Double-rocker transmission mechanism applicable to movable control surface of aerial vehicle
A technology of transmission mechanism and aircraft, which is applied in the directions of aircraft transmission, aircraft power transmission, and aircraft power devices, etc., can solve the problems of exposed high and low temperature environment, affect the performance of the motor, no layout space, etc., and achieve high connection rigidity of the mechanism. The effect of mechanism movement reliability and high transmission precision
A technology of transmission mechanism and aircraft, which is applied in the directions of aircraft transmission, aircraft power transmission, and aircraft power devices, etc., can solve the problems of exposed high and low temperature environment, affect the performance of the motor, no layout space, etc., and achieve high connection rigidity of the mechanism. The effect of mechanism movement reliability and high transmission precision
CN104290901AActive Publication Date: 2015-01-21CHINA ACAD OF LAUNCH VEHICLE TECH
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[0014] The double rocker arm transmission mechanism according to the present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.
[0015] figure 1 It is a structural schematic diagram of the double rocker arm transmission mechanism of the present invention, as figure 1 As shown, in the double rocker arm transmission mechanism, the movable rudder surface 2 is rotatably connected to the aircraft body 1, and can swing around the rotation point between it and the aircraft body 1 by means of the double rocker arm transmission mechanism. action.
[0016] As shown in the figure, the double rocker arm transmission mechanism of the present invention includes a rocker arm 3 , a connecting rod 4 , an auxiliary rocker arm 5 , a linear servo actuator 6 , a first base 7 , and a second base 8 . Wherein, the rocker arm 3 is fixedly installed on the movable rudder surface 2 , and the first base 7 and the second base 8 ar...
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The invention relates to a double-rocker transmission mechanism applicable to a movable control surface of an aerial vehicle. A first hinged joint pair is formed between a rocker and a connecting bar, a second hinged joint pair is formed between the connecting bar and an auxiliary rocker, a third hinged joint pair is formed between the auxiliary rocker and a linear servo actuator, a fourth hinged joint pair is formed between the linear servo actuator and a first base, and a fifth hinged joint pair is formed between the auxiliary rocker and a second base; in each hinged joint pair, the axial movement of a hinge bearing is prevented by the way that a bush 12 and a sleeve 13 arranged on corresponding connecting lugs are in abutted connection with two sides of an inner ring of a hinge bearing 9 on a connector between two connecting lugs. The double-rocker transmission mechanism applicable to a movable control surface of an aerial vehicle provided by the invention can avoid exposure of a driving part of the mechanism to external high-temperature environments, so that the movement reliability of the mechanism is improved.
Description
technical field [0001] The invention relates to a double rocker arm transmission mechanism suitable for a movable rudder surface of an aircraft, belonging to the field of mechanism device design. Background technique [0002] In order to control the flight attitude in real time, multiple active rudder surfaces are generally set on the aircraft. The transmission mechanism is an important device that transmits the active force of the servo actuator to manipulate the movable rudder surface for deflection. [0003] At present, the drive of the movable rudder surface mostly adopts the form of motor direct drive or single rocker mechanism drive. The motor direct drive mode is that the motor rotor is directly connected to the rudder shaft, and the rudder surface is driven to deflect by the rotation of the motor; the single rocker arm mechanism is driven by a linear servo actuator to push the rocker arm fixed on the rudder shaft to deflect, driving The rudder deflects. The above-...
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Patent Timeline
21 Jan 2015
Publication
CN104290901A
- IPC
- B64C13/30
- Inventors
- 贾磊; 彭波