CN209606459U - Unmanned plane pitot with fast assembling-disassembling function - Google Patents
Unmanned plane pitot with fast assembling-disassembling function Download PDFInfo
- Publication number
- CN209606459U CN209606459U CN201920526497.9U CN201920526497U CN209606459U CN 209606459 U CN209606459 U CN 209606459U CN 201920526497 U CN201920526497 U CN 201920526497U CN 209606459 U CN209606459 U CN 209606459U
- Authority
- CN
- China
- Prior art keywords
- pitot
- fixing seat
- quick release
- connecting conduit
- 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.)
- Expired - Fee Related
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- Laying Of Electric Cables Or Lines Outside (AREA)
Abstract
The utility model discloses a kind of unmanned plane pitot with fast assembling-disassembling function, including Quick Release pitot, pitot fixing seat and connecting conduit, the Quick Release pitot, pitot fixing seat and connecting conduit are sequentially communicated；The Quick Release pitot is connected through a screw thread with pitot fixing seat；The pitot fixing seat and connecting conduit are clamped by male and female head.The utility model has the beneficial effects that existing pitot has been designed to two pieces, and by the way of screw threads for fastening, quick release pitot; greatly protect the safety of pitot; after pitot disassembly, pitot leading portion the space occupied can be subtracted, for transport saving cost.
Description
Technical field
The utility model, which belongs to, is related to unmanned plane field, especially a kind of unmanned plane air speed with fast assembling-disassembling function
Pipe.
Background technique
In recent years, VTOL Fixed Wing AirVehicle is gradually approved by market, is now widely used for mapping, logistics etc.
Field.Aircraft body head, machine are embedded in currently, being commonly on the market for the pitot of VTOL Fixed Wing AirVehicle
The outer surfaces such as wing forward position, be easy to appear in transition transportational process external force operation lead to its bending at pitot, fracture etc. it is broken
It is bad, so that this job task be caused to fail.
Utility model content
Technical problem to be solved in the utility model is, by the way of screw threads for fastening, quick release pitot, and pole
The big safety for protecting pitot.
To solve the above problems, the technical solution of the utility model is: the unmanned plane air speed with fast assembling-disassembling function
Pipe, including Quick Release pitot, pitot fixing seat and connecting conduit, the Quick Release pitot, pitot fixing seat and connection are led
Pipe is sequentially communicated；The Quick Release pitot is connected through a screw thread with pitot fixing seat；The pitot fixing seat and connection are led
Pipe is clamped by male and female head.
Further, one end that the pitot fixing seat is connect with connecting conduit is provided with hierarchic structure, the ladder
The clamping of the inner wall of structure and connecting conduit.
Further, the one end of the Quick Release pitot not with pitot fixing seat connection is provided with ladder mouth.
The utility model has the beneficial effects that existing pitot has been designed to two pieces, it, can by the way of screw threads for fastening
Fast quick-detach pitot greatly protects the safety of pitot, and after pitot disassembly, pitot leading portion the space occupied can be with
It subtracts, for transport saving cost.
Detailed description of the invention
Fig. 1 is pitot fast assembling disassembling structure figure；
Fig. 2 is pitot fast assembling disassembling structure explosive view；
Fig. 3 is pitot fast assembling disassembling structure cross-sectional view.
Specific embodiment
The utility model is further elaborated with specific embodiment with reference to the accompanying drawing.
As shown in Figure 1-3, the unmanned plane pitot with fast assembling-disassembling function, including Quick Release pitot 1, pitot are solid
Reservation 2 and connecting conduit 3, the Quick Release pitot 1, pitot fixing seat 2 and connecting conduit 3 are sequentially communicated；The Quick Release is empty
Fast pipe 1 is connected through a screw thread with pitot fixing seat 2；The pitot fixing seat 2 and connecting conduit 3 are clamped by male and female head.
One end that the pitot fixing seat 2 is connect with connecting conduit 3 is provided with hierarchic structure 6, the hierarchic structure 6 with
The inner wall of connecting conduit 3 is clamped.The one end of the Quick Release pitot 1 not with 2 connection of pitot fixing seat is provided with ladder mouth 4.
Existing pitot has been designed to two pieces and has realized that fast quick-detach and fastening connect by way of screw thread 5 by us
It connects.Pitot fixing seat 2 and connecting conduit 3 are clamped by hierarchic structure 6 by male and female head, the hierarchic structure 6 and connecting conduit 3
Inner wall clamping realize with the sealing of connecting conduit 3, so that it is guaranteed that air speed information is accurate.
Pitot has been designed to detachable structure by my the application, can be kept separately to have saved the space of transport
And cost.
Those of ordinary skill in the art will understand that the embodiments described herein, which is to help reader, understands this reality
With novel principle, it should be understood that the scope of the present invention is not limited to such specific embodiments and embodiments.
Those skilled in the art can be made according to the technical disclosures disclosed by the utility model it is various do not depart from it is practical
Novel substantive various other specific variations and combinations, these variations and combinations are still within the protection scope of the present invention.
Claims (3)
1. the unmanned plane pitot with fast assembling-disassembling function, it is characterised in that: solid including Quick Release pitot (1), pitot
Reservation (2) and connecting conduit (3), the Quick Release pitot (1), pitot fixing seat (2) and connecting conduit (3) are sequentially communicated；
The Quick Release pitot (1) is connected through a screw thread with pitot fixing seat (2)；The pitot fixing seat (2) and connecting conduit
(3) it is clamped by male and female head.
2. the unmanned plane pitot according to claim 1 with fast assembling-disassembling function, it is characterised in that: the air speed
One end that pipe fixing seat (2) is connect with connecting conduit (3) is provided with hierarchic structure (6), the hierarchic structure (6) and connecting conduit
(3) inner wall clamping.
3. the unmanned plane pitot according to claim 1 with fast assembling-disassembling function, it is characterised in that: the Quick Release
The one end of pitot (1) not with pitot fixing seat (2) connection is provided with ladder mouth (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920526497.9U CN209606459U (en) | 2019-04-16 | 2019-04-16 | Unmanned plane pitot with fast assembling-disassembling function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920526497.9U CN209606459U (en) | 2019-04-16 | 2019-04-16 | Unmanned plane pitot with fast assembling-disassembling function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209606459U true CN209606459U (en) | 2019-11-08 |
Family
ID=68405915
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920526497.9U Expired - Fee Related CN209606459U (en) | 2019-04-16 | 2019-04-16 | Unmanned plane pitot with fast assembling-disassembling function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209606459U (en) |
-
2019
- 2019-04-16 CN CN201920526497.9U patent/CN209606459U/en not_active Expired - Fee Related
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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: 20191108 Termination date: 20210416 |