CN205345338U - Large -scale unmanned aerial vehicle of multipurpose - Google Patents
Large -scale unmanned aerial vehicle of multipurpose Download PDFInfo
- Publication number
- CN205345338U CN205345338U CN201620142242.9U CN201620142242U CN205345338U CN 205345338 U CN205345338 U CN 205345338U CN 201620142242 U CN201620142242 U CN 201620142242U CN 205345338 U CN205345338 U CN 205345338U
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- trigger
- air pump
- frame
- wing
- ball float
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Abstract
Large -scale unmanned aerial vehicle of multipurpose belongs to unmanned aerial vehicle equipment field, including frame, wing, rotor screw, carbon fiber rod, balloon, bull stick, rotation ware, floater ware, parachute, trigger, control system, camera, thermal imaging head, radar probe and air pump, the frame both sides is equipped with the wing, and there is the bull stick at the frame rear portion, is equipped with the rotor screw of VTOL on wing and the bull stick, and the rotor screw is other to be equipped with carbon fiber rod, the last balloon that is equipped with of carbon fiber rod, and frame upper portion is equipped with rotates ware, floater ware, trigger, control system, is equipped with the parachute on the trigger, rotates the ware and connects two bull sticks, and camera, thermal imaging head, radar probe, air pump are installed to the frame lower part, control system is connected with rotation ware, floater ware, trigger, camera, thermal imaging head, radar probe and air pump through the wire, and the air pump is connected with the balloon.
Description
Technical field
This utility model relates to the large-scale unmanned plane of multipurpose, belongs to unmanned plane apparatus field.
Background technology
Fast development along with ocean development implementation and economy, the use of unmanned plane is more and more extensive, but current unmanned plane is typically all small-sized gyroplane, it is essentially available for land short distance cruise, and easily air crash safety is poor, more it is difficult to carry out operation on the sea task, is currently a urgent problem.
Summary of the invention
The purpose of this utility model is to provide the large-scale unmanned plane of multipurpose.
Problem to be solved in the utility model is the deficiency that unmanned plane function singleness is easily had an accident.
For realizing the purpose of this utility model, the technical solution adopted in the utility model is:
The large-scale unmanned plane of multipurpose, including frame, wing, propeller aircraft, carbon fiber rod, balloon, bull stick, rot, ball float device, parachute, trigger, control system, photographic head, thermal imaging head, radar probe and air pump, described frame both sides is provided with wing, there is bull stick at frame rear portion, wing and bull stick are provided with the propeller aircraft of VTOL, carbon fiber rod it is provided with by propeller aircraft, carbon fiber rod is provided with balloon, upper rack is provided with rot, ball float device, trigger, control system, trigger is provided with parachute, rot connects two bull sticks, frame lower is provided with photographic head, thermal imaging head, radar probe, air pump.
Described control system is connected with air pump with rot, ball float device, trigger, photographic head, thermal imaging head, radar probe by wire, and air pump is connected with balloon.
Balancing weight, compression spring, lever, extension spring and pulley it is provided with in described trigger, compression spring is provided with balancing weight, balancing weight is slidably matched with lever one end on one side, and the lever other end connects extension spring, and parachute bracing wire is connected with extension spring by pulley.
Being provided with electromagnetism expansion link, metallic sodium, thin film, water and expansion flexible plastic in described ball float device, isolated by thin film between metallic sodium and water, thin film is provided with the electromagnetism expansion link of tip on one side, expands flexible plastic and is positioned at ball float device top.
The utility model has the advantages that: this unmanned plane can realize the dual-use function of VTOL and long-distance flight, multiple-task can be performed simultaneously, also there is anti-air crash function, safe and reliable, use suitable convenience, should have the wide market space.
Accompanying drawing explanation
Fig. 1 is the top perspective view of the large-scale unmanned plane of this utility model multipurpose；
Fig. 2 is the top perspective view of the large-scale unmanned plane of this utility model multipurpose；
Fig. 3 is trigger schematic internal view；
Fig. 4 is ball float device schematic internal view；
In figure: 1, frame 2, wing 3, propeller aircraft 4, carbon fiber rod 5, balloon 6, bull stick 7, rot 8, ball float device 9, parachute 10, trigger 11, control system 12, photographic head 13, thermal imaging 14, radar probe 15, air pump 16, balancing weight 17, compression spring 18, lever 19, extension spring 20, pulley 21, electromagnetism expansion link 22, metallic sodium 23, thin film 24, water 25, expand flexible plastic.
Detailed description of the invention
Below in conjunction with drawings and Examples, this utility model is further described.
The large-scale unmanned plane of multipurpose, including frame 1, wing 2, propeller aircraft 3, carbon fiber rod 4, balloon 5, bull stick 6, rot 7, ball float device 8, parachute 9, trigger 10, control system 11, photographic head 12, thermal imaging 13, radar probe 14 and air pump 15, described frame 1 both sides is provided with wing 2, wing carries small sized turbine jet engine 2 times, it is provided that powerful horizontal flight power；Frame 1 rear portion has bull stick 6, wing 2 and bull stick 6 to be provided with the propeller aircraft 3 of VTOL, and propeller aircraft 3 is other is provided with carbon fiber rod 4, has good elasticity；Carbon fiber rod 4 is provided with balloon 5, and frame 1 top is provided with rot 7, ball float device 8, trigger 10 and control system 11, and trigger 10 is provided with parachute 9, and rot 7 connects two bull sticks 6, center of gravity during scalable flight and attitude；Frame 1 bottom is provided with photographic head 12, thermal imaging 13, radar probe 14 and air pump 15, is used for performing each task.
