Aspects of the disclosure are directed to an engine of an aircraft. Aspects of the disclosure include an inlet housing configured to receive core air of an engine, and at least one valve coupled to the inlet housing and configured to bleed the core air during a starting of the engine, where the at least one valve is housed within the engine.
PNEUMATIC PORTING VIA SELF-ACTUATED DUAL PIVOT FLAPPER VALVE
2016-11-24
Patent
Electronic Resource
English