Translating-Rotating Hinge Assembly for Thrust Reverser
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Solution Overview
Problem
Thrust reverser systems for high-bypass turbofan engines require improvements in weight reduction, load distribution, and compactness while maintaining deployment and maintenance access capabilities.
Innovation Solution
A hinge assembly that enables both translational and rotational movements of the transcowl, allowing it to translate aft for deployment and pivot radially outward for maintenance, without an intermediate translating component, thus minimizing weight and space.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Ease of operation
If traditional separate translating and rotating mechanisms are used, then deployment and maintenance access capabilities are achieved, but weight and device complexity increase
Solution Approach 1:
The patent combines the translating and rotating functions into a single integrated hinge assembly. The hinge assembly includes a translating member that moves axially and a rotating member that pivots, working together as one unit to provide both deployment and maintenance access movements without requiring separate mechanisms.
Solution Approach 2:
The hinge assembly is designed to perform multiple functions: it enables the transcowl to translate aft for thrust reverser deployment, pivot radially outward for maintenance access, and return to stowed position. This multi-functional design eliminates the need for separate dedicated mechanisms for each operation.
2Ease of operation
If traditional separate translating and rotating mechanisms are used, then deployment and maintenance access capabilities are achieved, but device complexity and space occupation increase
Solution Approach 1:
The patent combines the translating and rotating functions into a single integrated hinge assembly. The hinge assembly includes a translating member that moves axially and a rotating member that pivots, working together as one unit to provide both deployment and maintenance access movements without requiring separate mechanisms.
Solution Approach 2:
The translating member is received within the rotating member in a nested arrangement. The translating member slides within a channel formed by the rotating member, allowing compact integration of both movement functions in a confined space while maintaining full functionality.
3Ease of operation
If intermediate translating components are used, then movement capability is achieved, but weight and compactness are compromised
Solution Approach 1:
The translating member is received within the rotating member in a nested arrangement. The translating member slides within a channel formed by the rotating member, allowing compact integration of both movement functions in a confined space while maintaining full functionality.
Solution Approach 2:
The patent combines the translating and rotating functions into a single integrated hinge assembly. The hinge assembly includes a translating member that moves axially and a rotating member that pivots, working together as one unit to provide both deployment and maintenance access movements without requiring separate mechanisms.
Data Source
AI summary
A thrust reverser system suitable for a high-bypass turbofan engine of a type having a nacelle. The thrust reverser system includes a transcowl having a stowed, deployed and open positions. A hinge assembly translationally and rotationally couples the transcowl to a fixed structure that does not translate when the transcowl is translated in the aft direction. The hinge assembly includes a first member connected to the transcowl for translation therewith, and a fixed second member that defines a channel in which a portion of the first member is slidably received. The first and second members are configured to enable the portion of the first member to translate within the slider channel in an aft direction corresponding to a translational movement of the transcowl, and to enable the portion of the first member to rotate within the channel corresponding to a pivotal movement of the transcowl.


