CN102882159A - Wiring method for airborne cable device frame of unmanned aerial vehicle - Google Patents
Wiring method for airborne cable device frame of unmanned aerial vehicle Download PDFInfo
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- CN102882159A CN102882159A CN2012103762309A CN201210376230A CN102882159A CN 102882159 A CN102882159 A CN 102882159A CN 2012103762309 A CN2012103762309 A CN 2012103762309A CN 201210376230 A CN201210376230 A CN 201210376230A CN 102882159 A CN102882159 A CN 102882159A
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Abstract
The invention discloses a wiring method for an airborne cable device frame of an unmanned aerial vehicle. By stereoscopic space wiring, most of instrument devices and control boxes of the unmanned aerial vehicle are mounted on the double-layered device frame, the airborne cable device frame is divided into four spaces, and the spaces are connected through a cable bundle. The cable bundle of the device frame is an integral cable set and is totally provided with 34 connectors. The device frame is divided into an upper layer and a lower layer, is divided into four areas A, B,C,D from top to bottom according to a principle of heading from front to back and from left to right, coordinates are sequentially set as locating points, namely, 25 locating points, and each locating point is provided with a fixing clip used for fixing wire harness. Due to the fact that by stereoscopic space wiring process, most of the instrument devices and the control boxes of the unmanned aerial vehicle are mounted on the double-layered device frame, the airborne cable device frame has four spaces, and the spaces are effectively connected through a complete cable bundle, normal operation of devices is achieved, the method is reasonable in wiring path and process and small in space occupation, wiring is easy, and reliable flight of the unmanned aerial vehicle is guaranteed.
Description
Technical field
The present invention relates to the pilotless aircraft airborne apparatus field, particularly a kind of unmanned aerial vehicle onboard cable apparatus frame wiring method.
Background technology
Drone is called for short " unmanned plane ", is the not manned aircraft that utilizes radio robot and the presetting apparatus of providing for oneself to handle.Without driving cabin, but the equipment such as flight control computer, air data computer, vertical gyro are installed on the machine.On ground, the naval vessels or machine tool remote control station personnel by equipment such as radars, to its follow the tracks of, location, remote control, remote measurement and Digital Transmission.Can under wireless remotecontrol, as conventional airplane, take off.During recovery, can adopt the mode automatic Landing the same with the conventional airplane landing mission.But Reusability repeatedly.Be widely used in aerial reconnaissance, military force strike, supervision, communication, antisubmarine, electronic jamming etc.
The electronic equipment that carries on the unmanned aerial vehicle is various, complicated, considering needs to intercom mutually between each functional module of electronic equipment internal, the voltage cable that lays is different, and electric current is different, and frequency is different, the mutual alignment of these cables, and the position of laying all will exert an influence to the Electro Magnetic Compatibility of equipment frame integral body, and these cables connect up by equipment frame, and it is the core in all aircraft cables, its quality directly has influence on the safety of aircraft with accurate with accurate.So must reasonably classify to each cable of wire, planning must be carried out rationally effectively space layout to cable and line bundle, to guarantee the normal operation of equipment.But existing airborne cable apparatus wire structures is complicated, and required wiring frame volume is larger, is difficult for operation, therefore causes wiring cost high, and wire structures to take the unmanned plane space larger so that unmanned plane inner space utilization ratio is lower.
Summary of the invention
The object of the invention is to propose a kind of unmanned aerial vehicle onboard cable apparatus frame wiring method, solved unmanned plane equipment frame wiring complicated, cost is high, and wire structures takes up room greatly, causes the low problem of unmanned plane space availability ratio.
For reaching this purpose, the present invention by the following technical solutions:
A kind of unmanned aerial vehicle onboard cable apparatus frame wiring method adopts the solid space wiring, and the most of instrumentation of unmanned plane and control box are installed on double-deck equipment frame, is divided into four-level space, and each space connects by a whole set of bunch of cables.
Preferably, the bunch of cables of described equipment frame is whole cable set, is provided with altogether 34 connectors.
Preferably, described equipment frame is divided into two-layer up and down, is divided into from top to bottom A, B, C, four districts of D, and by the course from front to back, principle from left to right sets up coordinate points as anchor point successively.
Preferably, described anchor point is totally 25.
