IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0103716
(2002-03-25)
|
우선권정보 |
FR-0005194 (2001-04-17) |
발명자
/ 주소 |
- Andre, Robert
- Porte, Alain
|
출원인 / 주소 |
|
인용정보 |
피인용 횟수 :
12 인용 특허 :
7 |
초록
▼
An air inlet cowl for a jet engine, particularly an aeroengine, includes a leading edge deicer, a hollow leading edge defining an internal peripheral chamber, closed by a first internal partition, and an exhaust orifice, in the leading edge, connecting the internal chamber with the outside. The cowl
An air inlet cowl for a jet engine, particularly an aeroengine, includes a leading edge deicer, a hollow leading edge defining an internal peripheral chamber, closed by a first internal partition, and an exhaust orifice, in the leading edge, connecting the internal chamber with the outside. The cowl further includes a pressurized hot air feedpipe for being connected, at its rear end away from the leading edge and passing through a second internal partition, to a pressurized hot air circuit and, at its front end toward the leading edge, to an injector of pressurized hot air into the internal chamber, a protective internal casing functioning with the first and second internal partitions to define an isolation volume enclosing the feedpipe, and an air extraction opening, in the first partition, to place the isolation volume in communication with the internal peripheral chamber. The area of this extraction opening is such that, in the event of damage to the feedpipe, the elimination of pressurized hot air in the isolation volume does not impair the protective internal casing and the injector injects into the internal chamber a pressurized hot air flow rate at least equal to 50% of the hot air flow rate in the feedpipe.
대표청구항
▼
1. An air inlet cowl for a jet engine, particularly an aeroengine, said air inlet cowl being provided with means for deicing its leading edge, and comprising: a hollow leading edge delimiting an internal peripheral chamber, closed by a first internal partition; at least one exhaust orifice placi
1. An air inlet cowl for a jet engine, particularly an aeroengine, said air inlet cowl being provided with means for deicing its leading edge, and comprising: a hollow leading edge delimiting an internal peripheral chamber, closed by a first internal partition; at least one exhaust orifice placing said internal chamber in communication with the outside and made in said hollow leading edge; a pressurized hot air feedpipe capable of being connected, at its rear end away from said leading edge and passing through a second internal partition, to a pressurized hot air circuit and, at its front end toward said leading edge, to an injector injecting said pressurized hot air into said internal chamber of the leading edge; a protective internal casing collaborating with said first and second internal partitions to delimit an isolation volume enclosing said feedpipe; and an air extraction opening made in said first partition to place said isolation volume enclosing said feedpipe in communication with said internal peripheral chamber of said leading edge, the area of this extraction opening being chosen from a range of values such that, in the event of damage to said hot air feedpipe: the elimination of pressurized hot air in said isolation volume is not detrimental to said protective internal casing; and the injector injects into said internal chamber a pressurized hot air flow rate at least equal to 50% of the hot air flow rate in said feedpipe. 2. The air inlet cowl as claimed in claim 1, which comprises, inside said internal peripheral chamber of the leading edge, a deflector capable of deflecting the hot air passing through said air extraction opening in the same direction as the hot air injected by said injector. 3. The air inlet cowl as claimed in claim 1, wherein said air extraction opening is formed of a single orifice. 4. The air inlet cowl as claimed in claim 1, wherein said air extraction opening is formed of a number of orifices. 5. The air inlet cowl as claimed in claim 1, wherein said air extraction opening is away from said feedpipe. 6. The air inlet cowl as claimed in claim 1, wherein said air extraction opening surrounds said feedpipe. 7. The air inlet cowl as claimed in claim 1, wherein said protective internal casing collaborates in addition with the internal face of the external wall of said cowl to delimit said isolation volume enclosing said feedpipe. 8. The air inlet cowl as claimed in claim 1, wherein said protective internal casing delimits, with said feedpipe, an isolation volume of annular cross section.
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