Rotor Mast Cuff Assembly for Ducted Fan Tip Gap Stability
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Solution Overview
Problem
Ducted fan systems face reduced thrust due to unfavorable flow characteristics caused by air mixing through the gap between fan blades and the duct, and the system requires increased out-of-plane stiffness to prevent catastrophic fan movement relative to the duct.
Innovation Solution
A rotor assembly with enhanced out-of-plane stiffness is achieved by applying a clamping force through components disposed between the hub and the mast bearing, using a combination of a rotor mast, cuff, and mast nut to supplement the stiffness of the mast, thereby reacting bending forces and maintaining alignment.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Productivity
If the tip gap between fan blades and duct is minimized to maximize thrust, then thrust generation is improved, but the risk of fan blade contact with duct increases due to movement caused by perpendicular forces
Solution Approach 1:
The system separates the fan assembly into independently adjustable components (fan hub, mounting structure, duct) that can be positioned relative to each other. This allows the fan to be mounted with precise positioning features that maintain optimal tip gap while accommodating movement through the adjustable mounting structure rather than requiring the entire system to be rigid or flexible.
Solution Approach 2:
The mounting structure includes adjustable parameters (positioning features, mounting angle, spacing) that can be changed to optimize the balance between tip gap minimization and movement accommodation. This allows the system to adapt the fan's position and orientation to maintain reliable operation while maximizing thrust performance.
2Reliability
If the fan is made more rigid to prevent movement and catastrophic contact, then reliability is improved, but the ability to accommodate perpendicular forces and maintain optimal alignment is reduced
Solution Approach 1:
The mounting structure incorporates dynamic elements that allow controlled movement and adjustment in response to perpendicular forces. The system transitions from a static rigid connection to a dynamic adjustable connection that can adapt to varying load conditions while maintaining reliable operation and optimal alignment.
Solution Approach 2:
The mounting structure acts as an intermediary between the fan hub and duct, providing a controlled interface that accommodates movement while preventing catastrophic contact. This intermediate structure absorbs and manages the effects of perpendicular forces, protecting both the fan and duct while maintaining reliable operation.
3Adaptability or versatility
If standard helicopter rotor flexion is allowed to accommodate movement, then adaptability is improved, but thrust generation is reduced due to increased tip gap and unfavorable flow characteristics
Solution Approach 1:
The system separates the fan assembly into independently adjustable components that can accommodate movement through controlled adjustment rather than uniform flexion. This segmentation allows the mounting structure to handle movement while the fan blades maintain their optimal position relative to the duct, preserving thrust-generating flow characteristics.
Solution Approach 2:
The mounting structure serves as an intermediary that absorbs and manages movement caused by flexion or external forces, isolating the fan blades from these movements. This allows the system to accommodate adaptability needs while the fan operates in a stable position that maintains optimal tip gap and favorable flow characteristics for maximum thrust.
Data Source
AI summary
A rotor assembly configured to increase the stiffness of a rotor mast. The rotor assembly includes the rotor mast, a rotor hub, a mast nut, a mast bearing, and a cuff disposed between the mast nut and the mast bearing. The cuff is captured and compressed between the mast nut and the inner race of the mast bearing along an uninterrupted load path that extends between the mast nut and the mast bearing.


