Easily adaptable compressor bleed system downstream of a vane platform

Patent metadata

Field	Value
Publication number	US-9567914-B2
Application number	US-201214117746-A
Country	US
Kind code	B2
Filing date	Apr 27, 2012
Priority date	May 30, 2011
Publication date	Feb 14, 2017
Grant date	Feb 14, 2017

Abstract

Discrete bleed behind stator vane platform is provided. The discrete bleed behind stator vane platform relates to a system for bleeding off a working fluid from an inner volume (Vi) of a turbo-machine. The system includes a vane carrier with an annular rail and a vane device comprising at least one vane element, a vane platform and a vane root. The vane element is mounted to the vane platform and the vane root is mounted to the annular rail. A first annular cavity is formed between the vane platform and the annular rail, wherein an annular gap is formed between an edge of the vane platform and the vane carrier such that a part of the working fluid of the turbo-machine is bleedable through the annular gap into the first annular cavity. A second annular cavity is formed between the vane root, the annular rail and the vane carrier, wherein at least one inlet hole is formed into the annular rail for coupling the first annular cavity and the second annular cavity.

First claim

The invention claimed is:

1. A system for bleeding off a working fluid from an inner volume (Vi) of a turbo-machine, the system comprising
a vane carrier comprising an annular rail, a vane device comprising at least one vane element, at least one vane platform and a vane root,
wherein the vane element is mounted to the vane platform,
wherein the vane root is mounted to the annular rail,
wherein a first annular cavity is formed by a space between a radially outer surface of the vane platform and the annular rail,
wherein an annular gap is formed between an edge of the vane platform and the vane carrier such that a part of the working fluid of the turbo-machine is bleedable through the annular gap into the first annular cavity,
wherein a second annular cavity is formed between the vane root, the annular rail and the vane carrier radially outward of the vane root along a radial axis of the vane element, and
wherein at least one inlet hole is formed into the annular rail without a further hole or other weakening provision being formed in the vane device for coupling the first annular cavity and the second annular cavity.

2. The system according to claim 1 ,
wherein the vane element comprises a leading edge and a trailing edge,
wherein the working fluid is streamable from the leading edge to the trailing edge along the vane element, and
wherein with respect to the vane element, the edge of the vane platform is located downstream with respect to a flow path of the working fluid.

3. The system according to claim 1 ,
wherein the vane root comprises an annular groove,
wherein the annular rail is engaged into the annular groove for mounting the vane root to the annular rail.

4. The system according to claim 1 , wherein the vane device comprises a plurality of vane elements.

5. The system according to claim 1 , further comprising
a further vane device comprising at least one further vane element, a further vane platform and a further vane root,
wherein the further vane element is mounted to the further vane platform,
wherein the further vane root is mounted to the annular rail,
wherein the first annular cavity is formed between the vane platform, the further vane platform and the annular rail,
wherein the annular gap is formed between a further edge of the further vane platform and the vane carrier such that a part of the working fluid is bleedable through the annular gap into the first annular cavity, and
wherein the second annular cavity is formed between the vane root, the further vane root, the annular rail and the vane carrier.

6. The system according to claim 5 , further comprising a seal,
wherein between the vane platform and the further vane platform a further gap is formed, and
wherein the seal abuts against the vane device and the further vane device such that a leakage of working fluid between the second annular cavity and the further gap is at least partially prevented.

7. The system according to claim 1 ,
wherein the vane carrier comprises a fluid outlet for bleeding the working fluid out of the second cavity into an outer volume (Vo) of the carrier device.

8. The system according to claim 1 further comprising
a radially inward further vane platform,
wherein the vane element is mounted between the vane platform and the radially inward further vane platform.

9. The system according to claim 8 , further comprising a radially inward further vane carrier,
wherein the radially inward further vane carrier is mounted radially inwards to the radially inward further vane platform.

10. The system according to claim 8 ,
wherein the radially inward further vane platform or the radially inward further vane carrier comprises a sealing arrangement which is abuttable to a rotatable shaft.

11. A turbo-machine, comprising
a rotatable shaft being rotatable around a rotary axis, wherein a radial direction is orientated perpendicular to the rotary axis, and
at least one system for bleeding off a working fluid as set forth in claim 1 ,
wherein the vane platform of the vane device surrounds partially the inner volume (Vi) of the turbo-machine, wherein inside the inner volume (Vi) the working fluid is flowable, and
wherein the at least one vane element extends from the vane platform into the inner volume (Vi) such that the working fluid is flowable along the vane element.

12. The turbo-machine according to claim 11 ,
wherein the at least one inlet hole is formed into the annular rail such that the inlet hole extends along the radial direction.

13. The turbo-machine according to claim 11 , wherein the at least one inlet hole is formed in the annular rail to have a radial direction inclined to coincide with a swirl direction of the working fluid at the annular gap.

14. A method for bleeding off a working fluid from an inner volume (Vi) of a turbo-machine, comprising
providing a system having a vane carrier comprising an annular rail, a vane device comprising at least one vane element, at least one vane platform and a vane root,
mounting the vane element to the vane platform,
mounting the vane root to the annular rail,
forming a first annular cavity between a radially outer surface of the vane platform and the annular rail,
forming an annular gap between an edge of the vane platform and the vane carrier such that a part of the working fluid of the turbo-machine is bleedable through the annular gap into the first annular cavity,
forming a second annular cavity between the vane root, the annular rail and the vane carrier radially outward of the vane root along a radial axis of the vane element, and
forming at least one inlet hole into the annular rail without need for forming a further hole or other weakening provision in the vane device for coupling the first annular cavity and the second annular cavity.

Assignees

• Twell Philip
• Siemens Ag

Inventors

• Twell Philip

Classifications

• F02C6/08

  the gas being bled from the gas-turbine compressor · CPC title

• F04D29/522

  especially adapted for elastic fluid pumps · CPC title

• F04D29/526

  Details of the casing section radially opposing blade tips (ducts F04D29/545) · CPC title

• F01D9/06 Primary

  Fluid supply conduits to nozzles or the like · CPC title

• F02C9/18 Primary

  by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages {(F02C3/113 takes precedence)} · CPC title