CN212125521U - Six-hole jet type vertical take-off and landing unmanned aerial vehicle - Google Patents
Six-hole jet type vertical take-off and landing unmanned aerial vehicle Download PDFInfo
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- CN212125521U CN212125521U CN202020752037.0U CN202020752037U CN212125521U CN 212125521 U CN212125521 U CN 212125521U CN 202020752037 U CN202020752037 U CN 202020752037U CN 212125521 U CN212125521 U CN 212125521U
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Abstract
The utility model discloses a six hole jet-propelled VTOL unmanned aerial vehicle, include the organism, spout engine, oil tank, jet-propelled pipe and carrier a little, the organism includes shell, skeleton and flight control mainboard, the shell cover on the surface of skeleton and with skeleton fixed connection, the inside fixedly connected with flight control mainboard of shell, the tip of skeleton stretches out shell and last fixed surface is connected with and spouts the engine a little, the jet of spouting the engine a little is equipped with the jet-propelled pipe, the middle part fixedly connected with oil tank of skeleton, oil tank outside fixedly connected with oil pump, the oil pump is connected with flight control mainboard, be connected through oil pipe between oil pump and the jet-propelled engine a little, the bottom of organism is equipped with the carrier a little. The utility model discloses a be equipped with six micro-jet engines on the surface of organism, compare in rotor unmanned aerial vehicle can possess better flight speed and thrust, be fit for more being used for article transportation and removing, improved unmanned aerial vehicle transportation article's work efficiency.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a six hole jet type VTOL 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.
At present, unmanned aerial vehicle in the market is the rotor structure mostly, drives unmanned aerial vehicle flight through the screw, but rotor unmanned aerial vehicle thrust when the flying speed is slower and flight is less, receives very big restriction when transporting the goods, and this type of unmanned aerial vehicle adopts the lithium cell to supply power mostly, need consume longer charge time, has reduced unmanned aerial vehicle and has transported the efficiency when the goods. For this reason, a new technical solution needs to be designed for solution.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a six hole jet-propelled VTOL unmanned aerial vehicle is equipped with six and spouts the engine a little through the surface at the organism, compares in rotor unmanned aerial vehicle can possess better flight speed and thrust, is fit for being used for article transportation and removal more, has improved unmanned aerial vehicle transportation article's work efficiency.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a six hole jet-propelled VTOL unmanned aerial vehicle, includes the organism, spouts engine, oil tank, jet-propelled pipe and carrier a little, the organism includes shell, skeleton and flies the accuse mainboard, the shell cover on the surface of skeleton and with skeleton fixed connection, the inside fixedly connected with of shell flies the accuse mainboard, the tip of skeleton stretches out shell and goes up fixed surface and spout the engine a little, the jet of spouting the engine a little is equipped with jet-propelled pipe, the middle part fixedly connected with oil tank of skeleton, oil tank outside fixedly connected with oil pump, the oil pump with fly the accuse mainboard and be connected, be connected through oil pipe between oil pump and the jet-propelled engine a little, the bottom of organism is equipped with the carrier a little, the carrier a little runs through shell and skeleton fixed connection.
As an improvement of the technical scheme, the framework is in a shape like a Chinese character 'wang', the bottom surface of the end part of the framework is fixedly connected with a supporting bracket, and the lower surface of the joint of the supporting bracket and the framework is fixedly connected with a first angle fixing block.
As an improvement of the technical scheme, the micro-jet engine comprises six micro-jet engines which are fixed on the surface of the framework in a bilateral symmetry mode, and the end parts of the micro-jet engines are sleeved inside the gas jet pipes and are in rotating connection with the gas jet pipes.
As an improvement of the technical scheme, the micro-jet engine adopts a diesel power micro-turbine jet engine.
As an improvement of the technical scheme, the end part of the framework is fixedly connected with a fixed plate in a vertical mode, one end of the air injection pipe is embedded in the fixed plate and is rotatably connected with the fixed plate, the top of the fixed plate is fixedly connected with a direction-adjusting steering engine, and the direction-adjusting steering engine is connected with a flight control main board.
As an improvement of the technical scheme, the upper surface of the joint of the fixing plate and the framework is fixedly connected with a second angular fixing block.
