Detachable anti-wear cap for rectifier sector

US10830079B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10830079-B2
Application numberUS-201816174531-A
CountryUS
Kind codeB2
Filing dateOct 30, 2018
Priority dateOct 31, 2017
Publication dateNov 10, 2020
Grant dateNov 10, 2020

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  1. Title

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  2. Abstract

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  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.

An assembly including a sector of fixed blades for turbomachine distributor including at one circumferential end a protuberance and at another circumferential end a contact surface, such that the protuberance of a sector arrives opposite the contact surface of another adjacent sector, a detachable cap including a surface with anti-wear material, configured to be engaged detachably on the protuberance of the sector, such that the anti-wear material is in contact with the contact surface of the other sector.

First claim

Opening claim text (preview).

The invention claimed is: 1. An assembly comprising: a sector of fixed blades for a turbomachine distributor comprising a protuberance at one circumferential end and a contact surface at another circumferential end a, such that the protuberance of a sector arrives opposite the contact surface of another adjacent sector, and a detachable cap comprising a surface with antiwear material, configured to be engaged detachably on the protuberance of the sector such that the cap envelopes the protuberance and such that the antiwear material is in contact with the contact surface of the other sector. 2. The assembly according to claim 1 , wherein the sector comprises an internal platform comprising an upper plate, on which are fixed the fixed blades and a lower plate, connected to the upper plate by a spacer. 3. The assembly according to claim 2 , wherein the protuberance and the contact surface are at the circumferential ends of the upper plate or of the lower plate. 4. The assembly according to claim 1 , wherein the anti-wear material is in a form of a wafer which defines the surface. 5. The assembly according to claim 1 , wherein the cap is made entirely of anti-wear material. 6. The assembly according to claim 1 , wherein the anti-wear material comprises cobalt or an alloy of cobalt. 7. The assembly according to claim 1 , wherein the cap is in a form of a block comprising a blind recess forming a cavity suitable for receiving the protuberance, such that the protuberance is enveloped by the cap. 8. The assembly according to claim 1 , wherein the contact surface comprises anti-wear material. 9. A portion of turbomachine distributor comprising at least two assemblies according to claim 1 , defining first and second sectors, wherein the protuberance of the first sector comprises the detachable cap put in place, the detachable cap being engaged with the contact surface of the second sector. 10. A distributor comprising a plurality of portions according to claim 9 , the portions being placed end to end. 11. An assembly comprising: a sector of fixed blades for a turbomachine distributor comprising a protuberance at one circumferential end and a contact surface at another circumferential end, such that the protuberance of a sector arrives opposite the contact surface of another adjacent sector, and a detachable cap comprising a surface with anti-wear material, configured to be engaged detachably on the protuberance of the sector, such that the anti-wear material is in contact with the contact surface of the other sector, wherein the cap is in a form of a block comprising a blind recess forming a cavity suitable for receiving the protuberance, such that the protuberance is enveloped by the cap.

Assignees

Inventors

Classifications

  • F01D5/225Primary

    by shrouding · CPC title

  • Nozzle boxes · CPC title

  • using positioning or alignment devices for aligning or centring, e.g. pins · CPC title

  • Preventing or minimising internal leakage of working-fluid, e.g. between stages (sealings in general F16J {; sealing arrangements for transition ducts of combustor cans F01D9/023}) · CPC title

  • forming ring or sector · CPC title

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Frequently asked questions

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What does patent US10830079B2 cover?
An assembly including a sector of fixed blades for turbomachine distributor including at one circumferential end a protuberance and at another circumferential end a contact surface, such that the protuberance of a sector arrives opposite the contact surface of another adjacent sector, a detachable cap including a surface with anti-wear material, configured to be engaged detachably on the protub…
Who is the assignee on this patent?
Safran Aircraft Engines
What technology area does this patent fall under?
Primary CPC classification F01D5/225. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Nov 10 2020 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 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).