Suspension part of a turbojet engine
원문보기
IPC분류정보
국가/구분 |
United States(US) Patent
등록
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국제특허분류(IPC7판) |
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출원번호 |
US-0450701
(2001-12-20)
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우선권정보 |
FR-00 16734(2000-12-21) |
국제출원번호 |
PCT/FR01/004088
(2001-12-20)
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§371/§102 date |
20031229
(20031229)
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국제공개번호 |
WO02/049914
(2002-06-27)
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발명자
/ 주소 |
- Brefort,Fran챌ois
- Chevalier,Lydie
- Picard,Jean Louis
- Pasquer,Jean Claude F챕lix
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출원인 / 주소 |
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대리인 / 주소 |
Oblon, Spivak, McClelland, Maier &
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인용정보 |
피인용 횟수 :
6 인용 특허 :
10 |
초록
▼
A suspension part for mounting a turbojet engine includes two ends equipped with two elements, juxtaposed in a widthwise direction of the suspension part, for fixing the suspension part to the fixed structure. The ends are shaped into pairs of yokes respectively flanking connecting rods and each in
A suspension part for mounting a turbojet engine includes two ends equipped with two elements, juxtaposed in a widthwise direction of the suspension part, for fixing the suspension part to the fixed structure. The ends are shaped into pairs of yokes respectively flanking connecting rods and each including fixing elements and a bearing of a journal of a connecting rod which bearing is situated underneath a fixing element. The suspension part also includes slots passing through the two ends of the suspension part and running between the yokes without running over a central portion of the suspension part. Each of the yokes has an upper portion with an additional thickness located on an inside of each of the yokes.
대표청구항
▼
What is claimed is: 1. A suspension part for mounting a turbojet engine to a fixed structure, said suspension part comprising: at least two connecting rods; and two ends equipped with two fixing elements, juxtaposed in a widthwise direction of the suspension part, the ends being shaped into pairs
What is claimed is: 1. A suspension part for mounting a turbojet engine to a fixed structure, said suspension part comprising: at least two connecting rods; and two ends equipped with two fixing elements, juxtaposed in a widthwise direction of the suspension part, the ends being shaped into pairs of yokes respectively flanking the connecting rods and each comprising one of the fixing elements and a drilling for a journal of a connecting rod, the drilling being situated underneath said fixing element, wherein slots passing through the two ends of the suspension part run between the yokes without running over a central portion of the suspension part, and each of said yokes has an upper portion with an additional thickness located on an inside of each of said yokes. 2. The suspension part as claimed in claim 1, wherein the yokes are thicker at the fixing elements than said yokes are at the drillings for the journal. 3. The suspension part as claimed in claim 1, wherein said additional thickness is located over the connecting rods. 4. The suspension part as claimed in claim 1, wherein each of said slots is narrower than a shortest distance between said yokes. 5. The suspension part as claimed in claim 1, wherein each of said yokes has a bottom portion located under said upper portion and configured to support said connecting rods. 6. The suspension part as claimed in claim 1, wherein each of said slots runs toward said central portion at least as far as the ends of the yokes. 7. The suspension part as claimed in claim 1, wherein each of said slots ends with an opening which is larger than other portions of the slots. 8. The suspension part as claimed in claim 1, further comprising ribs configured to connect corresponding yokes together, said corresponding yokes being positioned at opposite ends of said suspension part. 9. The suspension part as claimed in claim 8, wherein each of said ribs has an arch shape with a thinner portion under said central portion arid a thicker portion toward said yokes. 