Aircraft tripod locking device and aircraft
A locking device and aircraft technology, which is applied in the field of aircraft, can solve problems such as easy vibration of the tripod, and achieve the effect of preventing vibration and ensuring quality
Active Publication Date: 2020-06-30
POWERVISION ROBOT INC
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- Abstract
- Description
- Claims
- Application Information
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Problems solved by technology
[0005] The purpose of the present invention is to provide a locking device for the aircraft stand to solve the technical problem that the aircraft in the prior art is prone to vibration when flying
Method used
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[0032] The technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Apparently, the described embodiments are some of the embodiments of the present invention, but not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0033] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" etc. The indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, or...
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The invention provides an aircraft foot stool locking device and an aircraft. The aircraft foot stool locking device comprises a framework (51); the framework (51) is connected with a foot stool (3); a sliding component (54) is arranged on the framework (51); a first end of the sliding component (54) and the foot stool (3) are oppositely arranged; a second end of the sliding component (54) is connected with a driving component; and the driving component is used for driving the sliding component (54) to move towards the foot stool (3) so that the first end of the sliding component (54) props against the foot stool (3) outwards. When an aircraft is started or the foot stool is opened, the driving component works to drive the sliding component to move towards the foot stool; when the first end of the sliding component slides to prop against the foot stool in a contacting manner, the sliding component applies an outward pushing force to the foot stool to lock the foot stool so that the foot stool is prevented from shaking in the flying process; therefore, the flying safety is guaranteed and the quality of an image shot by the aircraft is guaranteed.
Description
technical field [0001] The invention relates to the technical field of aircraft, in particular to an aircraft tripod locking device and an aircraft. Background technique [0002] Multi-rotor aircraft are widely used in the three major fields of military, scientific research, and civilian use to perform tasks such as transportation, surveillance, reconnaissance, exploration, and photography because of their advantages such as flexible maneuverability, fast response, strong environmental adaptability, and low operational requirements. A multi-rotor aircraft typically consists of a fuselage, arms, undercarriage (also known as landing gear), and aircraft control systems. The arms are connected to the upper part of the fuselage, each arm has a power system for driving the multi-rotor aircraft, the lower part of the fuselage is equipped with a tripod, and the inside of the fuselage is provided with an aircraft control system. In general, a multi-rotor aircraft includes a pluralit...
Claims
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IPC IPC(8): B64C25/32
CPCB64C25/32
Inventor 郑卫锋其他发明人请求不公开姓名
Owner POWERVISION ROBOT INC