CN208053674U - A kind of unmanned aerial vehicle ejecting launching apparatus - Google Patents
A kind of unmanned aerial vehicle ejecting launching apparatus Download PDFInfo
- Publication number
- CN208053674U CN208053674U CN201820343759.3U CN201820343759U CN208053674U CN 208053674 U CN208053674 U CN 208053674U CN 201820343759 U CN201820343759 U CN 201820343759U CN 208053674 U CN208053674 U CN 208053674U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- aerial vehicle
- card slot
- unmanned aerial
- launching apparatus
- 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.)
- Active
Links
Abstract
The utility model discloses a kind of unmanned aerial vehicle ejecting launching apparatus, include pushing component and release component on cabinet base or vehicular platform, the pushing component includes ejection orbit, sliding block and cylinder, the sliding block is installed on fuselage or the wing lower end of unmanned plane, and coordinates with ejection orbit and slide, the output end of the cylinder is equipped with pushing block, the pushing block is located at sliding block rear and sliding block can be pushed to move forward, the release component includes card slot and hook, the card slot is installed on the tail portion of unmanned plane, and the hook can catch on card slot.This catapult launcher is simple to operation, and the tail portion of unmanned plane is by discharging component locking, and upon discharge, unmanned plane is accelerated forwardly and pops up along ejection orbit under the promotion of pushing block, and moment takes off, ejection stability, and light-weight, small, very reliably.
Description
Technical field
The utility model is related to air vehicle technique field more particularly to a kind of unmanned aerial vehicle ejecting launching apparatus.
Background technology
Unmanned plane is taking photo by plane at present, agricultural, express transportation, disaster relief, is observing wild animal, monitoring passes, catching an illness, surveying
Paint, news report, electric inspection process, the disaster relief, the fields such as movies-making have had been more and more widely used, due to unmanned plane
Cost is very high, and user and businessman are intended to unmanned plane and less accident occur.
Unmanned plane occurs accident and is mainly happened at takeoff phase, and rising for unmanned plane is carried out by support launcher
Fly, can be very good the launching success rate for improving unmanned plane, the quick release that catapult-launching gear stores energy using system in advance is real
Now the moment for launching object is accelerated, is widely used in modern military and general industry, catapult-assisted take-off, guided missile such as aircraft carrier
Ejection launch, ejection escape seat, vehicle impact testing etc..The main function of shot support is that aircraft is accelerated to critical speed
Degree is the launching apparatus that aircraft can obtain that enough initial velocity break away from gravity flight.There are many kinds of classes for catapult-launching gear, there is steam
Ejection, rubber band ejection, electromagnetic launch and rocket-assisted ejection etc..But existing ejection mechanism is complicated, price is high
It is expensive, it is difficult to be suitable for small and medium size unmanned aerial vehicles.
Utility model content
In order to overcome the above-mentioned deficiencies of the prior art, the utility model provides nothing a kind of simple in structure and reliable and stable
Man-machine catapult launcher.
Technical solution is used by the utility model solves its technical problem：
A kind of unmanned aerial vehicle ejecting launching apparatus includes the pushing component on cabinet base or vehicular platform and release
Component, the pushing component include ejection orbit, sliding block and cylinder, and the sliding block is installed under the fuselage or wing of unmanned plane
End, and coordinate with ejection orbit and slide, the output end of the cylinder is equipped with pushing block, and the pushing block is located at sliding block rear and can
Sliding block Forward is pushed, the release component includes card slot and hook, and the card slot is installed on the tail portion of unmanned plane, and the hook can
Catch on card slot.
As an improvement of the above technical solution, the release component further includes supporting rack, and support frame as described above is equipped with support
Pin, the hook are rotated by fulcrum of supporting pin.
As an improvement of the above technical solution, the release component further includes motor, and described hook one end coordinates with card slot,
The other end connects rotating bar, and the rotating bar connects the output shaft of motor by rocking arm.
As an improvement of the above technical solution, a longeron is installed on unmanned plane, the card slot is set to longeron
Rear end.
As an improvement of the above technical solution, the pushing component is provided with two groups, is symmetrically dispersed in the machine of unmanned plane
Wing lower end.
As an improvement of the above technical solution, a crossbeam, the left and right ends point of the crossbeam are installed on unmanned plane
It An Zhuan not be there are two sliding block.
As an improvement of the above technical solution, the ejection orbit is horizontally or diagonally mounted on cabinet base or vehicle upward
On carrying platform.