10. A suspension part for mounting an engine to a fixed structure, said suspension part comprising: at least two fixation elements positioned at each end of said suspension part; a pair of yokes at each end of said suspension part, each yoke comprising an upper portion located under one of said fixation element and a lower portion located under said upper portion, wherein a distance between inner faces of the upper portions for two yokes of said pair of yokes at a same end of the suspension part is shorter than a distance between inner faces of corresponding lower portions for said two yokes at said same end; and at least two slots, each slot passing through one of the ends of said suspension part and between two of said yokes without reaching a central portion of the suspension part. 11. The suspension part as claimed in claim 10, further comprising at least two connecting rods, each connecting rod being connected to a pair of said yokes. 12. The suspension part as claimed in claim 11, wherein said connecting rods are configured to be articulated to said engine. 13. The suspension part as claimed in claim 11, wherein said connecting rods are connected to said yokes below said upper portions of said yokes. 14. The suspension part as claimed in claim 13, wherein said connecting rods are connected to said yokes at said lower portions. 15. The suspension part as claimed in claim 14, wherein said slots define openings which are narrower than said distance between said inner faces of said corresponding lower portions. 16. The suspension part as claimed in claim 15, wherein said slots define openings which are narrower than said distance between said inner faces of said upper portions. 17. The suspension part as claimed in claim 14, wherein said upper portions are thicker than said lower portions. 18. The suspension part as claimed in claim 10, wherein each of said slots ends with an opening which is larger than other portions of the slots. 19. The suspension part as claimed in claim 10, further comprising ribs configured to connect corresponding yokes together, said corresponding yokes being positioned at opposite ends of said suspension part. 20. The suspension part as claimed in claim 19, wherein each of said ribs has an arch shape with a thinner portion under said central portion and a thicker portion toward said yokes.
이 특허에 인용된 특허 (10)
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Le Blaye Sebastien,FRX, Attachment device for an aircraft engine.
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Jule Pascal FR; Alain Porte FR; Stephane Levert FR, Device for attaching an aircraft engine.
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Levert, Stephane; Roszak, Sebastien, Device for the attachment of an engine to an aircraft.
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Langley Kenneth R. (Wotton-under-Edge GB2) Treby John M. (Bristol GB2) Fox Derek H. C. (Bristol GB2) Short Malcolm (Bristol GB2), Failure tolerant engine mounting.
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Brefort, François; Huet, Patrick; Pasquer, Félix, Jet engine suspension.
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Gwinn John J. (Erie PA) Schmidt Warren E. (Erie PA) Downing Marshall W. (Chambourcy FRX), Mounting for engines and the like.
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Pachomoff Guy R. (Corbeil Essonnes FRX), Rear hanging structure for a turbojet engine.
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Demouzon Fran.cedilla.is Michel,FRX ; Fer Rene Pierre,FRX ; Huet Patrick Jean Alibert,FRX ; Marnas Laurent Pierre Elysee Gaston,FRX, Redundant front suspension system for a turboshaft engine.
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Demouzon Francis Michel,FRX ; Fer Rene Pierre,FRX ; Alibert Huet Patrick Jean,FRX ; Marnas Laurent Pierre Elysee Gaston,FRX, Redundant front suspension system for a turboshaft engine.
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Schnelz James R. ; Powell Donald T., Tuned engine mounting system for jet aircraft.
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Martinou, Jean-Marc; Berjot, Michael, Aircraft engine attachment pylon having a rear engine attachment provided with a self-locking nut.
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Journade, Frederic; Bouchet, Eric; Grosseau, Nicolas; Mutin, Antoine, Aircraft engine mount comprising at least one transverse nut and aircraft comprising the said engine mount.
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Machado,St��phane; Cassagne,J��r��me; Del Blanco,Anthony; Martin,Yvon; Chambreuil,Arnaud, Engine mounting structure under an aircraft wing.
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Zameroski, Daniel, Helicopter engine mounting system and methods.
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Dron, Sebastien; Guibert, Thibaut; Prudhomme, Gregory; Tesniere, Marc Patrick, Suspension for suspending a jet engine on an aircraft strut.
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Dron, Sebastien; Fontenoy, Gilles Lucien; Tesniere, Marc Patrick, Suspension for suspending a turbine engine from the structure of an aircraft.
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