CN205044614U - On -vehicle unmanned aerial vehicle device that independently takes off - Google Patents
On -vehicle unmanned aerial vehicle device that independently takes off Download PDFInfo
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- CN205044614U CN205044614U CN201520784719.9U CN201520784719U CN205044614U CN 205044614 U CN205044614 U CN 205044614U CN 201520784719 U CN201520784719 U CN 201520784719U CN 205044614 U CN205044614 U CN 205044614U
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Abstract
The utility model relates to an unmanned aerial vehicle field provides an on -vehicle unmanned aerial vehicle device that independently takes off, and on -vehicle application of taking off of the small -size unmanned aerial vehicle of unmanned aerial vehicle and security problem have been solved to this kind of mode. The utility model discloses a device is including fixing device (3), angle modulation support, locking device, the angle modulation support includes pivot (4), angle modulation backup pad (5), rotates backup pad (6), fixed plate (7), locking device includes lockpin (8), unblock steering wheel (10), action draw gear (11). After the take -off speed who sets for was reachd to sensor measurements's airspeed, PWM signal control unblock steering wheel (8) unblock was sent in self -driving appearance (10) control, and unmanned aerial vehicle breaks away from the device that takes off, gets into the airline operation.
Description
Technical field
The invention belongs to aerocraft dolly takeoff technical field, relate to a kind of SUAV (small unmanned aerial vehicle) dolly takeoff method, and relate to vehicle transmitting architected.
Background technology
Unmanned plane dolly takeoff refers to and unmanned plane is placed on roof, utilizes the speed of automobile that unmanned plane is taken to takeoff speed, then discharges.Existing dolly takeoff technology is that unmanned plane is fixed on the vehicle-mounted fixing rack of automobile top, four points of locking unmanned plane skid, and automobile accelerates to unmanned plane takeoff speed, and utilize and manually pull open fixing lock, remotely pilotless machine takes off.
Existing unmanned plane dolly takeoff apparatus and method have some shortcoming following:
1, below 40kg SUAV (small unmanned aerial vehicle) is only applicable to;
2, the angle of car-mounted device is non-adjustable;
3, manually unblank to add risk of taking off;
4, unmanned plane is by multi-point fastening on launcher, adds and unlocks failed risk.
5, these features limit the promotion and application of unmanned plane dolly takeoff device above.
Summary of the invention
(1) goal of the invention
Main purpose of the present invention improves unmanned plane dolly takeoff apparatus and method, improves the take-off weight of dolly takeoff unmanned plane, reduce dolly takeoff stage Risk, improve unmanned plane service efficiency.
(2) technical scheme
The test macro that the present invention relates to by vehicle-mounted (comprising car-mounted device/unblock) system, DATA REASONING and register system (comprise speed, highly, rotating speed, the sensor such as shooting), control system etc. forms.
The present invention reaches the object of independently taking off in places such as highways by a complete SUAV (small unmanned aerial vehicle) dolly takeoff system.First by calculating the angle of attack of unmanned plane under normal rolling start condition and takeoff speed scope, according to the angle of attack adjustment car-mounted device setting angle calculated, and corresponding angle is fixed on dolly takeoff device.Aero-engine thrust direction is consistent with dolly working direction.Start the engine also accelerates by dolly drives aircraft, when dolly accelerate to take off speed range time autopilot control to unblank steering wheel action, aircraft departs from dolly and also climbs according to autopilot setup parameter, and enters the course line set.
The invention provides the autonomous launching apparatus of a kind of vehicle-mounted unmanned aerial vehicle, comprise anchor fitting (3), angle-adjusting bracket, blocking device;
Angle-adjusting bracket comprises rotating shaft (4), angular adjustment stay bearing plate (5), rotational support plate (6), adapter plate (7); Blocking device comprises lock pin (8), unlocks steering wheel (10), action draw gear (11);
The skid of unmanned plane (1) (2) can be locked on the rotational support plate (6) of angle-adjusting bracket by the lock pin (8) of blocking device, anchor fitting (3) is fixed on roof (9), adapter plate (7) is connected with anchor fitting (3), rotational support plate (6) and adapter plate (7) are by rotating shaft (4) pivot joint, angular adjustment stay bearing plate (5) one end is fixed on adapter plate (7), and in the positioning groove of angular adjustment stay bearing plate (5), there is multiple position location, rotational support plate (6) has the hole of grafting locating dowel pin, locating dowel pin can be positioned in any one position location of positioning groove,
The rocking arm unlocking steering wheel (10) connects lock pin (8) by action draw gear (11), unlocking steering wheel (10) can drive described rocking arm to rotate, and unlocks steering wheel (10) and is controlled by airborne autopilot (12).
Especially, angular adjustment stay bearing plate (5) is with angle dish at quarter, and angle dish at quarter shows the angle of rotational support plate (6) and adapter plate (7)
(3) beneficial effect
Compared with original unmanned plane dolly takeoff apparatus and method, advantage of the present invention:
1, add angle regulator, the unmanned plane of more volume and weight can be carried;
2, redesign blocking device, reduce the risk of takeoff phase;
3, achieve Full-automatic unlocking and take off, to the application popularization of unmanned plane, there is the effect of actively promoting.
