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公开(公告)号：EP1687200A2
公开(公告)日：2006-08-09
申请号：EP04810203.2
申请日：2004-11-01
IPC分类号： B63H1/00
CPC分类号： B64C11/003 , A63H27/02 , B64C11/04 , B64C11/14 , B64C11/28 , B64C39/024 , B64C2201/044 , B64C2201/082 , B64C2201/102 , B64C2201/165 , B64C2201/182 , B64C2201/201 , B64C2201/206 , B64D41/007 , F02K5/023 , F05D2260/85 , Y02T50/44 , Y02T50/672
摘要： Methods and systems for starting propeller driven aircraft and other devices are disclosed. A system in accordance with one embodiment of the invention includes a removable fixture that is coupled to the propeller and has at least one portion exposed to a flowstream to rotate the propeller during engine start-up. The fixture is configured to separate from the propeller after the engine begins to turn over (e.g., after the engine starts and/or rotates above a threshold rate). Accordingly, the system can include a releasable link between the fixture and the propeller.
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公开(公告)号：EP1965053B1
公开(公告)日：2013-01-30
申请号：EP08250714.6
申请日：2008-03-03
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公开(公告)号：EP1965053A2
公开(公告)日：2008-09-03
申请号：EP08250714.6
申请日：2008-03-03
发明人： Schwarz, Frederick M. , Fentress, Brian M. , Berryann, Andrew P. , Lents, Charles E. , Glahn, Jorn A.
IPC分类号： F02C6/08
摘要： An engine combination (10) for generating forces with a gas turbine engine (14) generating force, and an internal combustion engine (34) provided in the combination (10) as an intermittent combustion engine (34) generating force having an air intake (32), there being an air transfer duct (30) connected from a compressor (21,23) in the gas turbine engine (14) to the air intake (32) to transfer compressed air thereto.
摘要翻译： 一种用于与产生力的燃气涡轮发动机（14）产生力的发动机组合（10）和设置在所述组合（10）中的作为产生具有进气口的力的间歇式内燃机（34）的内燃机（34） 32），存在从燃气涡轮发动机（14）中的压缩机（21,23）连接到进气口（32）的空气传送管道（30），以将压缩空气传送到其上。
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公开(公告)号：EP1965053A3
公开(公告)日：2010-11-24
申请号：EP08250714.6
申请日：2008-03-03
发明人： Schwarz, Frederick M. , Fentress, Brian M. , Berryann, Andrew P. , Lents, Charles E. , Glahn, Jorn A.
IPC分类号： F02C6/08
摘要： An engine combination (10) for generating forces with a gas turbine engine (14) generating force, and an internal combustion engine (34) provided in the combination (10) as an intermittent combustion engine (34) generating force having an air intake (32), there being an air transfer duct (30) connected from a compressor (21,23) in the gas turbine engine (14) to the air intake (32) to transfer compressed air thereto.
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