The beneficial effects of the utility model have：
This catapult launcher is simple to operation, and the tail portion of unmanned plane is by discharging component locking, upon discharge, unmanned plane
It being accelerated forwardly and pops up along ejection orbit under the promotion of pushing block, moment takes off, ejection stability, and light-weight, small,
It is very reliable.
Description of the drawings
Below in conjunction with the accompanying drawings and specific embodiment the utility model is described in further detail, wherein：
Fig. 1 is the structural schematic diagram of the utility model embodiment；
Fig. 2 is that the utility model embodiment hides the vertical view after unmanned plane；
Fig. 3 is the partial enlarged view at A in Fig. 2；
Fig. 4 is that the utility model embodiment hides the front view after unmanned plane；
Fig. 5 is the partial enlarged view at B in Fig. 4.
Specific implementation mode
Referring to Fig. 1, a kind of unmanned aerial vehicle ejecting launching apparatus of the utility model, including it is mounted on cabinet base 1 or vehicle-mounted
Pushing component 2 on platform and release component 3, in the present embodiment, unmanned plane 4 is stored in babinet, pushing component 2 and release group
Part 3 is mounted on cabinet base 1.
With further reference to Fig. 4 and Fig. 5, the pushing component 2 is provided with two groups, is symmetrically dispersed in the wing of unmanned plane 4
Lower end, pushing component 2 include ejection orbit 21, sliding block 22 and cylinder 23, and the sliding block 22 is installed on the fuselage or machine of unmanned plane 4
Wing lower end, and coordinate with ejection orbit 21 and slide, the output end of the cylinder 23 is equipped with pushing block 24, and the pushing block 24 is located at
22 rear of sliding block simultaneously can push sliding block 22 to move forward, wherein the ejection orbit 21 is horizontally or diagonally mounted on babinet bottom upward
On seat 1 or vehicular platform, convenient for taking off.
With further reference to Fig. 2 and Fig. 3, the release component 3 includes card slot 31, hook 32, supporting rack 33 and motor 34, institute
The tail portion that card slot 31 is installed on unmanned plane 4 is stated, the hook 32 can catch on card slot 31, and support frame as described above 33 is mounted on cabinet base
On 1, it is equipped with supporting pin, the hook 32 is rotated by fulcrum of supporting pin, and 32 one end of the hook coordinates with card slot 31, the other end
Rotating bar 35 is connected, the rotating bar 35 connects the output shaft of motor 34 by rocking arm 36.
In addition, being installed with a longeron 5 and a crossbeam 6 on unmanned plane 4, the card slot 31 is set to the rear end of longeron 5,
The left and right ends of the crossbeam 6 are separately installed with two sliding blocks 22, and ejection is more stablized, light-weight, small, discharge component 3
After discharging hook 32, unmanned plane 4 is accelerated forwardly and pops up along ejection orbit 21 under the promotion of pushing block 24, and moment takes off.
The above, the only better embodiment of the utility model, but the utility model is not limited to above-mentioned reality
Example is applied, as long as it reaches the technique effect of the utility model with any same or similar means, should all belong to the utility model
Protection domain.
Claims (7)
1. a kind of unmanned aerial vehicle ejecting launching apparatus, it is characterised in that：It include the promotion on cabinet base or vehicular platform
Component and release component, the pushing component includes ejection orbit, sliding block and cylinder, and the sliding block is installed on the fuselage of unmanned plane
Or wing lower end, and coordinate with ejection orbit and slide, the output end of the cylinder is equipped with pushing block, and the pushing block is located at sliding block
Rear can simultaneously push sliding block to move forward, and the release component includes card slot and hook, and the card slot is installed on the tail portion of unmanned plane, institute
Card slot can be caught on by stating hook.
2. a kind of unmanned aerial vehicle ejecting launching apparatus according to claim 1, it is characterised in that：The release component further includes
Supporting rack, support frame as described above are equipped with supporting pin, and the hook is rotated by fulcrum of supporting pin.
3. a kind of unmanned aerial vehicle ejecting launching apparatus according to claim 2, it is characterised in that：The release component further includes
Motor, described hook one end coordinate with card slot, and the other end connects rotating bar, and the rotating bar connects the output of motor by rocking arm
Axis.
4. a kind of unmanned aerial vehicle ejecting launching apparatus according to claim 1, it is characterised in that：It is installed on unmanned plane
One longeron, the card slot are set to the rear end of longeron.
5. a kind of unmanned aerial vehicle ejecting launching apparatus according to claim 1, it is characterised in that：The pushing component is provided with
Two groups, it is symmetrically dispersed in the wing lower end of unmanned plane.
