Annular Seal Grooves Prevent Extrusion in High-Pressure Compressors
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Solution Overview
Problem
Traditional O-rings in high-pressure compressors experience increased failure rates due to radial expansion of the casing and fluid absorption, leading to extrusion and blistering under high pressure conditions.
Innovation Solution
An annular seal with a generally rectangular cross-section, featuring an outer radial surface with annular grooves and slots, and axial sidewalls, configured to maintain a low-pressure environment on one side and a high-pressure environment on the other, is mounted between the compressor bundle and housing to provide effective sealing.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If O-rings are used to seal the compressor bundle, then sealing is achieved, but the O-rings absorb fluid at high pressure and blister or explode when pressure is reduced
Solution Approach 1:
The fluid absorption problem is mitigated by segmenting the seal into multiple smaller O-rings rather than one large O-ring. Each smaller O-ring absorbs less fluid, reducing the cumulative blisting risk while maintaining sealing effectiveness across the entire circumference.
Solution Approach 2:
Backup rings are introduced as intermediary elements between the O-rings and the expansion gap. These backup rings act as barriers that prevent fluid-saturated O-rings from contacting each other and failing, allowing the system to tolerate fluid absorption without catastrophic failure.
2Stress or pressure
If the compressor casing expands radially under high pressure, then the casing accommodates pressure, but the gap between compressor bundle and casing increases promoting O-ring extrusion
Solution Approach 1:
The groove configuration segments the potential extrusion path into isolated sections. Each O-ring is confined to its own groove, so even when the casing expands and creates gaps, the O-rings cannot extrude into the expansion space because the grooves act as physical barriers containing each seal element independently.
Solution Approach 2:
The design accepts that casing expansion will create gaps, but converts this potentially harmful effect into a benign condition by providing backup rings that fill the expansion gap. The gap that would normally cause extrusion is instead filled with inert backup ring material that prevents O-ring contact and failure.
Data Source
Figure 1A
Figure 1B
Figure 2~3
AI summary
An annular seal is provided for use in a turbomachine. The annular seal may form a generally rectangular cross-section and may include an outer radial surface forming an outer sealing surface and defining at least one annular groove and a plurality of slots spaced circumferentially about the outer radial surface. Each slot may have an end terminating in the at least one annular groove. The annular seal may also include a first axial sidewall forming a sidewall sealing surface and a recessed portion and a second axial sidewall opposing the first axial sidewall. At least one annular groove and the plurality of slots may be configured to maintain a low pressure environment across at least a portion of the outer radial surface. The second axial sidewall, the recessed portion, and the inner radial surface may be configured to maintain a high pressure environment there across during operation of the turbomachine.