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CN-224225316-U - Unmanned aerial vehicle airspeed tube storage structure and unmanned aerial vehicle

CN224225316UCN 224225316 UCN224225316 UCN 224225316UCN-224225316-U

Abstract

The application provides an unmanned aerial vehicle airspeed tube containing structure and an unmanned aerial vehicle, wherein the unmanned aerial vehicle airspeed tube containing structure comprises an airspeed tube, a first elastic hose and a second elastic hose, wherein the first end of the airspeed tube is connected with the unmanned aerial vehicle body through a fixing seat, the first end of the first elastic hose is connected with the first end of the airspeed tube, the second end of the first elastic hose is connected with the unmanned aerial vehicle body, the first end of the airspeed tube is movably inserted into the fixing seat, so that the unmanned aerial vehicle airspeed tube has a working position and a containing position, when the airspeed tube is in the working position, the first end of the airspeed tube is in interference fit with the fixing seat and horizontally faces, and when the airspeed tube is in the containing position, the airspeed tube is separated from the fixing seat and bends downwards. The unmanned aerial vehicle airspeed tube containing structure can retract the airspeed tube to the containing position, so that the airspeed tube is close to the unmanned aerial vehicle body, the occupied space of the airspeed tube self structure is reduced, and the size of the unmanned aerial vehicle in the containing or carrying process is reduced.

Inventors

  • Request for anonymity
  • Request for anonymity

Assignees

  • 锐川机器人(深圳)有限公司

Dates

Publication Date
20260512
Application Date
20250526

Claims (10)

  1. 1. Unmanned aerial vehicle airspeed tube accomodates structure, a serial communication port includes: The first end of the airspeed tube is connected with the unmanned aerial vehicle body through the fixing seat; The first end of the first elastic hose is connected with the first end of the airspeed tube, and the second end of the first elastic hose is connected with the unmanned aerial vehicle body; the first end of the airspeed tube is movably inserted into the fixed seat, so that the airspeed tube has a working position and a storage position, when the airspeed tube is in the working position, the first end of the airspeed tube is in interference fit with the fixed seat and horizontally faces the fixed seat, and when the airspeed tube is in the storage position, the airspeed tube is separated from the fixed seat and bends downwards.
  2. 2. The unmanned aerial vehicle pitot tube storage structure of claim 1, wherein the first end of the pitot tube is provided with a first spacing tab, and the first end of the first flexible hose is tightened and connected to the first spacing tab.
  3. 3. The unmanned aerial vehicle airspeed head storage structure according to claim 2, wherein a first guide inclined plane is arranged on the inner peripheral side wall of the fixing seat, and a first matching surface matched with the first guide inclined plane is arranged on the first limit protruding part.
  4. 4. The unmanned aerial vehicle airspeed tube storage structure of claim 1, wherein a limiting boss is arranged on the inner peripheral side wall of the fixing seat, and the airspeed tube is in limiting fit with the limiting boss.
  5. 5. The unmanned aerial vehicle pitot tube receiving structure of claim 3, further comprising an adapter and an adapter tube; The adapter is used for being fixedly connected with the unmanned aerial vehicle body; The first end of the switching tube is inserted into the switching seat, and the second end of the first elastic hose is connected with the first end of the switching tube.
  6. 6. The unmanned aerial vehicle pitot tube storage structure of claim 5, wherein the first end of the adapter tube is provided with a second spacing tab, and the second end of the first flexible hose is tightened and connected to the second spacing tab.
  7. 7. The unmanned aerial vehicle airspeed tube storage structure of claim 6, wherein a second guide inclined plane is arranged on the inner peripheral side wall of the adapter seat, and a second matching surface matched with the second guide inclined plane is arranged on the second limit convex part; Wherein the first guide inclined plane and the second guide inclined plane are opposite in inclination direction.
  8. 8. The unmanned aerial vehicle pitot tube receiving structure of claim 5, further comprising a second flexible hose; The first end of the second elastic hose is connected with the second end of the transfer tube, and the second end of the second elastic hose is used for being connected with the airspeed plate on the unmanned aerial vehicle body.
  9. 9. The unmanned aerial vehicle pitot tube of claim 8, wherein the second end of the transfer tube is provided with a third limit protrusion, and the first end of the second flexible hose is tightened to connect to the third limit protrusion.
  10. 10. An unmanned aerial vehicle comprising an unmanned aerial vehicle pitot tube receiving structure as claimed in any one of claims 1 to 9.

