Turbine engine with a combustion chamber outer flange of sandwich type

Patent metadata

Field	Value
Publication number	US-9988982-B2
Application number	US-201514629840-A
Country	US
Kind code	B2
Filing date	Feb 24, 2015
Priority date	Feb 27, 2014
Publication date	Jun 5, 2018
Grant date	Jun 5, 2018

Abstract

A turbine engine has inner and outer annular covers containing an annular combustion chamber and an annular nozzle. The combustion chamber is held in position inside the outer annular cover between two radial holder rings that are nested at least in part one within the other and that have their radially outer first ends secured to the outer annular cover by fasteners and their radially inner second ends in the form of combs holding in position between them a transverse rim of the annular combustion chamber so as to enable a cooling stream to flow towards the annular nozzle and so as to hold the annular combustion chamber axially while leaving it free to move at least radially.

First claim

The invention claimed is:

1. A turbine engine comprising:
inner annular cover and outer annular cover defining therebetween an annular space for receiving a gas flow stream;
an annular combustion chamber having a longitudinal axis; and
an annular nozzle,
wherein said annular combustion chamber is held in position in said outer annular cover between a first radial holder ring and a second radial holder ring, each of the first radial holder ring and the second radial holder ring having radially outer first ends located outside the gas flow stream sandwiched between flanges of the outer annular cover and fastened to said outer annular cover by fastener means and radially inner second ends located inside the gas flow stream that sandwich a transverse rim of said annular combustion chamber between the radially inner second ends of the first radial holder ring and the second radial holder ring in such a manner as to hold said annular combustion chamber axially while leaving said annular combustion chamber free to move at least radially, and
wherein said radially outer first ends of said first radial holder ring and said second radial holder ring abut each other and are nested at least in part one within the other, and said radially inner second ends of said first radial holder ring and said second radial holder ring form of a comb having teeth with gaps therebetween that are directed radially inward and in alignment with one another and with gaps of the transverse rim so as to allow a cooling stream to flow through the first radial holder ring and the second radial holder ring towards said annular nozzle.

2. The turbine engine according to claim 1 , wherein said transverse rim is made up of teeth between which the gaps of the transverse rim are defined that are directed radially outward in order to allow said cooling stream to flow towards said annular nozzle.

3. The turbine engine according to claim 2 , wherein a first radial portion of the first radial holder ring is pierced by orifices that are regularly distributed around said annular combustion chamber in order to receive said fastener means, and a second radial portion of said first radial holder ring extends axially upstream over a length corresponding to an axial dimension of said transverse rim.

4. The turbine engine according to claim 3 , wherein said second radial holder ring has a crenellated first radial portion pierced by orifices for receiving said fastener means and extended by a second radial portion constituting said radially inner second ends in the form of a comb, said crenellated first radial portion being nested in complementary manner in a radial setback of said first radial portion of said first radial holder ring provided in register with each of the gaps of said first radial holder ring.

5. The turbine engine according to claim 4 , wherein once said first radial holder ring and said second radial holder ring have been assembled together by nesting, the gaps of said first radial holder ring and said second radial holder ring are substantially in alignment with one another and with the gaps of the transverse rim of said annular combustion chamber.

6. The turbine engine according to claim 4 , wherein each of said gaps of said comb of said first radial holder ring or of said second radial holder ring is closed by a band mounted at an radially inner end of said teeth and thereby forming an integral portion of said first radial holder ring or said second radial holder ring.

7. The turbine engine according to claim 4 , wherein at said second radial portion, one of said first radial holder ring and said second radial holder ring has a plurality of axially-projecting extensions forming peripheral rims of oblong-shaped passages that lie between the teeth of said transverse rim, each of the axially-projecting extensions presenting a height that is less than a height of said teeth of said transverse rim, other one of said first radial holder ring and said second radial holder ring having at a radial third portion a series of openings of a same shape as said oblong-shaped passages and coming into contact with said peripheral rims via inner faces thereof so that, regardless of a radial position of said annular combustion chamber relative to said inner annular cover and outer annular cover, the flow of said cooling stream towards said annular nozzle remains unchanged.

8. The turbine engine, according to claim 1 , wherein said fastener means are constituted by a plurality of screw-and-nut systems.

9. The turbine engine according to claim 1 , wherein the first radial holder ring is independent from the outer annular cover.

10. The turbine engine according to claim 1 , wherein the second radial holder ring is independent from the annular nozzle.

11. The turbine engine according to claim 1 , wherein the first radial holder ring includes an axial portion extending axially between a radially inner end of a first radial portion of the first radial holder ring including the radially outer first ends of the first radial holder ring and a radially outer end of a second radial portion of the first radial holder ring including the radially inner second ends of the first radial holder ring.

Assignees

• Snecma

Inventors

• Delaunay Frederic

Classifications

• F23R3/60 Primary

  Support structures; Attaching or mounting means · CPC title

• F05D2260/30

  Retaining components in desired mutual position · CPC title

• F02C7/20

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

• F02C7/18

  the medium being gaseous, e.g. air {(F02C7/125 takes precedence)} · CPC title

• F02C3/14 Primary

  characterised by the arrangement of the combustion chamber in the plant (combustion chambers per se F23R; F02C3/205 takes precedence) · CPC title