CN201368702Y - Take-off vehicle - Google Patents
Take-off vehicle Download PDFInfo
- Publication number
- CN201368702Y CN201368702Y CNU2008201898854U CN200820189885U CN201368702Y CN 201368702 Y CN201368702 Y CN 201368702Y CN U2008201898854 U CNU2008201898854 U CN U2008201898854U CN 200820189885 U CN200820189885 U CN 200820189885U CN 201368702 Y CN201368702 Y CN 201368702Y
- Authority
- CN
- China
- Prior art keywords
- take
- target drone
- vehicle
- tripod
- thrust
- 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 - Lifetime
Links
Images
Landscapes
- Valves And Accessory Devices For Braking Systems (AREA)
Abstract
The utility model relates to a take-off vehicle, which is a take-off device of a target drone (unmanned aircraft). The parking, ground debugging and take-off subjects of the target drone are realized via an airframe and a variety of devices arranged on the airframe to ensure the normal flying of the target drone. The utility model makes a great improvement on the original take-off vehicle in order to meet the performance improvement and the function expansion of the target drone. The take-off vehicle comprises a vehicle body and a cool-air system, wherein the vehicle body comprises a frame, accessories arranged on the frame, a front wheel component, a main wheel component, a slide rail component, a cool-air accessory box, an equipment cabin, a thrust block, a deceleration parachute bin and the like. The frame has a rigid structure made by welding steel tubes, and comprises a plane tripod and two columns. The cool-air system comprises an air supplying system, a release system, a brake system, a parachute opening system and a parachute throwing system. The take-off vehicle is used for the ground parking of the target drone, the ground test of engines, target drone traction, maintenance preparation and the take-off of the target drone. When the target drone runs to reach a take-off speed, a thrust pin is reliably pulled out at real time to separate the target drone and the take-off vehicle.
Description
Technical field
The utility model relates to the target drone launching apparatus, specifically is the driving that rises of a kind of target drone (UAV).
Background technology
Original target drone plays driving, in use has problems, a little less than, the rigidity unreasonable as the vehicle frame pillar construction, easily produces fatigue fracture, and the thrust pin insurance is unreliable, be prone to accident etc.Along with the improvement and the raising of target drone performance, the expansion of function of use, original driving far can not adapt to instructions for use, needs redesign development target drone to play driving.
Summary of the invention
The utility model is according to the needs of target drone serviceability, body construction and the cold gas system that plays driving redesigned, and according to the variation of control system and radio system, mobile unit has been made layout again, thereby provide an a kind of novel driving, to satisfy modern target drone instructions for use.
Technical scheme plays driving and comprises car body and cold gas system, the basis of car body is a vehicle frame, equipment compartment is housed on the vehicle frame, the wheel assembly, slide track component, thrust bearing, umbrella case and cold air accessory case etc., described vehicle frame is made of plane trigonometry frame and column, the tripod front end is installed front component, preceding slide track component is housed on the tripod intermediate member, the below is provided with equipment compartment, the tripod lower rear is equipped with thrust bearing, dress thrust pressurized strut in the thrust bearing, tripod rear portion upper fixed has column, and the aft ramp assembly is equipped with in its upper end, and the main wheel assembly is installed at place, two base angles, tripod rear end, drag parachute hook and shackle are housed on the tripod main beam, the drag parachute case is equipped with in the front lower place in the main beam, and front lower place, two is the cold air accessory case, and described cold gas system comprises air supply system, delivery system, brake system, parachute-opening and throwing umbrella system.
It is the prerequisite equipment of target drone that beneficial effect plays driving, prepares and the target drone usefulness of taking off for target drone ground run, traction, engineering.The utility model make a big improvement to original driving.1, body frame structure for automotive is reasonable in design, and the main stressed member such as the column back lower place are effectively strengthened, and has improved vehicle frame integral rigidity and intensity, has guaranteed safe in utilizationly, reliable, has prolonged service life; 2, cold gas system is rationally distributed, and working stability, reliable has been well positioned to meet the functional requirement of driving.
Description of drawings
Fig. 1-the bassinet structure sketch takes off
A Fig. 2-driving vertical view
A Fig. 3-driving rearview
The drawing explanation:
Among Fig. 1: 1-front component 2-equipment compartment 3-front wheel assembly 4-thrust bearing
5-rear wheel assembly 6-main wheel assembly 7-main beam 8-drag parachute case
9-drag parachute hook 10-shackle 11-cold air accessory case 12-pitot
Among Fig. 3: the 13-column
The specific embodiment
The existing accompanying drawings specific embodiment of the present utility model, play driving and comprise car body and cold gas system, the basis of car body is a vehicle frame, vehicle frame is the braced frame that steel pipe is welded into, and is made of plane trigonometry frame and two root posts, is welded with vertical, horizontal and oblique member on tripod and the column, the tripod front end is equipped with the front-wheel axle bed, front component 1 is installed on the axle bed, and front-wheel is a deflecting roller, is made up of shock strut, shimmy-damper, turning arm, wheel fork and front-wheel.Below, tripod middle part is an equipment compartment 2, slide track component 3 before being equipped with on the longitudinal member of middle part, and slide track component 3 belows are provided with thrust pin, insurance pressurized strut and discharge pressurized strut, in order to the position and the action of control thrust pin.Thrust bearing 4 is equipped with at the tripod rear portion, and the thrust pressurized strut is housed in the thrust bearing.Tripod rear portion top, symmetry be fixed with two root posts 13, column 13 be the ladder-shaped frame structure, and oblique fulcrum bar and back stay are arranged, and on it aft ramp assembly 5 is housed, the front and back slide track component is supported the target drone body jointly.The tripod rear end is a main beam 7, the main wheel seat is equipped with at place, two base angles, tripod rear end, main beam two ends, main wheel assembly 6 is housed on the wheel seat, main beam 7 front lower places are drag parachute case 8, drag parachute hook 9 is equipped with in the centre of main beam 7, shackle 10 is equipped with in its both sides, and the place ahead, main beam 7 two is a cold air accessory case 11, and the wheel seat of main wheel assembly is provided with pitot 12.
