Aircraft accurate control azimuth instrument
A technology of precise control and azimuth, which is applied in the field of aircraft, can solve the problems affecting the steering of the aircraft, the deformation of the tie rod, and the large load of the tie rod, and achieve the effect of reducing the length of the single tie rod, reducing the excessive force and effective control
Inactive Publication Date: 2016-12-07
马铿贵
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Problems solved by technology
[0002] In general, the steering rod of the steering assembly of the aircraft is connected by a rod. Because the rod of the steering device is connected between the integrated controller and the steering device, the rigidity is not enough due to the long length, and the load at both ends of the rod is large. This will deform the tie rod, and when the integrated controller is pulled by the whole tie rod, the angle between the tie rod and the integrated controller will not be perpendicular due to the deformation of the tie rod, which will affect the steering of the aircraft during flight, and the steering of the aircraft cannot be precisely controlled
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[0010] The present invention will be further described below in conjunction with the accompanying drawings.
[0011] refer to figure 1 As shown, the tail steering assembly 100 of the present invention is installed at the end of the aircraft for controlling the steering of the aircraft. It includes an integrated controller 1, a direction-changing actuator 2 and a connecting rod 3. The integrated controller 1 and the direction-changing actuator 2 are respectively installed at both ends of the connecting rod 3, and the work of the integrated controller is controlled by the direction-changing actuator 2.
[0012] The connecting rod 3 includes at least a single direction-changing actuator pull rod. In this embodiment, the connecting rod 3 includes two direction-changing actuator pull rods of different lengths, which are respectively the long direction-changing actuator pull rod 31 and the short direction-changing actuator Pull rod 32. The connecting rod 3 also includes a directio...
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The invention provides an aircraft accurate control azimuth instrument. The aircraft accurate control azimuth instrument comprises a connecting rod, an integrated controller and a turning executing device. For a steering unit of the aircraft accurate control azimuth instrument, a section of long turning executing device pull rod and a section of short turning executing device pull rod which are connected with each other are adopted for replacing a single pull rod, the two sections of pull rods are parallel to each other, and two ends of the two sections of pull rods are connected with the turning executing device and the integrated controller respectively; due to the segment-type pull rod, the stress applied to two ends of the single pull rod in the prior art is reduced, meanwhile, the overlarge stress applied to the two ends of the single pull rod due to the too long single pull rod is reduced, therefore, the deformation caused by the overlarge stress applied to the too long single pull rod is reduced, and thus the steering of the aircraft can be effectively controlled.
Description
technical field [0001] The invention relates to the field of aircraft, in particular to an aircraft precision control azimuth instrument. Background technique [0002] In general, the steering rod of the steering assembly of the aircraft is connected by a rod. Because the rod of the steering device is connected between the integrated controller and the steering device, the rigidity is not enough due to the long length, and the load at both ends of the rod is large. This will deform the pull rod, and when the integrated controller is pulled by the entire pull rod, the angle between the pull rod and the integrated controller will be non-perpendicular due to the deformation of the pull rod, which will affect the steering of the aircraft during flight and cannot accurately control the steering of the aircraft. [0003] In view of this, it is necessary to provide an assembly capable of controlling the steering of the aircraft more smoothly. Contents of the invention [0004] B...
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IPC IPC(8): A63H27/20
Inventor 马铿贵
Owner 马铿贵