Method for assembling a nozzle and an exhaust case of a turbomachine

US9399952B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9399952-B2
Application numberUS-201313974849-A
CountryUS
Kind codeB2
Filing dateAug 23, 2013
Priority dateAug 27, 2012
Publication dateJul 26, 2016
Grant dateJul 26, 2016

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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.

A method for assembling a nozzle and an exhaust case of a turbomachine is disclosed. The exhaust case includes a hub and an outer ferrule connected to each other by a plurality of arms. The nozzle is attached to the outer ferrule of the exhaust case substantially at the trailing edges of the arms.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method of assembling a nozzle and an exhaust case of a turbomachine, the exhaust case including a hub and an outer ferrule connected to each other by a plurality of arms, the method comprising: attaching the nozzle to the outer ferrule of the exhaust case in a same radial part of the turbomachine as that containing trailing edges of the arms of the exhaust case, wherein the attaching of the nozzle to the exhaust case is performed at least partly through radial attachment flanges carried by nozzle and the outer ferrule of the exhaust case, respectively, each including ports through which radial bolted joints pass, the ports and the radially bolted joints presenting an axis extending radially, wherein the axis of ports and the radially bolted joints is perpendicular to an axis of the turbo machine, and wherein an axial location of the trailing edges of the arms overlaps at least one of the radial attachment flanges carried by the nozzle and the outer ferrule of the exhaust case. 2. The method according to claim 1 , wherein the attachment of the nozzle to the exhaust case is performed at least partly through axial attachment flanges carried by the nozzle and the outer ferrule of the exhaust case respectively, using axial bolted joints. 3. The method according to claim 1 , wherein the nozzle includes a mixer, the attachment being performed through the mixer. 4. The method according to claim 1 , wherein at least one of the attachment flange of the outer ferrule or the attachment flange of the nozzle is scalloped. 5. The method according to claim 4 , wherein the attachment flanges of the outer ferrule and of the nozzle are secured together by bolted joints, and a scalloping is performed between each bolted joint. 6. An exhaust system of a turbomachine comprising: a nozzle; and an exhaust case, the exhaust case including a hub and an outer ferrule connected to each other by a plurality of arms, wherein the nozzle is attached to the outer ferrule of the exhaust case in a same radial part of the turbomachine as that containing trailing edges of the arms of the exhaust case, wherein the nozzle is attached to the exhaust case at least partly through radial attachment flanges carried by the nozzle and the outer ferrule of the exhaust case, respectively, each including ports through which radial bolted joints pass, the ports and the radially bolted joints present an axis extending radially, wherein an axis of ports and the radially bolted joints is perpendicular to an axis of the turbo machine, and wherein an axial location of the trailing edges of the arms overlaps at least one of the radial attachment flanges carried by the nozzle and the outer ferrule of the exhaust case. 7. The exhaust system according to claim 6 , wherein the nozzle is attached to the exhaust case at least partly through axial attachment flanges carried by the nozzle and the outer ferrule of the exhaust case respectively, using axial bolted joints. 8. The turbomachine comprising the nozzle and the exhaust case assembled by implementing the method according to claim 1 . 9. The turbomachine comprising the exhaust system according to claim 6 .

Assignees

Inventors

Classifications

  • F02K1/80Primary

    Couplings or connections · CPC title

  • Flange connections; Bolting arrangements (F01D25/265 takes precedence) · CPC title

  • Assembly methods · CPC title

  • Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids (see also F01D25/16, F01D25/24 and F01D25/26) · CPC title

  • Exhaust heads, chambers, or the like · CPC title

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Frequently asked questions

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What does patent US9399952B2 cover?
A method for assembling a nozzle and an exhaust case of a turbomachine is disclosed. The exhaust case includes a hub and an outer ferrule connected to each other by a plurality of arms. The nozzle is attached to the outer ferrule of the exhaust case substantially at the trailing edges of the arms.
Who is the assignee on this patent?
Snecma
What technology area does this patent fall under?
Primary CPC classification F02K1/80. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jul 26 2016 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).