CN103770951A - UAV (Unmanned Aerial Vehicle) assembling and debugging vehicle - Google Patents
UAV (Unmanned Aerial Vehicle) assembling and debugging vehicle Download PDFInfo
- Publication number
- CN103770951A CN103770951A CN201410032513.0A CN201410032513A CN103770951A CN 103770951 A CN103770951 A CN 103770951A CN 201410032513 A CN201410032513 A CN 201410032513A CN 103770951 A CN103770951 A CN 103770951A
- Authority
- CN
- China
- Prior art keywords
- chassis
- sides
- assembling
- balancing
- unmanned plane
- 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.)
- Granted
Links
Images
Landscapes
- Motorcycle And Bicycle Frame (AREA)
- Testing Of Balance (AREA)
Abstract
The invention relates to a UAV (Unmanned Aerial Vehicle) assembling and debugging vehicle which mainly comprises a chassis, a weighing disk, a balancing device, a display mechanism, support frames and lifting mechanisms. The weighing disk is arranged on the chassis; at least two pressure sensors are arranged between the chassis and the weighing disk; the T-shaped support frames are respectively arranged at the front and rear ends of the weighing disk; both sides of the upper parts of the support frames are provided with roller wheels; the chassis at both sides of the weighing disk is fixedly provided with the lifting mechanisms; each lifting mechanism is mainly formed by a motor, an electric push rod and a linear guide rail; the support frames arranged on the linear guide rails are pushed to ascend and descended by the electric push rods driven by the motors; the balancing device consists of balancing knife edges at both sides and a balancing cross bar; the balancing cross bar is fixedly arranged on supporting rods at both sides; and the balancing knife edges are symmetrically fixed at both sides of the balancing cross bar. The UAV assembling and debugging vehicle integrates each set of tool in each link of debugging, weighing, balancing and turnover of a UAV; the equipment is simple to operate, has reliable performance and is convenient to move; a work place is saved; and the UAV assembling and debugging vehicle can be suitable for the requirements for assembling and debugging of various types of UAVs.
Description
Technical field
The present invention relates to a kind of unmanned plane debugging apparatus, relate in particular to a kind of unmanned plane assembling and setting car, belong to unmanned plane rigging equipment technical field.
Background technology
At present, the unmanned plane of batch manufacturing is in fitting process because complex structure, require accurately, often debug, weigh, in balancing process, needs are repeated multiple times.Weighing and when balancing, need many people to operate simultaneously, repeated multiple timesly just can complete, inefficiency, labour intensity are large, can not meet the requirement of manufacturing schedule.For this reason, development collection is debugged, is weighed, the production tooling of balancing and shipment function integration is very necessary.
Summary of the invention
In view of the defect of above-mentioned prior art existence, the object of the invention is provides a kind of unmanned plane assembling and setting car for above-mentioned defect, by to unmanned plane debugging, weigh, each cover frock of trim and the each link of turnover integrates, make it have that equipment operating is simple, the feature of dependable performance, conveniently moving, saving work-yard, can meet the unmanned plane assembling and setting needs of Multiple Type.
For addressing the above problem, the technical solution used in the present invention is a kind of unmanned plane assembling and setting car, mainly formed by chassis, weighing pan, balancing device, indication mechanism, bracing frame and lifting mechanism, described weighing pan is arranged on described chassis, between chassis and weighing pan, be provided with at least two pressure sensors, described pressure sensor is connected by wire with the indication mechanism being arranged on chassis; Be separately installed with T shape bracing frame in the front and back end of described weighing pan, both sides, support frame as described above top are provided with running roller; On the chassis on described weighing pan both sides, be installed with lifting mechanism, described lifting mechanism is mainly made up of motor, electric pushrod and line slideway, by promoted to be arranged on the strut bar lifting on line slideway by motor-driven electric pushrod, described balancing device is made up of the both sides trim edge of a knife and trim cross bar, described trim cross bar is fixedly mounted on supported on both sides bar, and described trim edge of a knife symmetry is fixed on the both sides of trim cross bar.
The technical scheme that the present invention further limits is: aforesaid unmanned plane assembling and setting car, and described sensor is bellows pressure sensor, the upper and lower surface of described pressure sensor respectively has screw, is connected with chassis by screw with weighing pan.
Aforesaid unmanned plane assembling and setting car, described pressure sensor is provided with four altogether.
Aforesaid unmanned plane assembling and setting car, the poly-urethane rubber wheel that described running roller is locking mechanism.
Aforesaid unmanned plane assembling and setting car, the poly-urethane rubber wheel work of described locking mechanism is provided with four.
