Transverse Jet Control on Rotating Bodies to Reduce Flow Separation
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Solution Overview
Problem
High-speed rotating bodies experience flow separation and shock waves during flight, leading to reduced efficiency due to extreme rotation and velocity, which existing technologies have not effectively addressed.
Innovation Solution
The implementation of transverse jets that inject air into the airstream, altering the flow structure around and behind the body, specifically impacting viscous and pressure drag, shock wave interactions, boundary layer separations, recirculation, and wake, by modifying the flow characteristics through angle of attack, Reynolds number, and jet exit velocity.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Speed
If high-speed rotation and velocity are maintained, then flight speed and rotational performance are improved, but flow separation and shock waves occur leading to reduced efficiency
Solution Approach 1:
The patent applies preliminary anti-action by introducing transverse jets before flow separation occurs. The jets create a protective flow structure that prevents separation and shock wave formation in advance, allowing high-speed flight to maintain efficiency without the adverse effects that would otherwise occur at those speeds
2Productivity
If transverse jets are introduced to reduce flow separation, then flight efficiency is improved, but device complexity increases
Solution Approach 1:
The patent utilizes porous material principles by incorporating transverse jets through the body surface. This approach integrates the jet system into the existing body structure rather than adding separate complex components, thereby improving flight efficiency while minimizing the increase in device complexity
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
The introduction of transverse jets significantly reduces flow separation and shock waves, enhancing flight efficiency by modifying the flow structure and drag interactions, thereby improving the overall performance of high-speed rotating objects.
Implementation Method 1
The use of transverse jets significantly reduces flow separation and shock waves, enhancing flight efficiency by modifying drag interactions and boundary layer behavior
Implementation Method 2
specifically impacting viscous and pressure drag, shock wave interactions, boundary layer separations, recirculation, and wake
Data Source
AI summary
A system includes an elongated cylindrical body having a first end extending to a second end; an outer surface and an inner surface; a thickness extending from the inner surface to the outer surface; and a plurality of openings extending from the inner surface to the outer surface. The system further includes a fluid injection apparatus disposed within the elongated cylindrical body, the fluid injection apparatus is configured to pass fluid through the openings.


