Trunnion for high-pressure turbine, and turbojet engine including such a trunnion

Patent metadata

Field	Value
Publication number	US-2016186656-A1
Application number	US-201414897607-A
Country	US
Kind code	A1
Filing date	Jun 11, 2014
Priority date	Jun 12, 2013
Publication date	Jun 30, 2016
Grant date	—

Abstract

The invention relates to a trunnion ( 23 ) for a high-pressure turbine ( 11 ), to be arranged between a shaft of a low-pressure turbine ( 9 ) and an inner surface ( 34 ) of a seal mounting ( 26 ) of the low-pressure turbine ( 8 ), the trunnion ( 23 ) being characterised in that it includes a drop-launching extension ( 32 ) arranged such as to extend opposite a flared portion ( 33 ) of the inner surface ( 34 ) of the seal mounting ( 26 ), such that when the trunnion ( 23 ) is rotated about the shaft of the low-pressure turbine ( 9 ), oil (H 2 ), which tends to penetrate between the trunnion ( 23 ) and the seal mounting ( 26 ), is thrown by centrifugal effect from the drop-launching extension ( 32 ) toward the flared portion ( 33 ) of the inner surface ( 34 ) of the seal mounting ( 26 ).

First claim

1 . A trunnion for high-pressure turbine, intended to be arranged between a low-pressure turbine shaft and an inner surface of a seal support of a low-pressure turbine, the trunnion ( 23 ) comprising a drop-launching extension arranged to extend facing a flared portion of the inner surface of the seal support, such that when the trunnion is driven in rotation around the low-pressure turbine shaft, oil tending to penetrate between the trunnion and the seal support is projected by centrifugal effect from the drop-launching extension towards the flared portion of the inner surface of the seal support, the trunnion further comprising a recess arranged in the outer surface of the trunnion, the recess stopping penetration of the oil between the trunnion and the seal support and causing detachment of the oil towards the inner surface of the seal support by centrifugal effect, wherein the drop-launching extension has an outer surface tilted relative to an axis of rotation of the trunnion, tending to guide the oil towards the recess by centrifugal effect when the trunnion is driven in rotation.

2 . The trunnion according to claim 1 , wherein the recess is an annular groove arranged in the outer surface of the trunnion.

3 . The trunnion according to claim 1 , comprising a series of radial flanges suitable for form a sealing labyrinth between the trunnion and the seal support.

4 . A turbojet engine comprising a low-pressure compressor, a high-pressure compressor, a high-pressure turbine and a low-pressure turbine, the turbojet engine further comprising:
a low-pressure turbine shaft connecting the low-pressure compressor to the low-pressure turbine, a high-pressure compressor shaft extending around the low-pressure turbine shaft, and connecting the high-pressure compressor to the high-pressure turbine, wherein the low-pressure turbine comprises a seal support presenting an inner surface having a flared portion and the high-pressure turbine comprises a trunnion according to claim 1 , disposed between the low-pressure turbine shaft and the inner surface of the seal support of the low-pressure turbine.

5 - 6 . (canceled)

Assignees

• Snecma

Inventors

• Judet Maurice Guy
• Coulombeau Laurent
• Jacques Michel
• Garin Fabrice

Classifications

• F02C3/064 Primary

  the compressor having concentric stages · CPC title

• F02C7/20

  Mounting or supporting of plant; Accommodating heat expansion or creep · CPC title

• F02C7/06

  Arrangements of bearings (bearings F16C); Lubricating ({of turbo machines F01D25/18; of machines or} engines in general F01M) · CPC title

• F02C7/28

  Arrangement of seals · CPC title

• F01D25/183 Primary

  Sealing means · CPC title