Buffer air assembly for an aircraft engine
AssigneeRtx Corporation
InventorsAndrew E. Breault, William K. Ackermann
Life of this patent
Estimating the term…
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AssigneeRtx Corporation
InventorsAndrew E. Breault, William K. Ackermann
Estimating the term…
A buffer air assembly for an aircraft engine includes a low-pressure header, a high-pressure header, a low-pressure bleed air source, a high-pressure bleed air source, and an electric buffer compressor. The low-pressure header is connected to at least one low-pressure bearing compartment. The high-pressure header is connected to at least one high-pressure bearing compartment. The low-pressure bleed air source is connected to the low-pressure header. The low-pressure bleed air source is configured to direct a low-pressure buffering air to the at least one low-pressure bearing compartment through the low-pressure header. The high-pressure bleed air source is configured to direct a high-pressure buffering air to the at least one high-pressure bearing compartment through the high-pressure header. The electric buffer compressor is connected to the low-pressure header and the high-pressure header. The electric buffer compressor is configured to direct pressurized buffering air to the low-pressure header and the high-pressure header.
A buffer air assembly for an aircraft engine, the buffer air assembly comprising:
An engine for an aircraft, the engine comprising:
A buffer air assembly for an aircraft engine, the buffer air assembly comprising:
Dependencies are inferred from the claim text.