As the improvement of the technical scheme, the air injection pipe is made of a 90-degree bent pipe, the surface of the air injection pipe is connected with a fixing piece in a welded mode, a pull rod is arranged between the fixing piece and the working end of the direction-adjusting steering engine, and the two ends of the pull rod are respectively connected with the fixing piece and the steering engine in a rotating mode.
As an improvement of the technical scheme, the upper surface of the shell is fixedly connected with an oil filling port, and the oil filling port is communicated with an oil tank.
As an improvement of the technical scheme, the surface of the shell is provided with a ventilation opening, and the ventilation opening is positioned above the micro-jet engine and is embedded with a dust screen.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a be equipped with six micro-jet engines on the surface of organism, compare in rotor unmanned aerial vehicle can possess better flight speed and thrust, be fit for more being used for article transportation and removing, improved unmanned aerial vehicle transportation article's work efficiency.
2. The utility model discloses utilize to transfer to the jet-propelled pipe spout direction of steering wheel control, can effectually adjust jet-propelled angle, conveniently control unmanned aerial vehicle's flight state, use convenience more.
3. The utility model discloses use diesel oil to spout the engine a little as energy drive, the convenience adds fast when the oil mass is not enough, compares in the lithium cell that uses the electric energy, possess very fast energy supply speed, has shortened the time of waiting for to charge when using greatly.
Drawings
Fig. 1 is a schematic side view of a six-hole jet type vertical take-off and landing unmanned aerial vehicle according to the present invention;
fig. 2 is a schematic view of an end face structure of a six-hole jet type vertical take-off and landing unmanned aerial vehicle according to the present invention;
fig. 3 is a schematic side view of the fixing plate of the present invention;
fig. 4 is the structure diagram of the unmanned aerial vehicle control system of the present invention.
In the figure: the aircraft comprises an engine body-1, a micro-jet engine-2, an oil tank-3, a gas jet pipe-4, a carrier rack-5, a shell-6, a framework-7, a flight control main board-8, an oil pump-9, a support bracket-10, a corner fixing block-11, a fixing plate-12, a direction adjusting steering engine-13, a corner fixing block-14, a fixing piece-15, a pull rod-16, an oil filling port-17, a ventilation port-18 and a dust screen-19.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution: a six-hole jet type vertical take-off and landing unmanned aerial vehicle comprises a body 1, a micro-jet engine 2, an oil tank 3, a jet pipe 4 and a carrier 5, the aircraft body 1 comprises a shell 6, a framework 7 and a flight control mainboard 8, the shell 6 covers the surface of the framework 7 and is fixedly connected with the framework 7, a flight control main board 8 is fixedly connected inside the shell 6, the end part of the framework 7 extends out of the shell 6, the upper surface of the framework is fixedly connected with a micro-jet engine 2, the jet orifice of the micro-jet engine 2 is provided with a jet pipe 4, the middle part of the framework 7 is fixedly connected with an oil tank 3, an oil pump 9 is fixedly connected with the outer side of the oil tank 3, the oil pump 9 is connected with a flight control main board 8, the oil pump 9 is connected with the micro-jet engine 2 through an oil pipe, the bottom of the engine body 1 is provided with a carrier 5, and the carrier 5 penetrates through the outer shell 6 and is fixedly connected with the framework 7.
Further improved, as shown in fig. 1, the skeleton 7 is "king" font and the bottom surface fixedly connected with support bracket 10 of tip, the lower surface fixed connection of the junction of support bracket 10 and skeleton 7 has an angle fixed block 11, through designing "king" font skeleton 7, conveniently carries out fixed mounting to the micro-jetting engine 2, improves the stability of the installation of micro-jetting engine 2, utilizes at the junction fixed connection angle fixed block of support bracket 10 and skeleton 7, improves the stability that support bracket 10 and skeleton 7 are connected.
Further improved ground, as shown in fig. 1, the micro-jet engine 2 includes six and is the bilateral symmetry form and fixes the surface at skeleton 7, the tip of micro-jet engine 2 cup joints in the inside of jet pipe 4 and rotates with jet pipe 4 to be connected, through rotating jet pipe 4 and micro-jet engine 2 to be connected, conveniently adjusts the jet direction of jet pipe 4 to adjust unmanned aerial vehicle's flight state.
