CN210793680U - Structure for improving maintainability of speed sensor - Google Patents
Structure for improving maintainability of speed sensor Download PDFInfo
- Publication number
- CN210793680U CN210793680U CN201920966113.5U CN201920966113U CN210793680U CN 210793680 U CN210793680 U CN 210793680U CN 201920966113 U CN201920966113 U CN 201920966113U CN 210793680 U CN210793680 U CN 210793680U
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- China
- Prior art keywords
- cable
- plug
- socket
- speed sensor
- maintainability
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Abstract
The utility model discloses an improve structure of speedtransmitter maintainability, including response subassembly, cable, plug, socket, flight control computer, the response subassembly sets up in the wheel, and plug one end is connected with response subassembly, and the other end is connected with the socket, and cable one end is connected with the socket, and the other end is connected with the flight control computer, the utility model discloses a with plug direct mount on the response subassembly, pass the undercarriage axle hole with the cable and connect on the flight control computer to it is fixed through socket and product plug connection, when avoiding the dismouting product, need get rid of the clamp of fixed cable on the undercarriage earlier, improve product maintainability with the loaded down with trivial details process that cable and plug were taken out from undercarriage axle hole again.
Description
Technical Field
The utility model relates to an aircraft braking system technical field especially relates to a structure of improvement speedtransmitter maintainability.
Background
At present, speed sensor has wide application in unmanned aerial vehicle braking system, along with the needs of combat readiness, and to product reliability, maintainability, the requirement of guarantee nature constantly improve, current product structure can not satisfy the user demand yet. According to the actual use, the installation and the disassembly of the product, the structure of the product is improved, the maintainability of the product is improved, and the maintenance time is shortened.
SUMMERY OF THE UTILITY MODEL
Utility model purpose: the utility model provides a structure of improvement speed sensor maintainability, when can avoiding the dismouting product, need get rid of the clamp of fixed cable on the undercarriage earlier, the loaded down with trivial details process of taking out cable and plug from undercarriage axle hole improves product maintainability again.
The technical scheme is as follows:
a structure for improving maintainability of a speed sensor comprises a sensing assembly, a cable, a plug, a socket and a flight control computer, wherein the sensing assembly is arranged in a airplane wheel, one end of the plug is connected with the sensing assembly, the other end of the plug is connected with the socket, one end of the cable is connected with the socket, and the other end of the cable is connected with the flight control computer.
One end of the cable is connected with the socket, and the other end of the cable penetrates through an inner hole of the landing gear shaft to be connected with the flight control computer.
The plug is detachably connected with the socket.
The maximum external dimension of the plug is 15mm, and is 5mm smaller than the inner hole of the falling frame shaft.
The maximum external dimension of the socket is 5mm smaller than the inner hole of the falling frame shaft.
The cable length is 2500 mm.
Has the advantages that: the utility model provides an improve structure of speedtransmitter maintainability, through with plug direct mount on the response subassembly, pass the cable and rise and fall a frame hub connection on flying to control the computer to it is fixed with product plug connection through the socket, when avoiding the dismouting product, need get rid of the clamp of fixed cable on the undercarriage earlier, the loaded down with trivial details process of taking out cable and plug from rise and fall a frame hub connection again improves product maintainability.
Drawings
FIG. 1 is a schematic view of the connection structure of the present invention;
wherein: 1. the device comprises a sensing component, 2, a cable, 3, a plug, 4, a socket, 5, a flight control computer, 6, an airplane wheel, 7 and a landing gear shaft inner hole.
Detailed Description
It is right to combine the attached drawing below the utility model makes further introduction, a improve structure of speedtransmitter maintainability, including response subassembly 1, cable 2, plug 3, socket 4, flight control computer 5, response subassembly 1 set up in wheel 6, 3 one end of plug be connected with response subassembly 1, the other end is connected with socket 4, 2 one end of cable be connected with socket 4, the other end with fly control computer 5 and be connected.
