Invention Grant
US08480032B2 Aircraft de-icing device and engine nacelle of an aircraft gas turbine with de-icing device
有权
具有除冰装置的飞机燃气轮机的飞机除冰装置和发动机舱
- Patent Title: Aircraft de-icing device and engine nacelle of an aircraft gas turbine with de-icing device
- Patent Title (中): 具有除冰装置的飞机燃气轮机的飞机除冰装置和发动机舱
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Application No.: US12939609Application Date: 2010-11-04
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Publication No.: US08480032B2Publication Date: 2013-07-09
- 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: DE102009055879 20091126
- Main IPC: B64D15/02
- IPC: B64D15/02
Abstract:
An aircraft de-icing device and an engine nacelle of an aircraft gas turbine is provided with a de-icing device, with the engine nacelle 1 in the inflow area being provided with an annular air duct 2, into which heated air is introduced. At least one oil cooler 3 is arranged in the engine nacelle 1, to which engine oil is fed and which is supplied with ambient air, with the heated airflow leaving the oil cooler 3 being passed through the air duct 2.
Public/Granted literature
- US20110121136A1 AIRCRAFT DE-ICING DEVICE AND ENGINE NACELLE OF AN AIRCRAFT GAS TURBINE WITH DE-ICING DEVICE Public/Granted day:2011-05-26
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