Preferably, described each anchor point is equipped with the fixation clamp for fixed beam.
The present invention adopts the solid space Wiring technique, the most of instrumentation of unmanned plane and control box are installed in the bi-layered device frame, altogether in the four-level space, effective connection by a whole set of bunch of cables realizes the normal operation of each equipment, and its routing path and technique are reasonable, take up room little, wiring is operation easily, the making of cable-assembly and examination is accomplished evidence-based, provides guarantee to the reliable flight of unmanned plane.
Description of drawings
Fig. 1 is the equipment frame structural representation;
Fig. 2 is that equipment frame A face anchor point arranges schematic diagram;
Fig. 3 is that equipment frame C face anchor point arranges schematic diagram;
Fig. 4 is example cable connection table;
Fig. 5 is example cable trails dendrogram.
Among the figure: 1, upper bed rack; 2, lower floor's frame.
Embodiment
Further specify technical scheme of the present invention below in conjunction with accompanying drawing and by embodiment.
Fig. 1 is the wiring frame structural representation, and equipment frame is the double-deck stereo structure, comprises upper bed rack 1 and lower floor's frame 2, every layer of two sides, and separator is A, B, C, D four districts successively from top to bottom, is total to four-level space, each space connects by a whole set of bunch of cables; The bunch of cables of whole equipment frame is the cable set that can not be split, and 34 connectors are set altogether.
Such as Fig. 2, shown in Figure 3, for A face and C areal coordinate anchor point arrange schematic diagram, every layer by the course from front to back, principle from left to right, set up successively coordinate points A1, A2 ... A11, CI, C2 ... C14, totally 25 anchor points, each anchor point is all installed the fixation clamp as the fixed cable bundle.Q1, Q2 are the cable-through hole on equipment frame among the figure.
As shown in Figure 4, be the wiring chart of part cable and connector, Z1 to Z7 represents cable number in the chart, Y1 to Y10 is the connector numbering, cable Z3 to Z6, the customization cable of mating formation successively, with each connector, press anchor point shown in the chart successively, mat formation and wait for making to point of destination.
Be illustrated in figure 5 as example cable trails dendrogram, each root cable, institute is through the path, and it is different that maximal end point is reserved the plug surplus, and it also is different that surplus is made in the reservation of each connector.Pass through successively A11 such as " Y1 " connector among the Z3 in the dendrogram, A10, A9, A8, A7, the A6 point, and reserve 200mm plug surplus, overall length 1050mm.Make surplus and reserve the different surpluses of making by the operator according to different connector." Y1 " connector comes from the cable bundle of " Z1 " and " Z2 " simultaneously in addition.Pass through successively A11 such as " Y2 " connector among the figure, A10, A9, Q1, C7, C2, and reserve 80mm plug surplus, overall length 1220mm.Q1 are cables by A face Q1 to the C face anchor point of vertically boring a hole, all the other cables the like.
Wiring method of the present invention is installed in the bi-layered device frame with the most of instrumentation of unmanned plane and control box, altogether in the four-level space, by effective connection of a whole set of bunch of cables, realize the normal operation of each equipment, its routing path and technique are reasonable, take up room little, and wiring is operation easily.
Wiring technique of the present invention adopts the Wiring technique of solid space equipment frame and the manufacture craft of cable-assembly, accomplishes evidence-basedly for the making of cable-assembly and examination, provides guarantee to the reliable flight of unmanned plane.
Claims (5)
1. a unmanned aerial vehicle onboard cable apparatus frame wiring method is characterized in that, adopts the solid space wiring, and the most of instrumentation of unmanned plane and control box are installed on double-deck equipment frame, is divided into four-level space, and each space connects by a whole set of bunch of cables.
2. a kind of unmanned aerial vehicle onboard cable apparatus frame wiring method according to claim 1 is characterized in that, the bunch of cables of described equipment frame is whole cable set, is provided with altogether 34 connectors.
3. a kind of unmanned aerial vehicle onboard cable apparatus frame wiring method according to claim 2 is characterized in that, described equipment frame is divided into two-layer up and down, be divided into from top to bottom A, B, C, four districts of D, and by the course from front to back, principle from left to right sets up coordinate points as anchor point successively.
