Inflatable Flowpath Wall for Adaptive Turbofan Geometry
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Solution Overview
Problem
Existing turbofan engine flowpath geometries with fixed peripheral boundaries fail to optimize engine performance across various operating modes, necessitating a compromise in performance.
Innovation Solution
Incorporation of an inflatable bladder with a deformable face skin and an actuation system, including an air system and mechanical actuators, to dynamically adjust the flowpath geometry by inflating or deflating the bladder, thereby altering the exterior surface geometry.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Adaptability or versatility
If fixed peripheral boundaries are used in flowpath geometry, then structural simplicity and manufacturing ease are maintained, but engine performance cannot be optimized across various operating modes
Solution Approach 1:
The patent applies the dynamics principle by transforming the static fixed peripheral boundaries into dynamic adjustable boundaries using inflatable bladders. The bladders can be inflated or deflated to change the flowpath geometry, allowing the engine to optimize performance across different operating modes. This dynamic adjustment capability directly resolves the contradiction between adaptability and device complexity.
Solution Approach 2:
The patent utilizes parameter changes by modifying the physical state of the bladder material through inflation and deflation. By changing the volume and pressure parameters of the bladder, the flowpath geometry is adjusted to suit different operating conditions. This parameter-based approach enables performance optimization without requiring completely different structural designs.
2Productivity
If fixed flowpath geometry is used, then manufacturing precision is easier to achieve, but engine efficiency varies across operating modes
Solution Approach 1:
The dynamic bladder system allows the flowpath geometry to be adjusted after manufacturing, eliminating the need for multiple precision-manufactured components for different operating modes. A single manufactured structure can adapt its geometry through bladder inflation, maintaining manufacturing simplicity while achieving high efficiency across modes.
Solution Approach 2:
The inflatable bladder acts as an intermediary element between the fixed manufactured structure and the required variable geometry. The bladder provides the adaptability function without requiring the base structure to be manufactured with variable geometry, thus decoupling manufacturing precision requirements from operational adaptability.
3Adaptability or versatility
If variable geometry is implemented using traditional mechanisms, then engine performance can be optimized, but device complexity and mechanical failure risk increase
Solution Approach 1:
The patent employs pneumatic principles by using inflatable bladders to achieve geometry adjustment. This replaces complex mechanical linkages, gears, or motors with a simpler pneumatic system that has fewer moving parts and lower risk of mechanical failure. The pneumatic actuation method inherently improves reliability while maintaining adaptability.
Solution Approach 2:
The use of flexible bladder material allows for smooth geometry changes without rigid joints or connection points that could fail. The flexible shell approach eliminates stress concentration points and mechanical wear issues associated with traditional variable geometry mechanisms, thereby enhancing system reliability.
Applied Scientific Principles
This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.
Function Achieved in This Case
Enhances engine performance by allowing adaptive tuning of the flowpath geometry to suit varying operating conditions, improving efficiency and thrust generation.
Implementation Method 1
The air system is configured to regulate air pressure within the interior volume to deform the deformable face skin and change a geometry of the exterior surface
Implementation Method 2
The solenoid is configured to push or pull the deformable face skin to further deform the deformable face skin and change the geometry of the exterior surface
Implementation Method 3
The spring element is configured to push or pull the deformable face skin to further deform the deformable face skin and change the geometry of the exterior surface
Data Source
AI summary
An assembly is provided for an aircraft propulsion system. This assembly includes a flowpath wall and an actuation system. The flowpath wall includes an inflatable bladder with a deformable face skin and an interior volume. The deformable face skin includes an exterior surface that forms a peripheral boundary of a flowpath along the flowpath wall. The interior volume extends within the inflatable bladder to the deformable face skin. The actuation system includes an air system and an actuator. The air system is fluidly coupled to the interior volume. The air system is configured to inflate or deflate the inflatable bladder to change a geometry of the exterior surface. The actuator is disposed in the interior volume. The actuator is configured to mechanically apply a force to the deformable face skin to further change the geometry of the exterior surface.