In a further improvement mode, the micro-jet engine 2 adopts a diesel power micro-turbine jet engine, and the power generated by diesel combustion is used for generating stronger thrust, so that better thrust and flight speed are provided for the unmanned aerial vehicle.
Further improved, as shown in fig. 1-3, the perpendicular fixedly connected with fixed plate 12 of tip of skeleton 7, the one end of jet-propelled pipe 4 is embedded in fixed plate 12 and rotates with fixed plate 12 to be connected, the top fixedly connected with of fixed plate 12 transfers to steering wheel 13, transfer to steering wheel 13 and fly to control mainboard 8 and be connected, through the perpendicular fixedly connected with fixed plate 12 of tip at skeleton 7, conveniently support and fix jet-propelled pipe 4, improve the stability of unmanned aerial vehicle flight in-process.
Further improved, as shown in fig. 2, the upper surface fixed connection of the joint of the fixing plate 12 and the framework 7 has an angular fixing block two 14, so that the stability of the end connection of the fixing plate 12 and the framework 7 is improved, and the stability of the structure of the unmanned aerial vehicle is enhanced.
Further improved, as shown in fig. 1-3, the air injection pipe 4 is made of a 90-degree bent pipe, the surface of the air injection pipe is connected with a fixing piece 15 in a welded mode, a pull rod 16 is arranged between the fixing piece 15 and the working end of the direction adjusting steering engine 13, two ends of the pull rod 16 are respectively connected with the fixing piece 15 and the steering engine in a rotating mode, the pull rod 16 is arranged between the output end of the direction adjusting steering engine 13 and the fixing piece 15, the air injection pipe 4 is driven to rotate by the steering engine conveniently, the air injection direction of the air injection pipe 4 is adjusted, and the flying control of the unmanned aerial vehicle.
Further improved, as shown in fig. 1, the upper surface of the housing 6 is fixedly connected with an oil filler 17, the oil filler 17 is communicated with the oil tank 3, the oil filler 17 is fixedly connected with the surface of the housing 6, diesel oil is conveniently added into the oil tank 3, and the energy charging efficiency of the unmanned aerial vehicle is improved.
Specifically, as shown in fig. 1, a vent 18 is formed in the surface of the housing 6, the vent 18 is located above the micro-jet engine 2 and embedded with a dust screen 19, and the vent 18 with the dust screen 19 is formed in the surface of the housing 6, so that air can conveniently and rapidly enter the micro-jet engine 2, the combustion efficiency in the micro-jet engine 2 is improved, and meanwhile, the air injection efficiency can be improved.
The flight control mainboard is an FC1212-S flight control mainboard, the oil pump is an 059130755BK diesel pump, and the steering engine is an LD-27MG steering engine.
The utility model discloses a be equipped with six micro-blasting engines 2 on the surface of organism 1, compare and can possess better flight speed and thrust in rotor unmanned aerial vehicle, be fit for being used for article transportation and removal more, improved the work efficiency of unmanned aerial vehicle transportation article, utilize to transfer to the 4 spout directions of steering wheel 13 control jet-propelled pipe, can effectually adjust jet-propelled angle, conveniently control unmanned aerial vehicle's flight state, use convenience more.
