|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F16M-001/00 F16M-003/00 F16M-005/00 F16M-007/00 F16M-009/00 F02C-007/20 F04D-029/44 F04D-029/54|
|미국특허분류(USC)||248/637; 060/796; 415/189|
|§371/§102 date||20101206 (20101206)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 4 인용 특허 : 7|
A structural frame for a turbomachine, such as an intermediate frame or an exhaust frame, the frame including at least two coaxial rings, an inner ring and an outer ring, together with radial arms interconnecting the rings. At least one of these elements includes a plurality of parts that are fastened together by bolting.
1. A structural frame, an intermediate frame, or an exhaust frame, for a turbomachine, comprising: inner and outer coaxial rings; andradial arms interconnecting the rings, each of the radial arms comprising a soleplate at an end of the radial arm, the soleplate extending circumferentially and including first and second radial flanges disposed at first and second circumferential ends of the soleplate and extending axially from an upstream end to a downstream end of the sole plate, an upstream wall disposed at an upstream end of the soleplate and extending...