Further, aforesaid unmanned plane assembling and setting car, bottom, described chassis is provided with four road wheels.
The invention has the beneficial effects as follows: the present invention is directed to unmanned plane debugging, weigh, each cover frock of trim and the each link of turnover integrates, by debugging, weigh, balancing and loading and transporting in one, this equipment operating is simple, dependable performance, conveniently moving, saving work-yard, can be applicable to the unmanned plane assembling and setting needs of Multiple Type.Use by reality, unmanned plane can be saved operation number 1/3 with this assembling and setting car in fitting process, and completes time of setting up and also shorten 1/3, has met the requirement of manufacturing schedule.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Fig. 2 is the side schematic view of Fig. 1.
The specific embodiment
A kind of unmanned plane assembling and setting car that the present embodiment provides, as depicted in figs. 1 and 2, mainly formed by chassis 1, weighing pan 2, balancing device 12, indication mechanism 3, bracing frame 4 and lifting mechanism, bottom, chassis is provided with four road wheels 6, weighing pan 2 is arranged on chassis 1, between chassis and weighing pan, be provided with altogether four pressure sensors 5, pressure sensor is connected by wire with the indication mechanism 3 being arranged on chassis, sensor is bellows pressure sensor, the upper and lower surface of pressure sensor respectively has screw, is connected with chassis by screw with weighing pan; Be separately installed with T shape bracing frame 4 in the front and back end of weighing pan, both sides, bracing frame top are provided with the poly-urethane rubber wheel 7 of four locking mechanisms altogether; On the chassis on weighing pan both sides, be installed with lifting mechanism, lifting mechanism is mainly made up of motor, electric pushrod 8 and line slideway 9, by promoted to be arranged on the strut bar lifting on line slideway by motor-driven electric pushrod, balancing device 12 is made up of the both sides trim edge of a knife 11 and trim cross bar 10, trim cross bar is fixedly mounted on supported on both sides bar, and the trim edge of a knife 11 symmetries are fixed on the both sides of trim cross bar 10.
The principle of work of the present embodiment: opening device source switch, four polyurethane wheels that manually unmanned plane are placed in to equipment top are upper, and wing line of balance is overlapped with the trim edge of a knife, and telltale shows fuselage weight, after showing zero setting, add oil plant to required weight, complete the operation of weighing; Press " rising " button on operator's station, both sides electric pushrod drives trim bar, makes fuselage rising, and the postpone that puts in place stops and self-locking automatically; Carry out weight trim operation, after completing, press " decline " button, overall slow decreasing, it is upper that fuselage falls within polyurethane wheel, and whole flow process finishes.
In addition to the implementation, the present invention can also have other embodiments.All employings are equal to the technical scheme of replacement or equivalent transformation formation, all drop on the protection domain of requirement of the present invention.
Claims (6)
1. a unmanned plane assembling and setting car, mainly formed by chassis, weighing pan, balancing device, indication mechanism, bracing frame and lifting mechanism, it is characterized in that: described weighing pan is arranged on described chassis, between chassis and weighing pan, be provided with at least two pressure sensors, described pressure sensor is connected by wire with the indication mechanism being arranged on chassis; Be separately installed with T shape bracing frame in the front and back end of described weighing pan, both sides, support frame as described above top are provided with running roller; On the chassis on described weighing pan both sides, be installed with lifting mechanism, described lifting mechanism is mainly made up of motor, electric pushrod and line slideway, by promoted to be arranged on the strut bar lifting on line slideway by motor-driven electric pushrod, described balancing device is made up of the both sides trim edge of a knife and trim cross bar, described trim cross bar is fixedly mounted on supported on both sides bar, and described trim edge of a knife symmetry is fixed on the both sides of trim cross bar.
2. unmanned plane assembling and setting car according to claim 1, is characterized in that: described sensor is bellows pressure sensor, and the upper and lower surface of described pressure sensor respectively has screw, is connected with chassis by screw with weighing pan.
3. unmanned plane assembling and setting car according to claim 2, is characterized in that: described pressure sensor is provided with four altogether.
4. unmanned plane assembling and setting car according to claim 1, is characterized in that: the poly-urethane rubber wheel that described running roller is locking mechanism.
5. unmanned plane assembling and setting car according to claim 1, is characterized in that: the poly-urethane rubber wheel work of described locking mechanism is provided with four.
