CN209833984U - Arresting mechanism for sliding and landing of unmanned aerial vehicle - Google Patents
Arresting mechanism for sliding and landing of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN209833984U CN209833984U CN201920456007.2U CN201920456007U CN209833984U CN 209833984 U CN209833984 U CN 209833984U CN 201920456007 U CN201920456007 U CN 201920456007U CN 209833984 U CN209833984 U CN 209833984U
- Authority
- CN
- China
- Prior art keywords
- hook
- aerial vehicle
- unmanned aerial
- connecting plate
- arresting
- 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.)
- Expired - Fee Related
Links
- 230000008878 coupling Effects 0.000 claims abstract 2
- 238000010168 coupling process Methods 0.000 claims abstract 2
- 238000005859 coupling reaction Methods 0.000 claims abstract 2
- 239000008188 pellet Substances 0.000 claims 1
- 230000000903 blocking effect Effects 0.000 abstract description 7
- 239000000969 carrier Substances 0.000 description 2
- 230000000149 penetrating effect Effects 0.000 description 2
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model relates to an auxiliary mechanism field of supplementary unmanned aerial vehicle, especially an unmanned aerial vehicle slubby landing arrestment mechanism, including organism and runway, its characterized in that, the main undercarriage middle part of organism is fixed with the connecting plate, and connecting plate one end articulates there is the L type to block the hook, and there is the spring coupling to block main undercarriage and L type to block the hook connecting plate below, and bolted fixation has release on the organism back end bottom, and the L type blocks the hook and places on release, places the load piece on both sides around the runway, connects through blocking the cable between the load piece, the utility model discloses simple structure reduces required runway length when unmanned aerial vehicle slubby descends.
Description
Technical Field
The utility model relates to an auxiliary mechanism field, especially an unmanned aerial vehicle slubby landing arresting mechanism of assisting unmanned aerial vehicle.
Background
Traditional unmanned aerial vehicle relies on the parachute increase resistance to descend when descending, and the distance of slumping is long, requires highly to the runway.
Disclosure of Invention
In order to solve the problem, the utility model provides an unmanned aerial vehicle slubby landing arresting mechanism.
The sliding landing arresting mechanism for the unmanned aerial vehicle comprises a machine body and a runway, and is characterized in that a connecting plate is fixed in the middle of a main undercarriage of the machine body, an L-shaped arresting hook is hinged to one end of the connecting plate, a spring is arranged below the connecting plate and connected with the main undercarriage and the L-shaped arresting hook, a releasing device is fixed on the bottom of the rear section of the machine body through a bolt, the L-shaped arresting hook is placed on the releasing device, weight blocks are placed on the front side and the rear side of the runway, and the weight blocks are connected through arresting cables.
Furthermore, elastic small balls are uniformly penetrated on the arresting cable.
Furthermore, the releasing mechanism comprises a steering engine and a steering engine disc which are fixed on the bottom of the rear section of the machine body, an arc-shaped hook is arranged on the steering engine disc, a fixing ring is welded on the upper portion of the L-shaped blocking hook, and the fixing ring is arranged on the arc-shaped hook in a penetrating mode.
When the elevator is used and descends, the control rudder rotates clockwise for an angle, the L-shaped blocking hook slides down from the arc-shaped hook of the steering engine disc, hooks the blocking cable and decelerates through the load-bearing block.
The utility model discloses simple structure reduces required runway length when unmanned aerial vehicle runs and descends.
Drawings
Figure 1 is a front view of the present invention
Fig. 2 is a top view of the present invention
Figure 3 front view of the release device and L-shaped catch structure
Fig. 4 left side view of the release device and L-shaped catch structure
In fig. 1 to 4, 1, a machine body, 2, a runway, 101, a main landing gear, 3, a connecting plate, 4, an L-shaped blocking hook, 401, a fixing ring, 5, a spring, 6, a release device, 601, a steering engine, 602, a steering engine disc, 603, an arc-shaped hook, 7, a weight loading block, 8, a blocking cable, 9 and an elastic ball.
Detailed Description
In fig. 1 to 4, the sliding and landing arresting mechanism for the unmanned aerial vehicle comprises a machine body 1 and a runway 2, and is characterized in that a connecting plate 3 is fixed in the middle of a main undercarriage 101 of the machine body 1, one end of the connecting plate 3 is hinged with an L-shaped arresting hook 4, a spring 5 is arranged below the connecting plate 3 and connected with the main undercarriage 101 and the L-shaped arresting hook 4, a releasing device 6 is fixed on the bottom of the rear section of the machine body 1 through a bolt, the L-shaped arresting hook 4 is arranged on the releasing device 6, weight carriers 7 are arranged on the front side and the rear side of the runway 2, and the weight carriers 7 are connected through arresting cables 8.
Furthermore, elastic 9 balls are uniformly penetrated on the arresting cable 8.
Further, the release mechanism 6 comprises a steering engine 601 and a steering engine disk 602 which are fixed on the bottom of the rear section of the machine body 1, an arc-shaped hook 603 is arranged on the steering engine disk 602, a fixing ring 401 is welded on the upper portion of the L-shaped blocking hook 4, and the fixing ring 401 is arranged on the arc-shaped hook 603 in a penetrating mode.
Claims (3)
1. The utility model provides an unmanned aerial vehicle sliding landing arresting mechanism, includes organism and runway, its characterized in that, the main undercarriage middle part of organism is fixed with the connecting plate, and connecting plate one end articulates there is L type to block the hook, and main undercarriage and L type are blocked the hook to spring coupling below the connecting plate, and the bolt fastening has a release on the organism back end bottom, and L type blocks the hook and places on release, places the weight piece on the both sides around the runway, connects through the arrester cable between the weight piece.