Accompanying drawing explanation
Fig. 1-unmanned plane and car-mounted device scheme of installation;
Fig. 2-skid and tripper;
1-unmanned plane, 2-skid, 3-anchor fitting, 4-rotating shaft, 5-angular adjustment stay bearing plate, 6-rotational support plate, 7-adapter plate, 8-lock pin, 9-roof, 10-unlocks steering wheel, 11-action draw gear, the airborne autopilot of 12-.
Detailed description of the invention
Provide the autonomous launching apparatus of a kind of vehicle-mounted unmanned aerial vehicle, comprise anchor fitting (3), angle-adjusting bracket, blocking device;
Angle-adjusting bracket comprises rotating shaft (4), angular adjustment stay bearing plate (5), rotational support plate (6), adapter plate (7); Blocking device comprises lock pin (8), unlocks steering wheel (10), action draw gear (11);
The skid of unmanned plane (1) (2) can be locked on the rotational support plate (6) of angle-adjusting bracket by the lock pin (8) of blocking device, anchor fitting (3) is fixed on roof (9), adapter plate (7) is connected with anchor fitting (3), rotational support plate (6) and adapter plate (7) are by rotating shaft (4) pivot joint, angular adjustment stay bearing plate (5) one end is fixed on adapter plate (7), and in the positioning groove of angular adjustment stay bearing plate (5), there is multiple position location, rotational support plate (6) has the hole of grafting locating dowel pin, locating dowel pin can be positioned in any one position location of positioning groove,
The rocking arm unlocking steering wheel (10) connects lock pin (8) by action draw gear (11), unlocking steering wheel (10) can drive described rocking arm to rotate, and unlocks steering wheel (10) and is controlled by airborne autopilot (12).
Particularly: angular adjustment stay bearing plate (5) is with angle dish at quarter, and angle dish at quarter shows the angle of rotational support plate (6) and adapter plate (7)
Test method and step:
1, the skid (2) of unmanned plane (1) is fixed on rotational support plate (6), locked;
2, angular adjustment stay bearing plate (5) is mixed up according to the unmanned plane take-off angle of attack;
3, automobile starting accelerates;
4, after the air speed measured when airborne airspeed sensor arrives the takeoff speed of setting, autopilot (12) controls to send pwm signal control unblock steering wheel (10) and unlocks, and unmanned plane departs from launching apparatus, enters airline operation.
Claims (2)
1. the autonomous launching apparatus of vehicle-mounted unmanned aerial vehicle, is characterized in that: comprise anchor fitting (3), angle-adjusting bracket, blocking device;
Angle-adjusting bracket comprises rotating shaft (4), angular adjustment stay bearing plate (5), rotational support plate (6), adapter plate (7); Blocking device comprises lock pin (8), unlocks steering wheel (10), action draw gear (11);
The skid of unmanned plane (1) (2) can be locked on the rotational support plate (6) of angle-adjusting bracket by the lock pin (8) of blocking device, anchor fitting (3) is fixed on roof (9), adapter plate (7) is connected with anchor fitting (3), rotational support plate (6) and adapter plate (7) are by rotating shaft (4) pivot joint, angular adjustment stay bearing plate (5) one end is fixed on adapter plate (7), and in the positioning groove of angular adjustment stay bearing plate (5), there is multiple position location, rotational support plate (6) has the hole of grafting locating dowel pin, locating dowel pin can be positioned in any one position location of positioning groove,
The rocking arm unlocking steering wheel (10) connects lock pin (8) by action draw gear (11), unlocking steering wheel (10) can drive described rocking arm to rotate, and unlocks steering wheel (10) and is controlled by airborne autopilot (12).
