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A forward and reverse push interlocking mechanism

An interlocking mechanism, reverse push rod technology, applied in the direction of engine components, mechanical control devices, devices that prevent/restrict/restore the movement of parts of the control mechanism, etc.

Active Publication Date: 2021-05-04
BEIJING QINGYUN AVIATION INSTR CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, there is no forward and reverse thrust linkage integrated design forward and reverse thrust interlocking mechanism on large aircraft

Method used

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  • A forward and reverse push interlocking mechanism
  • A forward and reverse push interlocking mechanism

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Embodiment Construction

[0015] Below in conjunction with accompanying drawing, the present invention is further described:

[0016] Such as figure 1 As shown, a positive and negative push interlock mechanism includes a reverse push rod 1, a positive push rod 2, an intermediate baffle plate 3, and a pin shaft 5; the positive push rod 2 includes a connecting rod a6, a connecting rod b7, a lock arm 4. Cam assembly; connecting rod a6, connecting rod b7, lock arm 4 and the cam assembly are installed inside the forward push rod 2 through hinges, the reverse push rod 1 is linked with the positive push rod 2, and one end of the connecting rod a6 is connected to the reverse push rod The rod 1 is connected by a hinge, and the other end is connected to the lock arm 4, so that the anti-push rod 1, the connecting rod a6, and the lock arm 4 constitute a four-bar linkage mechanism; one end of the connecting rod b7 is connected to the lock arm 4, and the other end Connected with the cam mechanism, the connecting ro...

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PUM

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Abstract

The invention belongs to the flight automatic control technology, is used in the throttle console of the airborne power device system, and can also be used in other electromechanical products, and relates to a forward and reverse thrust interlocking mechanism, comprising a reverse thrust rod (1), a forward thrust rod (2), the middle baffle plate (3), the pin shaft (5); the present invention adopts the forward and reverse push rod design as an integral type, the structure is compact, and the interlock function can also be realized under the condition of realizing relatively independent movement, without occupying Excessive space, the design of the middle baffle, not only realizes the function of forward and reverse push interlock, but also realizes the physical isolation from other channels, and under certain circumstances, realizes the weight reduction design of the product, and the forward and reverse push interlock The realization of the function is guaranteed by mechanical parts, the structure is simple and reliable, and the safety is high.

Description

technical field [0001] The invention belongs to the flight automatic control technology, which is used in the throttle console of the airborne power plant system, and can also be used in other electromechanical products, and relates to a forward and reverse thrust interlocking mechanism. Background technique [0002] The forward and reverse thrust function is widely used in military and civilian large aircraft at home and abroad. For large aircraft that pursue safety, how to avoid misuse and how to realize the forward and reverse thrust self-locking function has become a hot spot of research. At present, foreign applications The interlocking technology of electrical appliances has the risk of failure of electronic components, which is not as reliable as the mechanical one. At present, there is no forward and reverse thrust interlocking mechanism with an integrated design of forward and reverse thrust connecting rods on large aircraft. Contents of the invention [0003] Th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02C9/26G05G5/02
Inventor 潘治赟梁赫刘帆杨金霖杨雪飞朱超
Owner BEIJING QINGYUN AVIATION INSTR CO LTD