2. An unmanned aerial vehicle rolloff and landing arresting mechanism according to claim 1, wherein the arresting cable is evenly threaded with elastic pellets.
3. An unmanned aerial vehicle running and landing arresting mechanism according to claim 2, wherein the releasing mechanism comprises a steering engine and a steering engine disc which are fixed to the bottom of the rear section of the machine body, an arc-shaped hook is arranged on the steering engine disc, a fixing ring is welded to the upper portion of the L-shaped arresting hook, and the fixing ring is threaded on the arc-shaped hook.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920456007.2U CN209833984U (en) | 2019-04-05 | 2019-04-05 | Arresting mechanism for sliding and landing of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920456007.2U CN209833984U (en) | 2019-04-05 | 2019-04-05 | Arresting mechanism for sliding and landing of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209833984U true CN209833984U (en) | 2019-12-24 |
Family
ID=68909984
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920456007.2U Expired - Fee Related CN209833984U (en) | 2019-04-05 | 2019-04-05 | Arresting mechanism for sliding and landing of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209833984U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112278313A (en) * | 2020-11-05 | 2021-01-29 | 湖南浩天翼航空技术有限公司 | Landing arresting rope mechanism of sliding unmanned aerial vehicle |
| CN112678196A (en) * | 2021-01-19 | 2021-04-20 | 西安爱生技术集团公司 | Cross-shaped supporting structure of unmanned aerial vehicle arresting cable, arresting system and method |
| CN113212784A (en) * | 2021-06-28 | 2021-08-06 | 天津大学 | Meeting butt joint device for ferry airship |
| WO2022080916A1 (en) * | 2020-10-15 | 2022-04-21 | 카페24 주식회사 | Device for supporting takeoff and landing of aerial vehicle |
| KR20220049785A (en) * | 2020-10-15 | 2022-04-22 | 카페24 주식회사 | An apparatus for supporting taking off and landing of flying object |
| KR20220049787A (en) * | 2020-10-15 | 2022-04-22 | 카페24 주식회사 | A method for controlling a device for supporting taking off and landing of flying object |
-
2019
- 2019-04-05 CN CN201920456007.2U patent/CN209833984U/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022080916A1 (en) * | 2020-10-15 | 2022-04-21 | 카페24 주식회사 | Device for supporting takeoff and landing of aerial vehicle |
| WO2022080626A1 (en) * | 2020-10-15 | 2022-04-21 | 카페24 주식회사 | Device for supporting takeoff and landing of aerial vehicle |
| KR20220049785A (en) * | 2020-10-15 | 2022-04-22 | 카페24 주식회사 | An apparatus for supporting taking off and landing of flying object |
| KR20220049787A (en) * | 2020-10-15 | 2022-04-22 | 카페24 주식회사 | A method for controlling a device for supporting taking off and landing of flying object |
| KR102400867B1 (en) * | 2020-10-15 | 2022-05-24 | 카페24 주식회사 | An apparatus for supporting taking off and landing of flying object |
| KR102422870B1 (en) * | 2020-10-15 | 2022-07-21 | 카페24 주식회사 | A method for controlling a device for supporting taking off and landing of flying object |
| CN112278313A (en) * | 2020-11-05 | 2021-01-29 | 湖南浩天翼航空技术有限公司 | Landing arresting rope mechanism of sliding unmanned aerial vehicle |
| CN112678196A (en) * | 2021-01-19 | 2021-04-20 | 西安爱生技术集团公司 | Cross-shaped supporting structure of unmanned aerial vehicle arresting cable, arresting system and method |
| CN113212784A (en) * | 2021-06-28 | 2021-08-06 | 天津大学 | Meeting butt joint device for ferry airship |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209833984U (en) | Arresting mechanism for sliding and landing of unmanned aerial vehicle | |
| CA2930986C (en) | Plane tractor | |
| CN107719689B (en) | One kind being used for unmanned plane tow trailer device | |
| CN204488768U (en) | A kind of railless free-wheeled vehicle transport stall protection system arrester wires device | |
| US3640490A (en) | Shipborne conveying means | |
| US11014654B2 (en) | Pitch trimmer | |
| CN103969019A (en) | Drop test device with delivery and posture adjusting function | |
| CN103786694B (en) | The automobile-used speed runaway protection system of a kind of trackless rubber-tyred | |
| US20200223664A1 (en) | Overspeed safety brake | |
| CN112829959B (en) | Fixed wing unmanned aerial vehicle removes transmission and retrieves integration platform | |
| CN103935341B (en) | A kind of for the urgent arrester in the malfunctioning situation of automobile brake system | |
| US2692121A (en) | Burden-switching apparatus and method | |
| CN108820240B (en) | Blocking device for carrier-based aircraft of aircraft carrier | |
| US2696957A (en) | Landing and launching system for aircraft | |
| CN213323748U (en) | Heavy-load unmanned aerial vehicle landing platform | |
| CN207631519U (en) | A kind of three-stage aircraft tractor | |
| CN209080653U (en) | A kind of wheeled Liftable bulk goods hopper | |
| CN108032998B (en) | Unmanned aerial vehicle undercarriage wheel-load signal device based on shock strut and torque arm | |
| CN209493268U (en) | Submarine omnidirectional runs AGV vehicle | |
| CN207725463U (en) | A kind of medium-sized wheel brake | |
| CN208616205U (en) | A kind of aircraft carrier arresting gear | |
| CN206107594U (en) | A catapult -assisted take -off device for model aeroplane and model ship stationary vane and unmanned aerial vehicle | |
| CN212358132U (en) | Tunnel inclined shaft swift current car arresting gear | |
| CN221189095U (en) | Unmanned aerial vehicle carries load cabin coupling mechanism | |
| CN109059617B (en) | Multi-stage deceleration missile launching test recovery device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191224 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |