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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0475877 (1999-12-30) |
발명자 / 주소 |
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출원인 / 주소 |
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인용정보 | 피인용 횟수 : 3 인용 특허 : 4 |
Accordingly, the present invention provides a ducting system for use on a gas turbine engine having two fans connected to a common shaft, and includes a primary inlet duct that is integral with a plurality of primary discharge ducts, a plurality of secondary inlet ducts that are integral with a seco
1. A ducting system for use on a gas turbine engine having two fans connected to a common shaft, said ducting system comprising:a primary inlet duct and a plurality of primary discharge ducts, each of said primary discharge ducts is integral with said primary duct, said primary inlet duct having a c
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