6. unmanned plane assembling and setting car according to claim 1, is characterized in that: bottom, described chassis is provided with four road wheels.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410032513.0A CN103770951B (en) | 2014-01-23 | 2014-01-23 | A kind of unmanned plane assembling and setting car |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410032513.0A CN103770951B (en) | 2014-01-23 | 2014-01-23 | A kind of unmanned plane assembling and setting car |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103770951A true CN103770951A (en) | 2014-05-07 |
| CN103770951B CN103770951B (en) | 2016-04-13 |
Family
ID=50563823
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410032513.0A Active CN103770951B (en) | 2014-01-23 | 2014-01-23 | A kind of unmanned plane assembling and setting car |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103770951B (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105059719A (en) * | 2015-07-30 | 2015-11-18 | 西安爱生技术集团公司 | Internal structure of packaging container for small unmanned aerial vehicle |
| CN106081119A (en) * | 2016-07-07 | 2016-11-09 | 广州飞机维修工程有限公司 | A kind of aircraft balanced counterweight handling system |
| CN106314823A (en) * | 2016-11-30 | 2017-01-11 | 江西洪都航空工业集团有限责任公司 | Auxiliary support device for aircraft tail compartment |
| CN106828962A (en) * | 2016-12-27 | 2017-06-13 | 航天神舟飞行器有限公司 | Rocket assist formula high-speed unmanned aerial vehicle trigger mechanism |
| CN107199554A (en) * | 2017-07-27 | 2017-09-26 | 孟凡星 | A kind of unmanned plane Fast-Maintenance debugging machine people |
| CN108516102A (en) * | 2018-04-28 | 2018-09-11 | 中电科芜湖钻石飞机制造有限公司 | Flexible universal aircraft supporting tool |
| CN108516103A (en) * | 2018-05-22 | 2018-09-11 | 东汉太阳能无人机技术有限公司 | Unmanned plane during flying angle balancing device and its Calculate Ways |
| CN112623274A (en) * | 2021-01-18 | 2021-04-09 | 陆颖怡 | Unmanned aerial vehicle flight angle balancing unit |
| CN114770079A (en) * | 2022-06-17 | 2022-07-22 | 四川腾盾科技有限公司 | Non-hoisting type disassembling and assembling method for medium and large unmanned aerial vehicle |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5587900A (en) * | 1995-05-23 | 1996-12-24 | Northrop Grumman Corporation | Self leveling independently programmable system |
| CN101028870A (en) * | 2007-04-12 | 2007-09-05 | 沈阳飞机工业（集团）有限公司 | Method for digitally assembling spatial composite angle positioner tool |
| CN101506039A (en) * | 2005-10-05 | 2009-08-12 | 贝尔直升机泰克斯特龙公司 | Integrated aircraft scale and leveling apparatus and methods for use |
| CN102001451A (en) * | 2010-11-12 | 2011-04-06 | 浙江大学 | Airplane component attitude adjusting and butting system based on four numeric control positioners, attitude adjusting platform and mobile bracket and corresponding method |
| CN102009340A (en) * | 2010-09-07 | 2011-04-13 | 成都立航科技有限公司 | Aircraft engine mounting vehicle |
| CN102582844A (en) * | 2011-12-30 | 2012-07-18 | 衡阳泰豪通信车辆有限公司 | Fixation and protection pulley for disassembly, assembly, transhipment and vehicle-mounted transport of wings |
| CN103204249A (en) * | 2013-03-25 | 2013-07-17 | 大连理工大学 | Multi-shaft posture adjusting platform for airplane engine mounting |
-
2014
- 2014-01-23 CN CN201410032513.0A patent/CN103770951B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5587900A (en) * | 1995-05-23 | 1996-12-24 | Northrop Grumman Corporation | Self leveling independently programmable system |
| CN101506039A (en) * | 2005-10-05 | 2009-08-12 | 贝尔直升机泰克斯特龙公司 | Integrated aircraft scale and leveling apparatus and methods for use |
| CN101028870A (en) * | 2007-04-12 | 2007-09-05 | 沈阳飞机工业（集团）有限公司 | Method for digitally assembling spatial composite angle positioner tool |
| CN102009340A (en) * | 2010-09-07 | 2011-04-13 | 成都立航科技有限公司 | Aircraft engine mounting vehicle |
| CN102001451A (en) * | 2010-11-12 | 2011-04-06 | 浙江大学 | Airplane component attitude adjusting and butting system based on four numeric control positioners, attitude adjusting platform and mobile bracket and corresponding method |
| CN102582844A (en) * | 2011-12-30 | 2012-07-18 | 衡阳泰豪通信车辆有限公司 | Fixation and protection pulley for disassembly, assembly, transhipment and vehicle-mounted transport of wings |
