IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0672101
(2008-06-16)
|
등록번호 |
US-8631640
(2014-01-21)
|
우선권정보 |
FR-07 05889 (2007-08-20) |
국제출원번호 |
PCT/FR2008/000834
(2008-06-16)
|
§371/§102 date |
20100204
(20100204)
|
국제공개번호 |
WO2009/027591
(2009-03-05)
|
발명자
/ 주소 |
- Rouyer, Pascal Gerard
- Lesteven, Emmanuel
|
출원인 / 주소 |
|
대리인 / 주소 |
|
인용정보 |
피인용 횟수 :
1 인용 특허 :
6 |
초록
▼
The present invention relates to a jet engine nacelle comprising a forward air inlet section, a mid-section intended to surround a jet engine fan, and an aft section equipped with at least one thrust reversal system comprising, on the one hand, means for deflecting at least part of an air flow of th
The present invention relates to a jet engine nacelle comprising a forward air inlet section, a mid-section intended to surround a jet engine fan, and an aft section equipped with at least one thrust reversal system comprising, on the one hand, means for deflecting at least part of an air flow of the jet engine and, on the other hand, at least one cowl (12) mounted translatably along at least one guide rail (15) in a direction substantially parallel to a longitudinal axis of the nacelle, said movable cowl being able to switch alternately from a closed position, in which it provides the nacelle with aerodynamic continuity and covers the deflection means, to an open position in which it opens a passage in the nacelle and uncovers said deflection means, the nacelle being characterized in that the aft section is equipped with at least one stud (18) mounted such that it can move over a fixed structure of the aft section in the region of the guide rail between a retracted position, in which said stud is withdrawn from the running track of the rail and allows a translational movement of the movable cowl, and an engaged position, in which it forms a stop capable of preventing the movable cowl from sliding in the downstream direction of the nacelle.
대표청구항
▼
1. A nacelle for a jet engine, comprising a forward air inlet section, a mid-section intended to surround a jet engine fan, and an aft section equipped with at least one thrust reversal system, comprising: means for deflecting at least part of an air flow of the jet engine, and,at least one cowl mou
1. A nacelle for a jet engine, comprising a forward air inlet section, a mid-section intended to surround a jet engine fan, and an aft section equipped with at least one thrust reversal system, comprising: means for deflecting at least part of an air flow of the jet engine, and,at least one cowl mounted translatably along at least one guide rail, in a direction substantially parallel to a longitudinal axis of the nacelle, the movable cowl being able to switch alternately from a closed position in which the cowl provides the nacelle with aerodynamic continuity, and covers the deflection means, to an open position in which the cowl opens a passage in the nacelle and uncovers the deflection means,wherein the aft section is equipped with at least one mechanical inhibition stud being movably mounted on a fixed structure of the aft section in a region of the guide rail such that the stud can move between a retracted position in which the stud is withdrawn from a running track of the guide rail, and allows translation of the movable cowl, and an engaged position, in which the stud forms a stop capable of preventing the movable cowl from sliding in a downstream direction of the nacelle,wherein the movable mechanical inhibition stud is equipped with manual activation means comprising a system of rocker bars. 2. A nacelle as claimed in claim 1, wherein the mechanical inhibition stud is fitted such as to be movable on a sliding plane of the rail, and perpendicularly to the latter. 3. A nacelle as claimed in claim 1, wherein the movable mechanical inhibition stud is equipped with electrical activation device. 4. A nacelle as claimed in claim 1, wherein the movable mechanical inhibition stud is associated with means for indication of a state of engagement and/or retraction. 5. A nacelle as claimed in claim 1, wherein the mechanical inhibition stud has a surface of contact which is substantially flat in relation to the rail. 6. A nacelle as claimed in claim 5, wherein the contact surface of the mechanical inhibition stud matches a profile of the rail. 7. A nacelle as claimed in claim 1, wherein at least one mechanical inhibition stud is fitted on a lower longitudinal beam of the aft section. 8. A nacelle as claimed in claim 1, further comprising two semi-cylindrical movable cowls. 9. A nacelle as claimed in claim 8, wherein the cowls can be mechanically connected to one another. 10. A nacelle as claimed in claim 1, wherein the movable mechanical inhibition stud is fitted on a fixed structure of the aft section by means of a drive system comprising at least one connecting rod which is fitted such as to pivot on the said fixed structure.
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