发明名称 ALTITUDE GAS TURBINE ENGINE TEST CELL
摘要 <p>The test cell has a pressure recovery pipe (26) receiving air from the tested engine (14). Excess air is inherently induced into the pipe. A source flow path for this excess air is provided from within the pipe (36) back to the entrance of the pipe passing through a perforated bulkhead (30). High local velocities of the recirculating air, resulting variable static pressures on the engine and uncertainty in the thrust measurement are avoided.</p>
申请公布号 WO1995008103(A1) 申请公布日期 1995.03.23
申请号 US1994010408 申请日期 1994.09.15
申请人 发明人
分类号 主分类号
代理机构 代理人
主权项
地址