Described cold gas system comprises air feed, release, brake, parachute-opening and throwing umbrella system, the air supply system main element has air bottle and accumulator, the action of delivery system control insurance pressurized strut and release pressurized strut, brake system comprise a brake deviation-rectifying system and dead brake system.Fig. 4 is the some deviation-rectifying system block diagram of stopping, and when playing that driving is sliding to be run, departs from if any direction, by the some system works of stopping, realizes correction control.Fig. 5 is the system block diagram of extremely stopping, sliding race and stopping in order to the control main wheel.The used annex of cold gas system is the outsourcing finished parts, and the used pipe material of pipeline is the General Aviation hydraulic tube.
Claims (4)
1, a kind of driving, comprise car body and cold gas system, it is characterized in that car body is based on vehicle frame, equipment compartment is housed on the vehicle frame, the wheel assembly, slide track component, thrust bearing, umbrella case and cold air accessory case, described vehicle frame is made of plane trigonometry frame and column, the tripod front end is installed front component (1), preceding slide track component (3) is housed on the intermediate member, the below is provided with equipment compartment (2), thrust bearing (4) is equipped with in the tripod back lower place, thrust bearing is equipped with the thrust pressurized strut in (4), tripod rear portion upper fixed has column (13), aft ramp assembly (5) is equipped with in its upper end, main wheel assembly (6) is installed at place, two base angles, tripod rear end, and drag parachute hook (9) and hook (10) are housed on the tripod main beam (7), and drag parachute case (8) is equipped with in the front lower place in the main beam (7), front lower place, two is cold air accessory case (11), and cold gas system comprises air supply system, delivery system, brake system, parachute-opening and throwing umbrella system.
2, according to claim 1 driving is characterized in that preceding slide track component (3) below is provided with thrust pin, insurance pressurized strut and discharges pressurized strut.
3, according to claim 1 driving is characterized in that in the thrust bearing (4) the thrust pressurized strut being housed.
4, according to claim 1 driving is characterized in that brake system comprises a little the stop correction and two systems of extremely stopping.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201898854U CN201368702Y (en) | 2008-12-11 | 2008-12-11 | Take-off vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201898854U CN201368702Y (en) | 2008-12-11 | 2008-12-11 | Take-off vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201368702Y true CN201368702Y (en) | 2009-12-23 |
Family
ID=41487593
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008201898854U Expired - Lifetime CN201368702Y (en) | 2008-12-11 | 2008-12-11 | Take-off vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201368702Y (en) |
-
2008
- 2008-12-11 CN CNU2008201898854U patent/CN201368702Y/en not_active Expired - Lifetime
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11667400B2 (en) | Tram system and methods for autonomous takeoff and landing of aircraft | |
| CN202345677U (en) | Fast carrying structure used for transportation | |
| US8172017B2 (en) | Circumferential movement device | |
| KR102112475B1 (en) | Apparatus for testing air vehicle on ground | |
| CN1511759A (en) | Aeroplane rescure car | |
| US11618587B2 (en) | Ground maneuver assistance system for aircraft | |
| US20210114725A1 (en) | Composite flying vehicle | |
| CN102975722A (en) | Fast carrying structure used for transportation and uses thereof | |
| CN102849211A (en) | Variable power vertical short-distance takeoff landing aircraft with fixed wings | |
| CN205293099U (en) | Use coaxial tandem twin engine's fixed wing uavs | |
| CN203528368U (en) | 6*2 flat-head diesel car transporter | |
| CN201368702Y (en) | Take-off vehicle | |
| CN104071229A (en) | Bus frame structure of full-carrying type pure electric bus | |
| CN102717841A (en) | Tourist sightseeing bus | |
| CN107512388A (en) | A kind of the aircraft takeoffs and landings control system and method for the separation of Flight main body and undercarriage | |
| US20100102167A1 (en) | Landing wheel gear | |
| WO2003076224A2 (en) | Ducted channel wing, high-lift devices and vehicles therefor | |
| CN204196826U (en) | A kind of automobile-used solid propellant rocket protective system | |
| US20100314180A1 (en) | Mobilizing apparatus for airplanes | |
| CN207207625U (en) | Omni-directional wheel and omnidirectional's wheel assembly | |
| CN2454279Y (en) | Receiving vehicle for plane forced-landing resulted from failure of landing-gear | |
| RU2624231C1 (en) | Passenger wig aircraft | |
| CN114103570B (en) | Flying motorcycle | |
| CN204196855U (en) | A kind of automobile-used lithergol rocket protective system | |
| CN204196827U (en) | Automobile-used pulse-jet motor protective system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20091223 Effective date of abandoning: 20100329 |
|
| C20 | Patent right or utility model deemed to be abandoned or is abandoned |