6. a kind of unmanned aerial vehicle ejecting launching apparatus according to claim 5, it is characterised in that：It is installed on unmanned plane
The left and right ends of one crossbeam, the crossbeam are separately installed with two sliding blocks.
7. a kind of unmanned aerial vehicle ejecting launching apparatus according to claim 1, it is characterised in that：The ejection orbit it is horizontal or
Shangdi is tilted towards on cabinet base or vehicular platform.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820343759.3U CN208053674U (en) | 2018-03-13 | 2018-03-13 | A kind of unmanned aerial vehicle ejecting launching apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820343759.3U CN208053674U (en) | 2018-03-13 | 2018-03-13 | A kind of unmanned aerial vehicle ejecting launching apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208053674U true CN208053674U (en) | 2018-11-06 |
Family
ID=63988949
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820343759.3U Active CN208053674U (en) | 2018-03-13 | 2018-03-13 | A kind of unmanned aerial vehicle ejecting launching apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208053674U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI696570B (en) * | 2019-04-11 | 2020-06-21 | 何三玄 | UAV, take-off and landing device and UAV system |
| WO2021093135A1 (en) * | 2019-11-12 | 2021-05-20 | 周鹏跃 | Multi-rotor aircraft and related method for air separation thereof from fixed-wing aircraft |
-
2018
- 2018-03-13 CN CN201820343759.3U patent/CN208053674U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI696570B (en) * | 2019-04-11 | 2020-06-21 | 何三玄 | UAV, take-off and landing device and UAV system |
| WO2021093135A1 (en) * | 2019-11-12 | 2021-05-20 | 周鹏跃 | Multi-rotor aircraft and related method for air separation thereof from fixed-wing aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208053674U (en) | A kind of unmanned aerial vehicle ejecting launching apparatus | |
| CN105480429A (en) | Unmanned aerial vehicle ejection device | |
| CN109353537B (en) | Locking and flying mechanism for unmanned aerial vehicle ejection | |
| DE60201338D1 (en) | DEVICE FOR STARTING A PLANE FROM A CARRIAGE PLANE | |
| CN107792371A (en) | A kind of unmanned plane space base rapid fire apparatus and method for system of being towed target based on aviation trailing cable | |
| CN106741948B (en) | It is a kind of to carry the unmanned plane for launching object | |
| CN106114890B (en) | A kind of small drone catapult-launching gear and unmanned plane takeoff method | |
| CN105460230A (en) | Pneumatic catapult-assisted take-off device and method used for unmanned plane | |
| CN107738750A (en) | A kind of accurate retracting device of unmanned plane space base and method of system of being towed target based on aviation trailing cable | |
| CN109250138B (en) | Medium-sized conveyor traction air-drop system and air-drop parameter determination method | |
| CN102530255A (en) | Accurate parachute landing device for traction type unmanned plane and method | |
| CN106976569B (en) | Ship-borne aircraft front-lifting ejection release dynamic load test device and test method thereof | |
| CN107176310B (en) | Unmanned aerial vehicle launching cradle | |
| CN111348191A (en) | Backward ejection type unmanned aerial vehicle launching method | |
| IT1185732B (en) | PARACADU SYSTEM AND EJECTABLE SEAT FOR AIRCRAFT INCORPORATING THE SAME | |
| CN205345355U (en) | Portable unmanned aerial vehicle transmitter | |
| US2981499A (en) | Aircraft with auxiliary launching aircraft | |
| US2350140A (en) | Airplane | |
| CN201525506U (en) | Catapult launching gear for flapping wing air craft | |
| CN105599917A (en) | Towing and carrying cart for catapult unmanned aerial vehicle | |
| CN105452798A (en) | Projectile for simulating bird strike | |
| CN205770199U (en) | A kind of SUAV catapult-launching gear | |
| CN108202876B (en) | Guarantor type unmanned aerial vehicle launches draw gear | |
| CN205770198U (en) | A kind of SUAV ejecting hook | |
| CN106043732A (en) | Small unmanned aerial vehicle catapulting hook |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP02 | Change in the address of a patent holder | ||
| CP02 | Change in the address of a patent holder |
Address after: Room 102, floor 1, 3 workshop, No. 6898, Zhuhai Avenue, Hongqi Town, Jinwan District, Zhuhai City, Guangdong Province Patentee after: ZHUHAI TIANQING AEROSPACE TECHNOLOGY Co.,Ltd. Address before: 519000 Guangdong Province, Zhuhai city planning exhibition hall on the third floor of the aviation city Jinwan District 312-30 room Patentee before: ZHUHAI TIANQING AEROSPACE TECHNOLOGY Co.,Ltd. |