Deflection Limiter Cascade Assembly Thrust Reverser
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Solution Overview
Problem
Existing thrust reverser designs for aircraft nacelles face challenges in effectively managing load paths and deflection limitations during the translation of cascade arrays from a stowed to a deployed position, which can lead to axial and radial deflections that compromise the efficiency and reliability of reverse thrust generation during landing.
Innovation Solution
The implementation of a cascade assembly with a forward hook device and a deflection limiter that includes a catch system to transfer loads and limit deflections, ensuring that the cascade assembly can move between stowed and deployed states while maintaining structural integrity and directing bypass airflow effectively.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If the cascade array translates from stowed to deployed position, then reverse thrust generation capability is improved, but axial and radial deflections increase compromising structural integrity
Solution Approach 1:
The deflection limiter is pre-configured in the cascade assembly before deployment, with the catch positioned to engage the arm at a predetermined location. This preliminary arrangement ensures that as soon as the cascade translates from stowed to deployed position, the deflection limiter is already in place to prevent excessive axial and radial deflections, thereby maintaining structural integrity while enabling reverse thrust generation.
Solution Approach 2:
The deflection limiter acts as an intermediary component between the cascade array and the fixed structure. The arm with catch mechanism serves as a mediator that transfers and controls the translation motion, allowing the cascade to move from stowed to deployed position while the deflection limiter prevents harmful deflections, thus resolving the contradiction between movement capability and structural stability.
2Force
If the cascade assembly is designed with effective load paths, then load transfer capability is improved, but device complexity increases due to additional deflection limiter components
Solution Approach 1:
The deflection limiter is segmented into distinct functional components: the arm, the catch with engaging surface, and the positioning features. This segmentation allows each component to be optimized independently for its specific function while maintaining overall simplicity. The load path is clearly defined through these segmented components, improving load transfer capability without requiring a completely complex redesign of the entire cascade assembly.
Solution Approach 2:
The deflection limiter is designed to be self-contained and self-activating. The catch automatically engages with the arm during the translation process without requiring external control systems or additional actuators. The positioning features on the arm and catch work together autonomously to establish the deflection limit, thereby improving load transfer capability while minimizing the increase in device complexity.
Data Source
Figure 1~2
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AI summary
A cascade assembly (60) of a nacelle (24) for a turbofan engine (20) includes a cascade (82) concentrically disposed about an centerline (C), and a translating sleeve (56) constructed and arranged to move between a forward position (64) and an aft position (66) along the centerline (C). A deflection limiter (85) of the cascade assembly (60) includes a first surface (147) facing at least in-part in a radial direction and a second surface (149) facing at least in-part in an opposite radial direction. The first surface (147) is carried by one of the cascade (82) and the translating sleeve (56) and the second surface (149) is carried by the other of the cascade (82) and the translating sleeve (56). The first and second surfaces (147, 149) oppose one-another for limiting deflection when the translating sleeve (56) is in the aft position (66) and are spaced axially apart when the translating sleeve (56) is in the forward position (64).