发明名称 MULTIPLE POWER ASSURANCE CHECK PROCEDURE FOR AIRCRAFT WITH AN ENGINE INLET BARRIER FILTER INSTALLED
摘要 A method of conducting an engine power assurance check includes performing a first engine power assurance check wherein the first engine power assurance check is judged as passing or failing based on power performance values calculated assuming the presence of a substantially clogged or blocked inlet barrier filter and in response to a fail result of the first engine power assurance check, performing a second engine power assurance check wherein the second power assurance check is judged as passing or failing based on power performance values calculated assuming at least one of no inlet barrier filter being installed and an open bypass of an installed inlet barrier filter.
申请公布号 US2016347479(A1) 申请公布日期 2016.12.01
申请号 US201615167886 申请日期 2016.05.27
申请人 Bell Helicopter Textron Inc. 发明人 O'Neil Joshua Robert;Peryea Martin;Birkenheuer Andrew Jordan
分类号 B64F5/00;B64D43/00 主分类号 B64F5/00
代理机构 代理人
主权项 1. A method of conducting an engine power assurance check, comprising: performing a first engine power assurance check wherein the first engine power assurance check is judged as passing or failing based on power performance values calculated assuming the presence of a substantially clogged or blocked inlet barrier filter; and in response to a fail result of the first engine power assurance check, performing a second engine power assurance check wherein the second power assurance check is judged as passing or failing based on power performance values calculated assuming at least one of no inlet barrier filter being installed and an open bypass of an installed inlet barrier filter.
地址 Fort Worth TX US