Invention Grant
US08690098B2 Air ejector nozzle tube for an oil heat exchanger of an aircraft engine
有权
用于飞机发动机的油热交换器的喷射器喷嘴管
- Patent Title: Air ejector nozzle tube for an oil heat exchanger of an aircraft engine
- Patent Title (中): 用于飞机发动机的油热交换器的喷射器喷嘴管
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Application No.: US13039795Application Date: 2011-03-03
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Publication No.: US08690098B2Publication Date: 2014-04-08
- Inventor: Predrag Todorovic
- Applicant: Predrag Todorovic
- Applicant Address: DE
- Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee Address: DE
- Agency: Shuttleworth & Ingersoll, PLC
- Agent Timothy J. Klima
- Priority: DE102010010128 20100304
- Main IPC: B64D33/10
- IPC: B64D33/10

Abstract:
An ejector nozzle tube, having along its length an essentially constant, essentially oval hollow cross-section, with a leading edge nozzle, having a rounded exterior cross-section, being arranged at a flow leading-edge area of the ejector nozzle tube. The leading edge nozzle includes a plurality of grooves issuing to the top and bottom sides of the ejector nozzle tube and connecting to an interior of the ejector nozzle tube formed by the hollow profile. An aircraft engine has an optimized oil heat exchanger with at least one oil cooler disposed in a trailing-edge area of an aerofoil-type structure, with at least one flow entrance area being provided to supply ambient air to the oil cooler disposed in a flow duct. The ejector nozzle tube can be arranged downstream of the oil cooler in the flow duct.
Public/Granted literature
- US20110215172A1 Aircraft engine with optimized oil heat exchanger Public/Granted day:2011-09-08
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