发明名称 |
Accessory mounting for a gas turbine |
摘要 |
Accessories are mounted to a gas turbine engine from a frame attached to a pylon which is used to mount the engine to an airframe. The frame independently mounts the accessories so that engine vibrations are not transmitted to the accessories. |
申请公布号 |
US9416734(B2) |
申请公布日期 |
2016.08.16 |
申请号 |
US201213713933 |
申请日期 |
2012.12.13 |
申请人 |
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG |
发明人 |
Thies Robert;Buchholz Carsten;Staudte Andreas |
分类号 |
F02C7/22;F02C7/32;F02C7/20 |
主分类号 |
F02C7/22 |
代理机构 |
Oliff PLC |
代理人 |
Oliff PLC |
主权项 |
1. An engine assembly for an aircraft, comprising:
an engine having a front mounting location for mounting the engine to the aircraft; and a frame supporting at least one accessory, the frame having a pair of forward struts, each strut of the pair of forward struts having a first end adjacent the front mounting location and a second end remote from the front mounting location, each strut within the pair of forward struts passing the engine on opposing sides, wherein the at least one accessory is mounted at the second end of the pair of forward struts, the pair of forward struts providing a direct load path between the accessory and the front mounting location of the engine. |
地址 |
Blankenfelde-Mahlow DE |