|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/2261 ; 60/3932|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 49 인용 특허 : 2|
A ducted fan gas turbine powerplant is mounted to aircraft structure via a single plane mounting which comprises a single peripheral array of struts which connect the core gas generator, the fan cowl and the aircraft structure. The structure which connects the struts to the core gas generator is extended downstream of the array of struts and terminates in a plain bearing. A downstream portion of the core gas generator includes a cylindrical portion which is in sliding engagement with the plain bearing, so that radial forces generated by the movement arm,...
A ducted fan gas turbine powerlant including a unitary structure comprising a plurality of mounting struts affixed by their radially inner ends to an annular strengthened outer casing portion of a core gas generator of the powerplant in peripheral alignment thereon and extending radially across the fan duct, a box structure which incorporates the radially outer ends of the struts and is fastened to aircraft structure so as to transmit powerplant loads via said struts to said aircraft structure and wherein the improvement comprises an annular portion of t...