Rohr, Inc.

Richard Haslim

Richard Scott Alloway

Bryce Tyler Kelford

Adam G Saunders

Travis Michael Frazier

Vijay V Pujar

Travis M Frazier

An assembly is provided for an aircraft propulsion system. This assembly includes a nozzle extending axially along and circumferentially about an axial centerline. The nozzle includes a nozzle panel and a nozzle fairing fixedly connected to the nozzle panel at an axial end of the nozzle. The nozzle is configured with an internal flow passage radially between the nozzle panel and the nozzle fairing. The internal flow passage extends axially within the nozzle to an outlet between the nozzle panel and the nozzle fairing at the axial end of the nozzle.

Aircraft propulsion system nozzle with internal flow passage

An assembly is provided for an aircraft propulsion system. This assembly includes an exhaust center body and a duct system. The exhaust center body includes an exterior skin. The duct system is fluidly coupled with a plurality of exterior skin perforations in the exterior skin. The duct system is configured to direct bypass air received from a bypass flow path within the aircraft propulsion system to the exterior skin perforations.

Transpirationally cooled exhaust center body for an aircraft propulsion system

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Chula Vista, CA, United States of America

Richard Haslim