Invention Grant
- Patent Title: Injection device for combustion chambers of liquid-fueled rocket engines
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Application No.: US12823283Application Date: 2010-06-25
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Publication No.: US08683810B2Publication Date: 2014-04-01
- Inventor: Ulrich Gotzig , Dieter May
- Applicant: Ulrich Gotzig , Dieter May
- Applicant Address: DE Bremen
- Assignee: EADS Space Transportation GmbH
- Current Assignee: EADS Space Transportation GmbH
- Current Assignee Address: DE Bremen
- Agency: Greenblum & Bernstein, P.L.C.
- Priority: DE102005024608 20050525
- Main IPC: F02C7/22
- IPC: F02C7/22

Abstract:
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.
Public/Granted literature
- US20100257840A1 INJECTION DEVICE FOR COMBUSTION CHAMBERS OF LIQUID-FUELED ROCKET ENGINES Public/Granted day:2010-10-14
Information query
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