The utility model discloses when using, start unmanned aerial vehicle's jet engine 2 a little, fly and control mainboard 8 control oil pump 9 and give the oil mass, make jet engine 2 a little normally start, operating personnel passes through the remote controller to flying control mainboard 8 send instruction, fly and control mainboard 8 control body and transfer to steering wheel 13 and drive pull rod 16 and rotate, thereby adjust jet pipe 4's orientation, when jet pipe 4 vertical ground, improve oil pump 9's the oil supply volume, strengthen jet engine 2's thrust a little, make unmanned aerial vehicle rise perpendicularly, can adjust unmanned aerial vehicle's flight state when adjusting jet pipe 4's different orientation, because jet pipe 4's orientation can't blow to carrier 5 under, effectually avoid causing the damage to article when carrying the thing.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above, it will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, but that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (9)
1. The utility model provides a six hole jet-propelled VTOL unmanned aerial vehicle, includes organism (1), spouts engine (2), oil tank (3), jet-propelled pipe (4) and carrier (5), its characterized in that: the machine body (1) comprises a shell (6), a framework (7) and a flight control main board (8), the shell (6) covers the surface of the framework (7) and is fixedly connected with the framework (7), a flight control mainboard (8) is fixedly connected inside the shell (6), the end part of the framework (7) extends out of the shell (6), the upper surface of the framework is fixedly connected with a micro-jet engine (2), the jet orifice of the micro-jet engine (2) is provided with a jet pipe (4), the middle part of the framework (7) is fixedly connected with an oil tank (3), an oil pump (9) is fixedly connected with the outer side of the oil tank (3), the oil pump (9) is connected with a flight control main board (8), the oil pump (9) is connected with the micro-jet engine (2) through an oil pipe, the bottom of the machine body (1) is provided with a carrier (5), and the carrier (5) penetrates through the outer shell (6) and is fixedly connected with the framework (7).
2. A six-hole jet vertical take-off and landing drone according to claim 1, characterized in that: skeleton (7) are "king" font and the bottom surface fixedly connected with support bracket (10) of tip, the lower surface fixed connection of the junction of support bracket (10) and skeleton (7) has angle fixed block (11).
3. A six-hole jet vertical take-off and landing drone according to claim 1, characterized in that: the micro-jet engine (2) comprises six micro-jet engines and is fixed on the surface of the framework (7) in a bilateral symmetry mode, and the end part of each micro-jet engine (2) is sleeved inside the corresponding gas jet pipe (4) and is rotationally connected with the corresponding gas jet pipe (4).
4. A six-hole jet vertical take-off and landing drone according to claim 3, characterized in that: the micro-jet engine (2) adopts a diesel power micro-turbine jet engine.
5. A six-hole jet vertical take-off and landing drone according to claim 1, characterized in that: the end part of the framework (7) is fixedly connected with a fixing plate (12) in a vertical mode, one end of the air injection pipe (4) is embedded in the fixing plate (12) and is rotatably connected with the fixing plate (12), the top of the fixing plate (12) is fixedly connected with a steering engine (13), and the steering engine (13) is connected with a flight control main board (8).
6. A six-hole jet type VTOL UAV according to claim 5, wherein: and a second angular fixing block (14) is fixedly connected to the upper surface of the joint of the fixing plate (12) and the framework (7).
7. A six-hole jet type VTOL UAV according to claim 6, wherein: jet-propelled pipe (4) adopt 90 return bends to make and surperficial welded connection have stationary blade (15), stationary blade (15) and transfer to be equipped with pull rod (16) between the work end of steering wheel (13), the both ends of pull rod (16) rotate with stationary blade (15) and transfer to steering wheel (13) respectively and be connected.
8. A six-hole jet vertical take-off and landing drone according to claim 1, characterized in that: the upper surface of the shell (6) is fixedly connected with an oil filling port (17), and the oil filling port (17) is communicated with the oil tank (3).
9. A six-hole jet vertical take-off and landing drone according to claim 8, characterised in that: the surface of the shell (6) is provided with a ventilation opening (18), and the ventilation opening (18) is positioned above the micro-spraying engine (2) and is embedded with a dust screen (19).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020752037.0U CN212125521U (en) | 2020-05-09 | 2020-05-09 | Six-hole jet type vertical take-off and landing unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020752037.0U CN212125521U (en) | 2020-05-09 | 2020-05-09 | Six-hole jet type vertical take-off and landing unmanned aerial vehicle |
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| CN212125521U true CN212125521U (en) | 2020-12-11 |
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| CN202020752037.0U Expired - Fee Related CN212125521U (en) | 2020-05-09 | 2020-05-09 | Six-hole jet type vertical take-off and landing unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102385180B1 (en) * | 2020-12-21 | 2022-04-08 | 이정용 | Multi-directional jet propulsion drone |
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2020
- 2020-05-09 CN CN202020752037.0U patent/CN212125521U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102385180B1 (en) * | 2020-12-21 | 2022-04-08 | 이정용 | Multi-directional jet propulsion drone |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201211 Termination date: 20210509 |