Connecting device of airplane flap rocker arm

Abstract

The invention provides a connecting device of an aircraft flap rocker arm. The connecting device of the aircraft flap rocker arm comprises a flap rocker arm 1, a connecting joint 2, a suspension rib joint 3, a front beam 4 and a rear beam 5, wherein the flap rocker arm 1 is of a triangular truss type structure, the flap rocker arm 1 is provided with at least three suspension points, two suspensionpoints arranged at the upper end of the flap rocker arm 1 are connected with the lower wing surface of the flap, and suspension points arranged at the lower end of the flap rocker arm 1 are connectedwith a support arm at the rear edge of the wing; the rear lower end of the suspension rib joint 3 is provided with a lug, the front end of the suspension rib joint 3 relative to the course is connected with the front beam 4, and the rear end of the suspension rib joint 3 relative to the course is connected with the rear beam 5; the connecting joint 2 is of an L-shaped structure, and a lug part isarranged at the L-shaped lower end of the connecting joint 2; a lug part of the suspension rib connector 3 is connected with a suspension point arranged at the upper end of the flap rocker arm 1, anda lug part of the connecting connector 2 is connected with another suspension point arranged at the upper end of the flap rocker arm 1.

Description

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AI Technical Summary

Benefits of technology

This new type of linkage for a flapper rocking arm can be designed that includes various technical improvements over existing methods such as screws or rivets. It's easier to put together than previous versions without sacrificed strength due to their simplicity compared to other ways they were connected. Additionally, it makes them more stable during use by taking care of how well these connections are made when installed properly on different parts of the vehicle. Overall, this innovative solution improves the performance and ease-of-installability of the flapping arms used in vehicles while maintaining overall safety standards.

Problems solved by technology

This invention relates to improving the strength and durability of wings used for airplanes by adding extra parts called suspending joints between certain components like the fuselage's main body frame (or other support structures) and its tailpieces. These connections help prevent damage from external factors such as vibrations caused during flight.

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