Invention Grant
- Patent Title: Compact, high performance swirl combustion rocket engine
- Patent Title (中): 紧凑，高性能的涡流燃烧火箭发动机
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Application No.: US11805016Application Date: 2007-05-22
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Publication No.: US07690192B2Publication Date: 2010-04-06
- Inventor: Robert J. Pederson , Stephen N. Schmotolocha
- Applicant: Robert J. Pederson , Stephen N. Schmotolocha
- Applicant Address: US CA Canoga Park
- Assignee: Pratt & Whitney Rocketdyne, Inc.
- Current Assignee: Pratt & Whitney Rocketdyne, Inc.
- Current Assignee Address: US CA Canoga Park
- Agency: Carlson, Gaskey & Olds
- Main IPC: F02K9/28
- IPC: F02K9/28
Abstract:
A rocket engine includes a combustor assembly for carrying out a combustion process of fuel and oxidizer rocket propellants to produce thrust. A swirl generator is positioned within the combustor assembly to produce a turbulent flowfield of the fuel and oxidizer rocket propellants within the combustor assembly.
Public/Granted literature
- US20080256925A1 Compact, high performance swirl combustion rocket engine Public/Granted day:2008-10-23
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