发明名称 Aircraft combination engines plural airflow conveyances system
摘要 An engine combination for generating forces with a gas turbine engine generating force, and an internal combustion engine provided in the combination as an intermittent combustion engine generating force having an air intake, there being a plurality of air transfer ducts each extending from a different location in the gas turbine engine so as to be capable to provide air in each of those air transfer ducts at one end thereof at pressures differing from one another and connected at the other end of each to the air intake to transfer air thereto.
申请公布号 US8015795(B2) 申请公布日期 2011.09.13
申请号 US20070804429 申请日期 2007.05.18
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SCHWARZ FREDERICK M.;FENTRESS BRIAN M.
分类号 F02K3/00;F02K7/00;F02K9/00;F02K99/00 主分类号 F02K3/00
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