One end of the cable 2 is connected with the socket 3, and the other end of the cable penetrates through an inner hole 7 of the landing gear shaft to be connected with the flight control computer 5.
The plug 3 and the socket 4 are detachably connected, and are convenient to install and detach.
The maximum external dimension of the plug 3 is 5mm smaller than that of the inner hole 7 of the landing gear shaft, so that the plug 3 can smoothly pass through the inner hole 7 of the landing gear shaft, in the patent, the maximum dimension of the plug 3 is 15mm, the inner diameter of the inner hole 7 of the landing gear shaft is about 19-20 mm, and the plug is provided with a right-angle turn.
The maximum external dimension of the socket 4 is 5mm smaller than that of the inner hole 7 of the landing gear shaft, so that the socket can smoothly pass through the inner hole 7 of the landing gear shaft.
The length of the cable 2 is 2500 mm.
The utility model discloses a with plug 3 direct mount on response subassembly 1, pass undercarriage axle hole 7 with cable 2 and connect on flying to control computer 5 to be connected fixedly through socket 4 and plug 3, when avoiding the dismouting product, need get rid of the clamp of fixed cable on the undercarriage earlier, the loaded down with trivial details process of taking cable 2 and plug 3 out from undercarriage axle hole 7 again improves product maintainability.
The above embodiments are only for illustrating the technical conception and features of the present invention, and the purpose thereof is to enable those skilled in the art to understand the contents of the present invention and to implement the same, so as not to limit the protection scope of the present invention, and all the equivalent changes or modifications made according to the spirit of the present invention should be covered in the protection scope of the present invention.
Claims (8)
1. The utility model provides an improve structure of speed sensor maintainability which characterized in that: the flight control device comprises a sensing assembly (1), a cable (2), a plug (3), a socket (4) and a flight control computer (5), wherein one end of the plug (3) is connected with the sensing assembly (1), the other end of the plug is connected with the socket (4), one end of the cable (2) is connected with the socket (4), and the other end of the cable is connected with the flight control computer (5).
2. The structure for improving maintainability of a speed sensor according to claim 1, wherein: one end of the cable (2) is connected with the socket (4), and the other end of the cable penetrates through an inner hole (7) of the landing gear shaft to be connected with the flight control computer (5).
3. The structure for improving maintainability of a speed sensor according to claim 1, wherein: the plug (3) is detachably connected with the socket (4).
4. The structure for improving maintainability of a speed sensor according to claim 1, wherein: the induction assembly (1) is arranged in the wheel (6).
5. The structure for improving maintainability of a speed sensor according to claim 1, wherein: the maximum external dimension of the plug (3) is 5mm smaller than that of the inner hole (7) of the drop frame shaft.
6. The structure for improving maintainability of a speed sensor according to claim 1, wherein: the maximum external dimension of the socket (4) is 5mm smaller than that of the inner hole (7) of the drop frame shaft.
7. The structure for improving maintainability of a speed sensor according to claim 1, wherein: the length of the cable (2) is 2500 mm.
8. The structure for improving maintainability of a speed sensor according to claim 1, wherein: the maximum external dimension of the plug (3) is 15 mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920966113.5U CN210793680U (en) | 2019-06-24 | 2019-06-24 | Structure for improving maintainability of speed sensor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920966113.5U CN210793680U (en) | 2019-06-24 | 2019-06-24 | Structure for improving maintainability of speed sensor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210793680U true CN210793680U (en) | 2020-06-19 |
Family
ID=71247272
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920966113.5U Expired - Fee Related CN210793680U (en) | 2019-06-24 | 2019-06-24 | Structure for improving maintainability of speed sensor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210793680U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110341982A (en) * | 2019-06-24 | 2019-10-18 | 贵州新安航空机械有限责任公司 | A kind of structure improving velocity sensor maintainability |
-
2019
- 2019-06-24 CN CN201920966113.5U patent/CN210793680U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110341982A (en) * | 2019-06-24 | 2019-10-18 | 贵州新安航空机械有限责任公司 | A kind of structure improving velocity sensor maintainability |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200619 |