Aircraft ice-melter
A technology for deicing vehicles and aircrafts, which is applied to aircraft parts, steering mechanisms, vehicle components, etc., which can solve the problem of difficult real-time control of the relative position and swing angle between the working cabin and the body, affecting the safety and operability of the aircraft, and the pilot's control of the aircraft. Difficulty, etc.
Active Publication Date: 2019-03-19
山河机场设备股份有限公司
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Problems solved by technology
[0002] When the aircraft encounters cold weather such as low temperature, high humidity, rainfall, and snowfall, a layer of frost, snow or ice will be formed on its surface. The ice and snow will condense on the wings of the aircraft, which will make the surface of the wings rough and reduce flight resistance. increase, this will make the aircraft’s aerodynamic performance worse when the take-off speed is not fast, and it will be more difficult for the pilot to control the aircraft, which will affect the safety and operability of the aircraft
[0003] However, when the existing deicing vehicle for deicing the aircraft is in operation, it is difficult to control the relative position and swing angle of the operation cabin and the vehicle body in real time after the operation cabin swings, and it is also impossible to control the rotation direction and angle of the steering axle of the deicing vehicle in real time. During the operation process, when the vehicle is moving, it is easy to collide with the aircraft
Method used
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[0022] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. 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.
[0023] The core of the present invention is to provide an aircraft deicing vehicle, the steering wheel can rotate with the operating cabin 1 during its work.
[0024] Please refer to figure 1 with figure 2 , figure 1 The schematic diagram of the aircraft deicing vehicle provided by the present invention; figure 2 It is a schematic diagram of the operation of the aircraft deicing vehicle provided by the present invention.
[0025] An aircraft deicing vehi...
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The invention discloses an aircraft ice-melter, comprising a cart body and an operating cabin mounted on the cart body. A first detection sensor used for detecting rotation angle of the operating cabin is arranged on the operating cabin; the cart body is provided with a controller and a steering wheel rotation angle detection sensor for detecting rotation angle of steering wheels, the first detection sensor and the steering wheel rotation angle detection sensor are both in signal connection with the controller; the controller controls rotation angle of the steering wheels according to the rotation angle value sent from the first detection senor and the steering wheel rotation angle detection sensor. The first detection sensor can monitor and measure rotation angle of of the operating cabinin real time, the controller acquires rotatable angle of the steering wheels according to the received rotation angle of the operating cabin, the steering wheel rotation angle detection sensor can monitor rotation angle of the steering wheels in real time, the controller can control actual rotation angle of the steering wheels, and thus, the steering wheels can rotate by corresponding angle according to rotation angle of the operating cabin.
Description
technical field [0001] The invention relates to the field of technical aircraft deicing, and more specifically relates to an aircraft deicing vehicle. Background technique [0002] When the aircraft encounters cold weather such as low temperature, high humidity, rainfall, and snowfall, a layer of frost, snow or ice will be formed on its surface. The ice and snow will condense on the wings of the aircraft, which will make the surface of the wings rough and reduce flight resistance. Increase, this will cause the aerodynamic performance of the aircraft to deteriorate when the take-off speed is not fast, and it will be more difficult for the pilot to control the aircraft, which will affect the safety and operability of the aircraft. [0003] However, when the existing deicing vehicle for deicing the aircraft is in operation, it is difficult to control the relative position and swing angle of the operation cabin and the vehicle body in real time after the operation cabin swings, ...
Claims
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Patent Timeline
Login to View More IPC IPC(8): B62D5/06B62D6/00B64F5/20
CPCB62D5/06B62D6/00B64F5/20
Inventor 王忠仁李燕
Owner 山河机场设备股份有限公司