- Patent Title: Propelling nozzle for a turbofan engine on a supersonic aircraft
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Application No.: US16954053Application Date: 2018-12-05
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Publication No.: US11448162B2Publication Date: 2022-09-20
- Inventor: Predrag Todorovic , Thomas Schillinger
- Applicant: Rolls-Royce Deutschland Ltd & Co KG
- Applicant Address: DE Blankenfelde-Mahlow
- Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee Address: DE Blankenfelde-Mahlow
- Agency: Shuttleworth & Ingersoll, PLC
- Agent Timothy Klima
- Priority: DE102017130563.7 20171219
- International Application: PCT/EP2018/083676 WO 20181205
- International Announcement: WO2019/121022 WO 20190627
- Main IPC: F02K1/08
- IPC: F02K1/08 ; F02K1/56 ; B64D27/16 ; F02K1/78 ; F02K5/00 ; F02K1/70 ; B64C30/00
Abstract:
The invention relates to a propelling nozzle for a turbofan engine on a supersonic aircraft, the propelling nozzle including: a propelling nozzle wall, a duct, which is radially outwardly bounded by the propelling nozzle wall, and a central body arranged in the duct. According to the invention, the central body is connected to the propelling nozzle wall via at least one brace.
Public/Granted literature
- US20210079870A1 PROPELLING NOZZLE FOR A TURBOFAN ENGINE ON A SUPERSONIC AIRCRAFT Public/Granted day:2021-03-18
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