- 专利标题: Injection device for combustion chambers of liquid-fueled rocket engines
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申请号: US12823283申请日: 2010-06-25
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公开(公告)号: US08683810B2公开(公告)日: 2014-04-01
- 发明人: Ulrich Gotzig , Dieter May
- 申请人: Ulrich Gotzig , Dieter May
- 申请人地址: DE Bremen
- 专利权人: EADS Space Transportation GmbH
- 当前专利权人: EADS Space Transportation GmbH
- 当前专利权人地址: DE Bremen
- 代理机构: Greenblum & Bernstein, P.L.C.
- 优先权: DE102005024608 20050525
- 主分类号: F02C7/22
- IPC分类号: F02C7/22
摘要:
An injection device including at least one injection plate adjacent a combustion space of a combustion chamber, and at least one first injection nozzle including a first entry bore having a first discharge into the combustion chamber, and a first orifice bore, having a cross-sectional dimension less than or equal to the first entry bore, coaxially arranged with the first entry bore and remote from the first discharge. At least one second injection nozzle includes a second entry bore having a second discharge into the combustion chamber, and a second orifice bore, having a cross-sectional dimension less than or equal to the second entry bore, coaxially arranged with the second entry bore and remote from the second discharge. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.
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