发明名称 STARTER SYSTEM AND METHOD FOR AIRCRAFT GAS TURBINE ENGINE
摘要 A turbine engine starter system (10) includes a power source (14) connected with a starter (16) and configured to provide starter power at first and second settings with different voltages. The first setting initiates the start cycle and the second accelerates the engine thrugh the cycle after ignition. A controller (12) connected with the starter monitors the start cycle. The power source may comprise a pair of batteries (14a, 14b).
申请公布号 WO9915402(A3) 申请公布日期 1999.06.10
申请号 WO1998US17381 申请日期 1998.08.20
申请人 PRECISION AIRMOTIVE CORPORATION 发明人 MASSEY, GEORGE
分类号 B64D;F02C7/26;F02C7/268 主分类号 B64D
代理机构 代理人
主权项
地址