Assembly for a turbomachine

Patent metadata

Field	Value
Publication number	US-11221141-B2
Application number	US-201917260719-A
Country	US
Kind code	B2
Filing date	Jul 18, 2019
Priority date	Jul 19, 2018
Publication date	Jan 11, 2022
Grant date	Jan 11, 2022

Abstract

A turbomachine includes a combustion chamber with a radially extending downstream flange at its downstream end. A distributor is disposed downstream of the combustion chamber and includes a platform from which at least one vane extends radially. The platform has an upstream edge extending radially and delimiting, with the downstream flange disposed opposite, a gap opening into the combustion chamber at its radially inner end and closed at its radially outer end by sealing means fixed to the distributor. The downstream flange of the combustion chamber has at least one rectilinear cooling orifice passing through the flange and opening into the gap opposite the platform of the distributor.

First claim

The invention claimed is:

1. An assembly for a turbomachine, comprising:
a combustion chamber comprising a radially extending downstream flange positioned at a downstream end; and
a distributor disposed downstream of the combustion chamber and comprising a platform from which at least one vane extends radially, the platform comprising an upstream edge extending radially and delimiting, with the downstream flange disposed opposite, a gap opening into the combustion chamber at its radially inner end and closed at its radially outer end by sealing means fixed to the distributor,
wherein the downstream flange of the combustion chamber comprises at least one rectilinear cooling orifice passing through said flange and opening into the gap opposite the platform of the distributor, and
the radial portion of the downstream flange of the combustion chamber has at least two cooling orifices passing through the downstream flange and opening into the gap, two of said orifices extending in two directions forming an angle with each other.

2. The assembly according to claim 1 , wherein the sealing means comprise at least one radially and circumferentially extending lamella, which bears axially on the downstream flange of the combustion chamber and on the upstream edge of the distributor.

3. The assembly according to claim 1 , further comprising at least one orifice inclined in a first circumferential direction and at least one orifice inclined in a second circumferential direction, opposite to the first circumferential direction.

4. The assembly according to claim 1 , further comprising at least one axially oriented orifice.

5. The assembly according to claim 3 , further comprising at least one first axially oriented orifice and at least one second and one third orifice located circumferentially on either side of the first orifice, the second and third orifices being inclined in two opposite circumferential directions.

6. The assembly according to claim 5 , further comprising at least one fourth orifice and at least one fifth orifice, situated respectively circumferentially on either side of the second and third orifices, opposite the first orifice, the fourth and fifth orifices being oriented axially.

7. The assembly according to claim 1 , further comprising at least two orifices radially and circumferentially offset from each other.

8. The assembly according to claim 1 , wherein edges of the orifices opening into the gap are offset from one another by a distance of between 0.1 and 6 mm.

Assignees

• Tamizier Julien Michel
• Texier Christophe Bernard
• Bonneau Damien
• Bonnefoi Damien
• Chapelle Francois Xavier
• Safran Aircraft Engines

Inventors

• Tamizier Julien Michel
• Texier Christophe Bernard
• Bonneau Damien
• Bonnefoi Damien
• Chapelle François Xavier

Classifications

• F23R2900/03042

  Film cooled combustion chamber walls or domes · CPC title

• F23R3/005 Primary

  Combined with pressure or heat exchangers · CPC title

• F23R3/10

  for primary air (F23R3/06, F23R3/045 take precedence) · CPC title

• F05D2240/35

  Combustors or associated equipment · CPC title

• F23R2900/00012

  Details of sealing devices · CPC title