Strainer for a gas turbine engine

Details Strainer for a gas turbine engine Strainer for a gas turbine engine

2006-08-23

2009-12-01

Smith, Duane (Department: 1797)

Gas separation

Aircraft anti-ingestion means

C055S336000, C055S350100, C055S385100, C055S463000, C055S521000, C055S488000, C055S489000, C055SDIG017, C060S039092, C244S05300R

Reexamination Certificate

active

07625415

ABSTRACT:
The strainer comprises an unitary body having a main section and a collar section located around the main section. The collar section has a substantially outwardly-projecting portion located around the main section and an upstream projecting portion located around the substantially outwardly-projecting portion.

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