2. the autonomous launching apparatus of vehicle-mounted unmanned aerial vehicle according to claim 1, is characterized in that: angular adjustment stay bearing plate (5) is with angle dish at quarter, and angle dish at quarter shows the angle of rotational support plate (6) and adapter plate (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201520784719.9U CN205044614U (en) | 2015-10-10 | 2015-10-10 | On -vehicle unmanned aerial vehicle device that independently takes off |
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| CN201520784719.9U CN205044614U (en) | 2015-10-10 | 2015-10-10 | On -vehicle unmanned aerial vehicle device that independently takes off |
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Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN106080354A (en) * | 2016-07-22 | 2016-11-09 | 国网电力科学研究院武汉南瑞有限责任公司 | Operation Van patrolled and examined by a kind of power transmission line unmanned machine being applicable to alpine terrain |
| CN106394886A (en) * | 2016-06-15 | 2017-02-15 | 珠海市磐石电子科技有限公司 | Multi-axis aircraft capable of movably flying, flying assisting platform and flying method |
| CN106494636A (en) * | 2016-10-20 | 2017-03-15 | 北京华信宇航科技有限公司 | Trailed model vehicle launch system and its discharger |
| CN108609196A (en) * | 2016-12-10 | 2018-10-02 | 中国人民解放军军械工程学院 | Unmanned propeller-parachuting is vehicle-mounted to let platform fly away |
| CN108873930A (en) * | 2018-05-31 | 2018-11-23 | 苏州市启献智能科技有限公司 | Unmanned plane landing method and system based on mobile platform |
| CN108928500A (en) * | 2018-09-05 | 2018-12-04 | 成都云鼎智控科技有限公司 | A kind of fixed-wing unmanned plane emitter |
| CN109094811A (en) * | 2017-06-20 | 2018-12-28 | 成都飞机工业（集团）有限责任公司 | Multipoint positioning locking, quick release mechanism |
| CN111392057A (en) * | 2019-12-31 | 2020-07-10 | 航天时代飞鸿技术有限公司 | A on-vehicle machinery device of flying that lets for unmanned aerial vehicle |
| CN111427376A (en) * | 2020-04-02 | 2020-07-17 | 重庆市亿飞智联科技有限公司 | Unmanned aerial vehicle take-off method and device, storage medium, automatic pilot and unmanned aerial vehicle |
| CN111422371A (en) * | 2020-03-12 | 2020-07-17 | 西安羚控电子科技有限公司 | Ground launching system and control method for fixed-wing unmanned aerial vehicle |
| CN114228599A (en) * | 2016-04-29 | 2022-03-25 | 深圳市大疆创新科技有限公司 | System and method for unmanned aerial vehicle transport and data acquisition |
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| CN114228599A (en) * | 2016-04-29 | 2022-03-25 | 深圳市大疆创新科技有限公司 | System and method for unmanned aerial vehicle transport and data acquisition |
| CN114228599B (en) * | 2016-04-29 | 2023-11-17 | 深圳市大疆创新科技有限公司 | System and method for unmanned aerial vehicle transportation and data acquisition |
| CN106394886A (en) * | 2016-06-15 | 2017-02-15 | 珠海市磐石电子科技有限公司 | Multi-axis aircraft capable of movably flying, flying assisting platform and flying method |
| CN106080354A (en) * | 2016-07-22 | 2016-11-09 | 国网电力科学研究院武汉南瑞有限责任公司 | Operation Van patrolled and examined by a kind of power transmission line unmanned machine being applicable to alpine terrain |
| CN106494636A (en) * | 2016-10-20 | 2017-03-15 | 北京华信宇航科技有限公司 | Trailed model vehicle launch system and its discharger |
| CN106494636B (en) * | 2016-10-20 | 2019-01-15 | 北京华信宇航科技有限公司 | Trailed model vehicle launch system and its emitter |
| CN108609196A (en) * | 2016-12-10 | 2018-10-02 | 中国人民解放军军械工程学院 | Unmanned propeller-parachuting is vehicle-mounted to let platform fly away |
| CN109094811A (en) * | 2017-06-20 | 2018-12-28 | 成都飞机工业（集团）有限责任公司 | Multipoint positioning locking, quick release mechanism |
| CN108873930A (en) * | 2018-05-31 | 2018-11-23 | 苏州市启献智能科技有限公司 | Unmanned plane landing method and system based on mobile platform |
| CN108928500A (en) * | 2018-09-05 | 2018-12-04 | 成都云鼎智控科技有限公司 | A kind of fixed-wing unmanned plane emitter |
| CN111392057B (en) * | 2019-12-31 | 2021-06-08 | 航天时代飞鸿技术有限公司 | A on-vehicle machinery device of flying that lets for unmanned aerial vehicle |
| CN111392057A (en) * | 2019-12-31 | 2020-07-10 | 航天时代飞鸿技术有限公司 | A on-vehicle machinery device of flying that lets for unmanned aerial vehicle |
| CN111422371A (en) * | 2020-03-12 | 2020-07-17 | 西安羚控电子科技有限公司 | Ground launching system and control method for fixed-wing unmanned aerial vehicle |
| CN111422371B (en) * | 2020-03-12 | 2023-02-17 | 西安羚控电子科技有限公司 | Ground launching system and control method for fixed-wing unmanned aerial vehicle |
| CN111427376A (en) * | 2020-04-02 | 2020-07-17 | 重庆市亿飞智联科技有限公司 | Unmanned aerial vehicle take-off method and device, storage medium, automatic pilot and unmanned aerial vehicle |
| CN111427376B (en) * | 2020-04-02 | 2024-05-24 | 重庆市亿飞智联科技有限公司 | Unmanned aerial vehicle take-off method and device, storage medium, autopilot and unmanned aerial vehicle |
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Address after: 723213 Liulin Town, Chenggu County, Hanzhong City, Shaanxi Province Patentee after: Shaanxi Aircraft Industry Co.,Ltd. Address before: Box 34, Hanzhong City, Shaanxi Province, 723213 Patentee before: Shaanxi Aircraft INDUSTRY(GROUP) Co.,Ltd. |