|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/796; 060/797; 060/226.1; 244/054; 248/554; 248/555; 415/191; 415/211.2; 415/220|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 13|
A coupling assembly for an engine core of a turbomachine is provided. The coupling assembly comprises a duct having a substantially circular shape and surrounding the engine core, and a plurality of coupling struts, each coupling strut extending only in a substantially vertical direction relative to the direction of gravity when the engine core is at a rest position with zero pitch and zero roll, each of the plurality of coupling struts coupling the engine core to the duct.
1. A coupling assembly for coupling an engine core of a turbomachine to the side of an aircraft, the coupling assembly comprising: a duct having a substantially circular shape and surrounding the engine core;a forward frame coupled to the duct and a forward portion of the engine core, the forward frame configured to bend with respect to the body of the aircraft in a horizontal direction when the engine core is operating under thrust-induced loads; anda plurality of coupling struts coupling the engine core to the duct and positioned around a rear portion ...