Description

Unmanned aerial vehicle airspeed tube storage structure and unmanned aerial vehicle Technical Field The application relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle airspeed tube storage structure and an unmanned aerial vehicle. Background Existing unmanned aerial vehicles are generally loaded with airspeed tubes for measuring the total and static pressures of the airflow in the unmanned aerial vehicle's flight to determine the airflow rate. Pitot tubes are typically mounted on the nose portion of the unmanned aerial vehicle, and pitot tubes of the prior art are typically simply affixed to the unmanned aerial vehicle. However, because the pitot tube has a certain length, the pitot tube is easily crushed during packaging and transportation, and occupies a considerable portion of the packaging space. In view of the above, it is important to provide an unmanned aerial vehicle airspeed tube accommodating structure and an unmanned aerial vehicle capable of being accommodated for packaging and transportation. Disclosure of utility model In order to solve the technical problems, the application provides an unmanned aerial vehicle airspeed tube storage structure and an unmanned aerial vehicle. According to a first aspect of the present application, there is provided an unmanned aerial vehicle airspeed tube housing structure, comprising: The first end of the airspeed tube is connected with the unmanned aerial vehicle body through the fixing seat; The first end of the first elastic hose is connected with the first end of the airspeed tube, and the second end of the first elastic hose is connected with the unmanned aerial vehicle body; the first end of the airspeed tube is movably inserted into the fixed seat, so that the airspeed tube has a working position and a storage position, when the airspeed tube is in the working position, the first end of the airspeed tube is in interference fit with the fixed seat and horizontally faces the fixed seat, and when the airspeed tube is in the storage position, the airspeed tube is separated from the fixed seat and bends downwards. Preferably, the first end of the airspeed tube is provided with a first limit protrusion, and the first end of the first elastic hose is tightly connected to the first limit protrusion. Preferably, a first guide inclined plane is arranged on the inner peripheral side wall of the fixing seat, and a first matching surface matched with the first guide inclined plane is arranged on the first limit protruding part. Preferably, a limiting boss is arranged on the inner peripheral side wall of the fixing seat, and the airspeed tube is in limiting fit with the limiting boss. Preferably, the device further comprises an adapter seat and an adapter tube; The adapter is used for being fixedly connected with the unmanned aerial vehicle body; The first end of the switching tube is inserted into the switching seat, and the second end of the first elastic hose is connected with the first end of the switching tube. Preferably, the first end of the adapter tube is provided with a second limit protrusion, and the second end of the second elastic hose is tightly connected to the second limit protrusion. Preferably, a second guide inclined plane is arranged on the inner peripheral side wall of the adapter seat, and a second matching surface matched with the second guide inclined plane is arranged on the second limit protruding part; Wherein the first guide inclined plane and the second guide inclined plane are opposite in inclination direction. Preferably, the device further comprises a second elastic hose; The first end of the second elastic hose is connected with the second end of the transfer tube, and the second end of the second elastic hose is used for being connected with the airspeed plate on the unmanned aerial vehicle body. Preferably, the second end of the transfer tube is provided with a third limit protrusion, and the first end of the second elastic hose is tightly connected to the third limit protrusion. According to a second aspect of the present application, there is provided an unmanned aerial vehicle, comprising an unmanned aerial vehicle pitot tube housing structure as described above. Compared with the prior art, the application has the beneficial effects that: The utility model provides an increase is connected first elastic hose on the pitot tube to the pitot tube passes through the fixing base installation fixedly, and under the unmanned aerial vehicle at the state of use, makes pitot tube and fixing base interference fit, and the pitot tube carries out gas velocity measurement at working position, when unmanned aerial vehicle needs to accomodate or pack the transportation, outwards draws the pitot tube, makes the pitot tube break away from the fixing base, and is in the storage position with the help of the elasticity of first elastic hose, makes the pitot tube withdraw to the region of pressing