Foot stool structure of air vehicle and air vehicle

An aircraft and tripod technology, applied in the field of aircraft, can solve problems such as aircraft damage and aircraft crash, achieve the effect of good support and balance, and simplify user operations

Active Publication Date: 2016-05-04
XIAOMI INC +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, the application environment of the aircraft may have adverse factors such as stagnant water and silt. If the fuselage of the aircraft is directly placed in the corresponding environment for take-off or landing, it may cause damage to the aircraft; at the same time, if the user has insufficient control experience, it may Cause the aircraft to crash when it lands on a hard ground

Method used

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  • Foot stool structure of air vehicle and air vehicle
  • Foot stool structure of air vehicle and air vehicle
  • Foot stool structure of air vehicle and air vehicle

Examples

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Embodiment Construction

[0037] Reference will now be made in detail to the exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, the same numerals in different drawings refer to the same or similar elements unless otherwise indicated. The implementations described in the following exemplary examples do not represent all implementations consistent with the present disclosure. Rather, they are merely examples of apparatuses and methods consistent with aspects of the present disclosure as recited in the appended claims.

[0038] figure 1 is a three-dimensional structure diagram of an aircraft in a working mode according to an exemplary embodiment, as shown in figure 1 As shown, the present disclosure configures a tripod structure 2 under the fuselage 1 of the aircraft. On the one hand, it can provide support during the take-off and landing phase of the aircraft, so that the fuselage 1 of the aircraft i...

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Abstract

The invention relates to a fool stool structure of an air vehicle and the air vehicle. The foot stool structure comprises connecting supports, a plurality of foot stools, and a fixing part, wherein the connecting supports are installed at the bottom of a vehicle body of the air vehicle; each foot stool is connected with the corresponding connecting support in the preset direction so that the foot stool can be connected to the vehicle body of the air vehicle; each foot stool can rotate around the axis of the preset direction so as to be switched between a storing mode of a first preset angle and a working mode of a second preset angle; the fixing part is installed in the position of the vehicle body of the air vehicle; when the fixing part is in the first posture, rotation operation of the foot stools in the working mode can be limited; when the fixing part is in the second posture, the rotation limitation on the foot stools can be cancelled, so that the fool stools are switched from the working mode to the storing mode. By the adoption of the technical scheme, using and storage of the foot stools of the air vehicle can be achieved easily.

Description

technical field [0001] The present disclosure relates to the technical field of aircraft, in particular to an aircraft stand structure and the aircraft. Background technique [0002] At present, unmanned aerial vehicles such as quadcopters and octocopters have been widely used in various fields such as aerial photography and search and rescue due to their simple operation and stable performance, and they are increasingly playing an important role. [0003] However, the application environment of the aircraft may have adverse factors such as stagnant water and silt. If the fuselage of the aircraft is directly placed in the corresponding environment for take-off or landing, it may cause damage to the aircraft; at the same time, if the user has insufficient control experience, it may Cause the aircraft to crash when it lands on a hard ground. Contents of the invention [0004] The disclosure provides an aircraft stand structure and the aircraft to solve the deficiencies in t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/12B64C25/18B64C25/32
CPCB64C25/12B64C25/18B64C25/32
Inventor 车建明蔡炜贺孟华叶华林
Owner XIAOMI INC
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