724A true CN111361724A (en) | 2020-07-03 |
Family
ID=71201026
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010233939.8A Pending CN111361724A (en) | 2020-03-28 | 2020-03-28 | Hybrid rotor relay unmanned aerial vehicle |
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| Country | Link |
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| CN (1) | CN111361724A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114926948A (en) * | 2021-03-25 | 2022-08-19 | 北京国电高科科技有限公司 | Forestry fire prevention monitoring method and system based on satellite Internet of things |
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2020
- 2020-03-28 CN CN202010233939.8A patent/CN111361724A/en active Pending
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|---|---|---|---|---|
| KR20160120383A (en) * | 2015-04-07 | 2016-10-18 | 만진항공건설 주식회사 | Tank of a hollow cylinder for unmanned vehicle |
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| CN114926948A (en) * | 2021-03-25 | 2022-08-19 | 北京国电高科科技有限公司 | Forestry fire prevention monitoring method and system based on satellite Internet of things |
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Application publication date: 20200703 |