4. a kind of unmanned aerial vehicle onboard cable apparatus frame wiring method according to claim 3 is characterized in that totally 25 of described anchor points.
5. a kind of unmanned aerial vehicle onboard cable apparatus frame wiring method according to claim 4 is characterized in that, described each anchor point is equipped with the fixation clamp for fixed beam.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012103762309A CN102882159A (en) | 2012-09-29 | 2012-09-29 | Wiring method for airborne cable device frame of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012103762309A CN102882159A (en) | 2012-09-29 | 2012-09-29 | Wiring method for airborne cable device frame of unmanned aerial vehicle |
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| CN102882159A true CN102882159A (en) | 2013-01-16 |
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| CN2012103762309A Pending CN102882159A (en) | 2012-09-29 | 2012-09-29 | Wiring method for airborne cable device frame of unmanned aerial vehicle |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103545757A (en) * | 2013-10-29 | 2014-01-29 | 北京航天易联科技发展有限公司 | Unmanned aerial vehicle cable laying method |
| CN108390325A (en) * | 2018-01-18 | 2018-08-10 | 倪惠芳 | A kind of unmanned aerial vehicle onboard cable apparatus frame |
| CN111383795A (en) * | 2020-03-09 | 2020-07-07 | 西安联飞智能装备研究院有限责任公司 | Unmanned aerial vehicle shielding cable grounding point determining method and device, cable and unmanned aerial vehicle |
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| US6974261B1 (en) * | 2003-12-22 | 2005-12-13 | Itt Manufacturing Enterprises, Inc. | Optical bonding structure |
| CN201296386Y (en) * | 2008-12-02 | 2009-08-26 | 中国电子科技集团公司第十四研究所 | Composite material light colligate device machine frame |
| CN201516793U (en) * | 2009-10-23 | 2010-06-30 | 吉林大学 | Air-ground amphibious intelligent vehicle |
| CN102381471A (en) * | 2010-09-02 | 2012-03-21 | 梦想空间世界有限公司 | Unmanned flying vehicle made with PCB |
| CN102424111A (en) * | 2012-01-06 | 2012-04-25 | 厦门大学 | Flexible saucer-shaped aircraft |
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Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6974261B1 (en) * | 2003-12-22 | 2005-12-13 | Itt Manufacturing Enterprises, Inc. | Optical bonding structure |
| CN201296386Y (en) * | 2008-12-02 | 2009-08-26 | 中国电子科技集团公司第十四研究所 | Composite material light colligate device machine frame |
| CN201516793U (en) * | 2009-10-23 | 2010-06-30 | 吉林大学 | Air-ground amphibious intelligent vehicle |
| CN102381471A (en) * | 2010-09-02 | 2012-03-21 | 梦想空间世界有限公司 | Unmanned flying vehicle made with PCB |
| CN102424111A (en) * | 2012-01-06 | 2012-04-25 | 厦门大学 | Flexible saucer-shaped aircraft |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103545757A (en) * | 2013-10-29 | 2014-01-29 | 北京航天易联科技发展有限公司 | Unmanned aerial vehicle cable laying method |
| CN108390325A (en) * | 2018-01-18 | 2018-08-10 | 倪惠芳 | A kind of unmanned aerial vehicle onboard cable apparatus frame |
| CN111383795A (en) * | 2020-03-09 | 2020-07-07 | 西安联飞智能装备研究院有限责任公司 | Unmanned aerial vehicle shielding cable grounding point determining method and device, cable and unmanned aerial vehicle |
| CN111383795B (en) * | 2020-03-09 | 2021-11-19 | 西安联飞智能装备研究院有限责任公司 | Unmanned aerial vehicle shielding cable grounding point determining method and device, cable and unmanned aerial vehicle |
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| Date | Code | Title | Description |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C53 | Correction of patent of invention or patent application | ||
| CB03 | Change of inventor or designer information |
Inventor after: Lv Chao Inventor after: Li Gang Inventor after: Xiao Aiying Inventor before: Lv Chao Inventor before: Xiao Aiying |
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| COR | Change of bibliographic data |
Free format text: CORRECT: INVENTOR; FROM: LV CHAO XIAO AIYING TO: LV CHAO LI GANG XIAO AIYING |
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| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20130116 |