Described control system 11 is connected with air pump 15 with rot 7, ball float device 8, trigger 10, photographic head 12, thermal imaging 13, radar probe 14 by wire, it is achieved the Based Intelligent Control to various kinds of equipment；Air pump 15 is connected with balloon 5, once need at sea to land, air pump 15 inflates to balloon 5, can float across the sea.
Balancing weight 16, compression spring 17, lever 18, extension spring 19 and pulley 20 it is provided with in described trigger 10, compression spring 17 is provided with balancing weight 16, balancing weight 16 is slidably matched with lever 18 one end on one side, lever 18 other end connects extension spring 19, parachute 9 bracing wire is connected with extension spring 19 by pulley 20, once airplane fault runs out of steam, balancing weight 16 rises under compression spring 17 effect, L-shaped lever 18 bottom and balancing weight 16 depart from, extension spring 19 action is made to pull parachute 9 bracing wire, thus releasing a parachute 9, it is prevented that accident.
It is provided with electromagnetism expansion link 21, metallic sodium 22, thin film 23, water 24 in described ball float device 8 and expands flexible plastic 25, isolated by thin film 23 between metallic sodium 22 and water 24, thin film 23 is provided with the electromagnetism expansion link 21 of tip on one side, expand flexible plastic 25 and be positioned at ball float device 8 top, once electromagnetism expansion link 21 action is by thin film 23, the hydrogen that reaction produces will be filled with expanding flexible plastic 25, thus producing lift can prevent tenesmus, it is simple to the recovery in later stage.
Using method of the present utility model: when needs perform maritime cruising task; can pass through after propeller aircraft 3 VTOL in horizontal flight; general flying power is up to 200km; once engine failure runs out of steam; can preventing air crash by the duplicate protection of parachute 9 and ball float device 8, efficiency height will not lose again aircraft.
Claims (4)
1. the large-scale unmanned plane of multipurpose, including frame (1), wing (2), propeller aircraft (3), carbon fiber rod (4), balloon (5), bull stick (6), rot (7), ball float device (8), parachute (9), trigger (10), control system (11), photographic head (12), thermal imaging head (13), radar probe (14) and air pump (15), it is characterized in that: described frame (1) both sides is provided with wing (2), there is bull stick (6) at frame (1) rear portion, wing (2) and bull stick (6) are provided with the propeller aircraft (3) of VTOL, propeller aircraft (3) is other is provided with carbon fiber rod (4), carbon fiber rod (4) is provided with balloon (5), and frame (1) top is provided with rot (7), ball float device (8), trigger (10), control system (11), trigger (10) is provided with parachute (9), and rot (7) connects two bull sticks (6), and frame (1) bottom is provided with photographic head (12), thermal imaging head (13), radar probe (14), air pump (15).
2. the large-scale unmanned plane of multipurpose according to claim 1, it is characterized in that: described control system (11) is connected with air pump (15) with rot (7), ball float device (8), trigger (10), photographic head (12), thermal imaging head (13), radar probe (14) by wire, and air pump (15) is connected with balloon (5).
3. the large-scale unmanned plane of multipurpose according to claim 1, it is characterized in that: in described trigger (10), be provided with balancing weight (16), compression spring (17), lever (18), extension spring (19) and pulley (20), compression spring (17) is provided with balancing weight (16), balancing weight (16) is slidably matched with lever (18) one end on one side, lever (18) other end connects extension spring (19), and parachute (9) bracing wire is connected with extension spring (19) by pulley (20).
4. the large-scale unmanned plane of multipurpose according to claim 1, it is characterized in that: be provided with electromagnetism expansion link (21), metallic sodium (22), thin film (23), water (24) in described ball float device (8) and expand flexible plastic (25), isolated by thin film (23) between metallic sodium (22) and water (24), thin film (23) is provided with the electromagnetism expansion link (21) of tip on one side, expands flexible plastic (25) and is positioned at ball float device (8) top.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620142242.9U CN205345338U (en) | 2016-02-26 | 2016-02-26 | Large -scale unmanned aerial vehicle of multipurpose |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620142242.9U CN205345338U (en) | 2016-02-26 | 2016-02-26 | Large -scale unmanned aerial vehicle of multipurpose |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205345338U true CN205345338U (en) | 2016-06-29 |
Family
ID=56179209
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620142242.9U Expired - Fee Related CN205345338U (en) | 2016-02-26 | 2016-02-26 | Large -scale unmanned aerial vehicle of multipurpose |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205345338U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105752336A (en) * | 2016-02-26 | 2016-07-13 | 舟山巨洋技术开发有限公司 | Multipurpose large-sized unmanned aerial vehicle |
| CN106218873A (en) * | 2016-08-23 | 2016-12-14 | 成都翼高九天科技有限公司 | The anti-protection structure of crashing of a kind of unmanned plane |
| TWI657012B (en) * | 2018-06-01 | 2019-04-21 | 大陸商昆山安費諾正日電子有限公司 | Aircraft with umbrella structure |
| CN110478828A (en) * | 2019-09-07 | 2019-11-22 | 励土峰 | A kind of parachute ball and its extinguishing method for fire extinguishing |
-
2016
- 2016-02-26 CN CN201620142242.9U patent/CN205345338U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105752336A (en) * | 2016-02-26 | 2016-07-13 | 舟山巨洋技术开发有限公司 | Multipurpose large-sized unmanned aerial vehicle |
| CN106218873A (en) * | 2016-08-23 | 2016-12-14 | 成都翼高九天科技有限公司 | The anti-protection structure of crashing of a kind of unmanned plane |
| TWI657012B (en) * | 2018-06-01 | 2019-04-21 | 大陸商昆山安費諾正日電子有限公司 | Aircraft with umbrella structure |
| CN110478828A (en) * | 2019-09-07 | 2019-11-22 | 励土峰 | A kind of parachute ball and its extinguishing method for fire extinguishing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160629 Termination date: 20190226 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |