Gas turbine engine

US11840960B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11840960-B2
Application numberUS-202117799004-A
CountryUS
Kind codeB2
Filing dateFeb 12, 2021
Priority dateFeb 14, 2020
Publication dateDec 12, 2023
Grant dateDec 12, 2023

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  1. Title

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  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A gas turbine engine including a compressor that compresses air taken in; a combustor that sprays a fuel into the compressed air and combusts the fuel; a turbine rotated by energy of the combustion gas generated by the combustor; a rotating shaft coupling the compressor and the turbine; a rear bearing that is a cageless ball bearing including an inner race, an outer race, and a ball, the inner race being fixed to a portion of the rotating shaft which portion is close to the turbine; a housing to which the rear bearing is attached; and a rear bearing holding member that is interposed between the rear bearing and the housing and holds the outer race of the rear bearing such that the outer race of the rear bearing is movable in an axial direction relative to the housing.

First claim

Opening claim text (preview).

The invention claimed is: 1. A gas turbine engine comprising: a compressor that compresses air which has been taken in; a combustor that sprays a fuel to the air compressed by the compressor and combusts the fuel; a turbine that is rotated by energy of a combustion gas generated by the combustor; a rotating shaft that couples the compressor and the turbine; a rear bearing that is a cageless ball bearing including an inner race, an outer race, and a ball, the inner race being fixed to a portion of the rotating shaft which portion is close to the turbine; a housing to which the rear bearing is attached; and a rear bearing holding member that is interposed between the rear bearing and the housing, is fixed to the housing, holds the outer race of the rear bearing such that the outer race of the rear bearing is movable in an axial direction relative to the rear bearing holding member, and therefore, holds the outer race of the rear bearing such that the outer race of the rear bearing is movable in the axial direction relative to the housing. 2. The gas turbine engine according to claim 1 , further comprising a front bearing including an inner race, an outer race, and a ball, the inner race being fixed to a portion of the rotating shaft which portion is close to the compressor, the outer race being fixed to the housing so as not to be movable in the axial direction relative to the housing. 3. The gas turbine engine according to claim 1 , wherein the rear bearing holding member holds the outer race of the rear bearing such that the rear bearing is movable in a radial direction relative to the housing. 4. The gas turbine engine according to claim 3 , wherein a portion of the rear bearing holding member which portion holds the outer race of the rear bearing is movable in the radial direction relative to the housing while attenuating vibration of the rear bearing. 5. The gas turbine engine according to claim 3 , wherein: the rear bearing holding member includes an elastic member that is elastically deformable in the axial direction and the radial direction relative to the housing; and the rear bearing holding member holds the rear bearing through the elastic member. 6. The gas turbine engine according to claim 1 , wherein the rear bearing is a ceramic bearing in which the inner race, the outer race, and the ball are made of ceramics or a hybrid bearing in which the inner race and the outer race are made of metal, and the ball is made of ceramics. 7. The gas turbine engine according to claim 1 , further comprising a non-circulation lubricator that injects lubricating oil to the rear bearing.

Assignees

Inventors

Classifications

  • Ceramic matrix composites [CMC] · CPC title

  • F02C7/06Primary

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

  • Arrangement of bearings; Supporting or mounting bearings in casings (bearings per se F16C) · CPC title

  • Lubricating arrangements (of machines or engines in general F01M) · CPC title

  • in gas turbines · CPC title

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Frequently asked questions

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What does patent US11840960B2 cover?
A gas turbine engine including a compressor that compresses air taken in; a combustor that sprays a fuel into the compressed air and combusts the fuel; a turbine rotated by energy of the combustion gas generated by the combustor; a rotating shaft coupling the compressor and the turbine; a rear bearing that is a cageless ball bearing including an inner race, an outer race, and a ball, the inner …
Who is the assignee on this patent?
Kawasaki Heavy Ind Ltd
What technology area does this patent fall under?
Primary CPC classification F02C7/06. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Dec 12 2023 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).