Invention Grant
- Patent Title: Aircraft propulsion system nozzle with internal flow passage
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Application No.: US17307570Application Date: 2021-05-04
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Publication No.: US11746726B2Publication Date: 2023-09-05
- Inventor: Adam Saunders , Bryce T. Kelford , Travis M. Frazier , Richard Haslim , Richard S. Alloway , Vijay V. Pujar
- Applicant: Rohr, Inc.
- Applicant Address: US CA Chula Vista
- Assignee: Rohr, Inc.
- Current Assignee: Rohr, Inc.
- Current Assignee Address: US CA Chula Vista
- Agency: GETZ BALICH LLC
- Main IPC: F02K1/52
- IPC: F02K1/52 ; B64D29/06 ; F02K1/80 ; F02K1/04 ; F02K1/82 ; F02K1/38 ; B64D27/26 ; B64D27/18 ; F02K3/06
Abstract:
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.
Public/Granted literature
- US20210348581A1 AIRCRAFT PROPULSION SYSTEM NOZZLE WITH INTERNAL FLOW PASSAGE Public/Granted day:2021-11-11
Information query