| CN103204249A (en) * | 2013-03-25 | 2013-07-17 | 大连理工大学 | Multi-shaft posture adjusting platform for airplane engine mounting |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105059719B (en) * | 2015-07-30 | 2017-08-29 | 西安爱生技术集团公司 | A kind of SUAV packing case internal structure |
| CN105059719A (en) * | 2015-07-30 | 2015-11-18 | 西安爱生技术集团公司 | Internal structure of packaging container for small unmanned aerial vehicle |
| CN106081119A (en) * | 2016-07-07 | 2016-11-09 | 广州飞机维修工程有限公司 | A kind of aircraft balanced counterweight handling system |
| CN106314823B (en) * | 2016-11-30 | 2018-12-25 | 江西洪都航空工业集团有限责任公司 | A kind of auxiliary support apparatus for aircraft deck store |
| CN106314823A (en) * | 2016-11-30 | 2017-01-11 | 江西洪都航空工业集团有限责任公司 | Auxiliary support device for aircraft tail compartment |
| CN106828962A (en) * | 2016-12-27 | 2017-06-13 | 航天神舟飞行器有限公司 | Rocket assist formula high-speed unmanned aerial vehicle trigger mechanism |
| CN107199554A (en) * | 2017-07-27 | 2017-09-26 | 孟凡星 | A kind of unmanned plane Fast-Maintenance debugging machine people |
| CN108516102A (en) * | 2018-04-28 | 2018-09-11 | 中电科芜湖钻石飞机制造有限公司 | Flexible universal aircraft supporting tool |
| CN108516102B (en) * | 2018-04-28 | 2023-09-26 | 中电科芜湖钻石飞机制造有限公司 | Flexible general aircraft support tool |
| CN108516103A (en) * | 2018-05-22 | 2018-09-11 | 东汉太阳能无人机技术有限公司 | Unmanned plane during flying angle balancing device and its Calculate Ways |
| CN112623274A (en) * | 2021-01-18 | 2021-04-09 | 陆颖怡 | Unmanned aerial vehicle flight angle balancing unit |
| CN112623274B (en) * | 2021-01-18 | 2023-09-01 | 福建海狮集团有限公司 | Unmanned aerial vehicle flight angle balancing device |
| CN114770079A (en) * | 2022-06-17 | 2022-07-22 | 四川腾盾科技有限公司 | Non-hoisting type disassembling and assembling method for medium and large unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103770951B (en) | 2016-04-13 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103770951A (en) | UAV (Unmanned Aerial Vehicle) assembling and debugging vehicle | |
| CN203667917U (en) | Lifting and sliding device of automobile test bench | |
| CN108082531B (en) | Reconfigurable aircraft wall plate assembling device | |
| CN206344050U (en) | One kind miniaturization spatial locator device | |
| CN205103212U (en) | Automatic nondestructive test device of aircraft wheel wheel hub normal position | |
| CN102785236B (en) | Multifunctional mounting and dismounting vehicle for aircraft landing gear | |
| CN204197308U (en) | A kind of flexible apparatus to the assembling of aircraft housing | |
| CN110549729B (en) | Car sun visor board label thermoprint equipment | |
| CN203391888U (en) | Variable-pitch material collecting and conveying robot | |
| CN103376220B (en) | Composite material C-type beam deflection and distortion detection and prestress application experiment table | |
| CN207118736U (en) | A kind of Aero-Space dining car expanded surface area device | |
| CN206804019U (en) | A kind of unmanned plane debugs platform | |
| CN204674820U (en) | A kind of manual operation of landing gear | |
| CN204324148U (en) | A kind of stereo warehouse formula dyestuff weighing machine | |
| CN208630875U (en) | VTOL fixed-wing unmanned plane iron bird testing stand | |
| CN203581020U (en) | Laminar vehicle with horizontal docking mechanism | |
| CN208254628U (en) | Bridge platform weighing system and aerial work platform | |
| CN209453104U (en) | A kind of pressurizing device and compression system of short floor car bogie | |
| CN210416107U (en) | Full-automatic tire assembly line | |
| CN208422167U (en) | It is a kind of for testing the teaching experiment platform of unmanned plane sensor | |
| CN206344740U (en) | A kind of Multifunctional navigation engine transfering car | |
| CN202728274U (en) | Multifunctional test car for maintaining relaying protection device | |
| CN111806691A (en) | Special anticollision locking logistics distribution unmanned aerial vehicle of transportation based on automatic control | |
| CN108100293B (en) | Method for dismounting main undercarriage of airbus A330 aircraft | |
| CN213136575U (en) | Mounting platform for component assembly |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |