CN204297121U - A kind of vertical unmanned plane launcher - Google Patents
A kind of vertical unmanned plane launcher Download PDFInfo
- Publication number
- CN204297121U CN204297121U CN201420668005.7U CN201420668005U CN204297121U CN 204297121 U CN204297121 U CN 204297121U CN 201420668005 U CN201420668005 U CN 201420668005U CN 204297121 U CN204297121 U CN 204297121U
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- CN
- China
- Prior art keywords
- launching trolley
- unmanned plane
- cylinder
- launching
- servomotor
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Abstract
The utility model discloses a kind of vertical unmanned plane launcher, it comprises launching trolley (1), emitter and grab ground device, the top of launching trolley (1) is provided with perpendicular to launching trolley (1) and is in the spring (3) of compressive state, the top of spring (3) is provided with transmitting station (4), rubber band (7) is provided with between transmitting station (4) and launching trolley (1), the piston rod of cylinder (5) is provided with the blade (6) for cutting off rubber band (7), oil cylinder (8) is perpendicular to launching trolley (1) and be fixedly mounted on the bottom of launching trolley (1), the piston rod of oil cylinder (8) is provided with the servomotor (9) perpendicular to launching trolley (1), the output shaft of servomotor (9) is provided with the drill bit (10) for drilling stratum.The beneficial effects of the utility model are: easily arrive most launch place, can carry out remote transmission unmanned plane, can carry out unmanned plane transmitting on uneven terrain.
Description
Technical field
The utility model relates to the technical field, particularly a kind of vertical unmanned plane launcher of the transmitting of launching unmanned plane.
Background technology
At present, taking off of SUAV is mainly adopted in two ways: hand is thrown and launched.Hand mode of throwing is taken off, is difficult to ensure that unmanned plane takes off the normal attitude of volume, very easily unsuccessfully.Ejection mode, all that employing is vehicle-mounted or fixed, and some SUAV weight is many more than 5 kilograms, length, more than 1 meter, is not easy to carry in complexity advance, and is difficult to arrive best launch site, larger restriction is had for the performance giving full play to unmanned plane, in addition, ejection mode needs just can launch under the environment of level terrain, and this limits use.Therefore, in order to adapt to the demand of modern war and rescue and relief work, being badly in need of a kind of lighter in weight, can being carried by individual soldier, the unmanned plane launcher of unmanned plane transmitting can be carried out under the adverse circumstances such as various weather and sand and dust.
Utility model content
The purpose of this utility model is the shortcoming overcoming prior art, provides the vertical unmanned plane launcher that a kind of structure simply, easily arrives most launch place, can carry out remote transmission unmanned plane, can carry out unmanned plane transmitting on uneven terrain.
The purpose of this utility model is achieved through the following technical solutions: a kind of vertical unmanned plane launcher, it comprises launching trolley, emitter and grab ground device, the bottom of launching trolley is provided with multiple universal wheel, described emitter is by spring, transmitting station, cylinder, blade and rubber band composition, the top of launching trolley is provided with perpendicular to launching trolley and is in the spring of compressive state, the top of spring is provided with transmitting station, rubber band is provided with between transmitting station and launching trolley, the top of launching trolley is also installed with cylinder, the piston rod of cylinder is provided with the blade for cutting off rubber band, described grabs ground device by oil cylinder, servomotor and drill bit composition, oil cylinder is perpendicular to launching trolley and be fixedly mounted on the bottom of launching trolley, the piston rod of oil cylinder is provided with the servomotor perpendicular to launching trolley, the output shaft of servomotor is provided with the drill bit for drilling stratum.
Described transmitting station is arranged perpendicular to spring.
It also comprises controller, and described controller is connected with cylinder, servomotor and oil cylinder.
The bottom of described launching trolley is provided with four universal wheels.
The utility model has the following advantages: the bottom of (1) launching trolley of the present utility model is provided with four universal wheels, thus can move whole launcher on the hill path of complicated landform.(2) drill bit of the present utility model can wedging in stratum, thus firmly whole launcher is fixed on the ground, avoid whole launcher displacement, simultaneously for the transmitting of unmanned plane provides advantage, therefore, be particularly suitable for carrying out unmanned plane transmitting on uneven terrain.(3) piston rod of cylinder of the present utility model is provided with the blade for cutting off rubber band, after rubber band is cut off by blade, unmanned plane is shifted onto in the air by the spring being in compressive state under the effect of spring restoring force, thus achieve the transmitting of unmanned plane, without the need to artificial field operation, only need operated from a distance, operate very simple.(4) controller of the present utility model stretching out or retracting with the piston rod of control cylinder and oil cylinder, can also control startup or the closedown of servomotor simultaneously, thus can the transmitting of Long-distance Control unmanned plane.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
In figure, 1-launching trolley, 2-universal wheel, 3-spring, 4-transmitting station, 5-cylinder, 6-blade, 7-rubber band, 8-oil cylinder, 9-servomotor, 10-drill bit.
Detailed description of the invention
Be further described the utility model below in conjunction with accompanying drawing, protection domain of the present utility model is not limited to the following stated:
As shown in Figure 1, a kind of vertical unmanned plane launcher, it comprises launching trolley 1, emitter and grabs ground device, and the bottom of launching trolley 1 is provided with four universal wheels 2, thus can move whole launcher on the hill path of complicated landform.As shown in Figure 1, emitter is by spring 3, transmitting station 4, cylinder 5, blade 6 and rubber band 7 form, the top of launching trolley 1 is provided with perpendicular to launching trolley 1 and is in the spring 3 of compressive state, the top of spring 3 is provided with the transmitting station 4 perpendicular to spring 3, unmanned plane is placed on transmitting station 4, rubber band 7 is provided with between transmitting station 4 and launching trolley 1, the top of launching trolley 1 is also installed with cylinder 5, the piston rod of cylinder 5 is provided with the blade 6 for cutting off rubber band 7, after rubber band 7 is cut off by blade 6, unmanned plane is shifted onto in the air by the spring 3 being in compressive state under the effect of spring restoring force, thus achieve the transmitting of unmanned plane.As shown in Figure 1, grab ground device by oil cylinder 8, servomotor 9 and drill bit 10 form, oil cylinder 8 is perpendicular to launching trolley 1 and be fixedly mounted on the bottom of launching trolley 1, the piston rod of oil cylinder 8 is provided with the servomotor 9 perpendicular to launching trolley 1, the output shaft of servomotor 9 is provided with the drill bit 10 for drilling stratum, under the condition that accident of terrain is whole, the piston rod controlling oil cylinder 8 stretches out control servomotor 9 simultaneously and starts, drill bit 10 just can wedging in stratum, thus firmly whole launcher is fixed on the ground, avoid whole launcher displacement, simultaneously for the transmitting of unmanned plane provides advantage, therefore, be particularly suitable for carrying out unmanned plane transmitting on uneven terrain.
It also comprises controller, described controller is connected with cylinder 5, servomotor 9 and oil cylinder 8, launching crew can via controller stretching out or retracting with the piston rod of control cylinder 5 and oil cylinder 8, can also control startup or the closedown of servomotor 9 simultaneously, thus can the transmitting of Long-distance Control unmanned plane.
The course of work of the present utility model is as follows: be first placed on by unmanned plane on transmitting station 4, again launching trolley 1 is moved to suitable transmitting landform, then the piston rod controlling oil cylinder 8 stretches out control servomotor 9 simultaneously and starts, drill bit 10 just can wedging in stratum, thus firmly whole launcher is fixed on the ground, finally the piston rod of control cylinder 5 is only needed to stretch out, blade 6 moves to rubber band 7 direction with piston rod, rubber band 7 cuts off by blade 6, unmanned plane is shifted onto in the air by spring 3 under the effect of restoring force, thus achieves the transmitting of unmanned plane.
The above is only preferred embodiment of the present utility model, be to be understood that the utility model is not limited to the form disclosed by this paper, should not regard the eliminating to other embodiments as, and can be used for other combinations various, amendment and environment, and can in contemplated scope described herein, changed by the technology of above-mentioned instruction or association area or knowledge.And the change that those skilled in the art carry out and change do not depart from spirit and scope of the present utility model, then all should in the protection domain of the utility model claims.
Claims (4)
1. a vertical unmanned plane launcher, it is characterized in that: it comprises launching trolley (1), emitter and grab ground device, the bottom of launching trolley (1) is provided with multiple universal wheel (2), described emitter is by spring (3), transmitting station (4), cylinder (5), blade (6) and rubber band (7) composition, the top of launching trolley (1) is provided with perpendicular to launching trolley (1) and is in the spring (3) of compressive state, the top of spring (3) is provided with transmitting station (4), rubber band (7) is provided with between transmitting station (4) and launching trolley (1), the top of launching trolley (1) is also installed with cylinder (5), the piston rod of cylinder (5) is provided with the blade (6) for cutting off rubber band (7), described grabs ground device by oil cylinder (8), servomotor (9) and drill bit (10) composition, oil cylinder (8) is perpendicular to launching trolley (1) and be fixedly mounted on the bottom of launching trolley (1), the piston rod of oil cylinder (8) is provided with the servomotor (9) perpendicular to launching trolley (1), the output shaft of servomotor (9) is provided with the drill bit (10) for drilling stratum.
2. the vertical unmanned plane launcher of one according to claim 1, is characterized in that: described transmitting station (4) is arranged perpendicular to spring (3).
3. the vertical unmanned plane launcher of one according to claim 1, is characterized in that: it also comprises controller, and described controller is connected with cylinder (5), servomotor (9) and oil cylinder (8).
4. the vertical unmanned plane launcher of one according to claim 1, is characterized in that: the bottom of described launching trolley (1) is provided with four universal wheels (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420668005.7U CN204297121U (en) | 2014-11-11 | 2014-11-11 | A kind of vertical unmanned plane launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420668005.7U CN204297121U (en) | 2014-11-11 | 2014-11-11 | A kind of vertical unmanned plane launcher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204297121U true CN204297121U (en) | 2015-04-29 |
Family
ID=53102684
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420668005.7U Withdrawn - After Issue CN204297121U (en) | 2014-11-11 | 2014-11-11 | A kind of vertical unmanned plane launcher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204297121U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104401500A (en) * | 2014-11-11 | 2015-03-11 | 成都航天万欣科技有限公司 | Vertical unmanned aerial vehicle launcher |
| WO2020010611A1 (en) * | 2018-07-13 | 2020-01-16 | 彭子航 | Forward-thrust-type launch process method for aerospace vehicle, and apparatus therefor |
-
2014
- 2014-11-11 CN CN201420668005.7U patent/CN204297121U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104401500A (en) * | 2014-11-11 | 2015-03-11 | 成都航天万欣科技有限公司 | Vertical unmanned aerial vehicle launcher |
| WO2020010611A1 (en) * | 2018-07-13 | 2020-01-16 | 彭子航 | Forward-thrust-type launch process method for aerospace vehicle, and apparatus therefor |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20150429 Effective date of abandoning: 20160413 |
|
| C25 | Abandonment of patent right or utility model to avoid double patenting |