Clipped heat shield assembly

Patent metadata

Field	Value
Publication number	US-10539153-B2
Application number	US-201715458105-A
Country	US
Kind code	B2
Filing date	Mar 14, 2017
Priority date	Mar 14, 2017
Publication date	Jan 21, 2020
Grant date	Jan 21, 2020

Abstract

Bleed air system includes bleed port with annular bleed slot in a compressor inner casing surrounding flowpath circumscribing a centerline in compressor inner casing. Inner and outer slot walls bound bleed flow passage through the bleed slot. Annular array of arcuate shields radially inwardly bound the bleed flow passage downstream and aft of inner slot wall. Each shield includes integrally-formed axially forward retaining portion, downstream portion, and upstream portion therebetween. Clipping means clips retaining portion to aft facing radial wall of annular lip on inner slot wall. Clipping means may be arcuate or annular clip having forward annular portion attached to annular aft flange substantially perpendicular to the centerline and forward annular portion disposed in annular slot extending into inner slot wall. Forward annular portion and annular slot may be cylindrical or conical. Clip may include aft conical portion radially offset from forward conical portion and transition portion therebetween.

First claim

What is claimed:

1. A gas turbine engine bleed air system comprising:
a bleed port in a compressor inner casing surrounding a compressor flowpath of a high pressure compressor circumscribing a centerline;
the bleed port including an annular bleed slot in the compressor inner casing;
inner and outer slot walls radially inwardly and outwardly respectively bounding a bleed flow passage through the bleed slot;
an annular lip on the inner slot wall;
an annular array of arcuate shields radially inwardly bounding the bleed flow passage downstream and aft of the inner slot wall;
each of the shields including an integrally-formed axially forward retaining portion, a downstream portion, and an upstream portion therebetween;
the retaining portion being a free end having a radially inner annular edge; and
a clip portion that secures the forward retaining portion to an aft facing radial wall of the annular lip, wherein the clip portion is separate and apart from the arcuate shields.

2. The system as claimed in claim 1 , further comprising:
the clip portion including an annular clip having a forward annular portion attached to an annular aft flange,
the aft flange substantially perpendicular to the centerline, and
the forward annular portion disposed in an annular slot extending into the inner slot wall.

3. The system as claimed in claim 2 , further comprising the retaining portion being substantially perpendicular to the centerline.

4. The system as claimed in claim 3 , further comprising the forward annular portion and the annular slot being cylindrical.

5. The system as claimed in claim 3 , further comprising the forward annular portion and the annular slot being conical.

6. The system as claimed in claim 1 , further comprising:
the clip portion including an annular clip including an aft conical portion aft of and radially offset from a forward conical portion,
a transition portion therebetween connecting the aft conical portion to the forward conical portion, and
the forward conical portion disposed in an annular slot extending into the inner slot wall.

7. The system as claimed in claim 6 , further comprising the forward retaining portion of the arcuate shield bonded to the aft conical portion of the annular clip.

8. The system as claimed in claim 7 , further comprising the forward retaining portion and the forward and aft conical portions being congruent having the same conical angle.

9. The system as claimed in claim 6 , further comprising the forward retaining portion and the forward and aft conical portions being congruent having the same conical angle.

10. The system as claimed in claim 1 , further comprising:
the clip portion including an annular clip including an annular block radially inwardly resting on a step machined into the inner slot wall,
the annular block clipping the retaining portion to the aft facing radial wall of the annular lip, and
the forward retaining portion radially inwardly restrained by the step.

11. The system as claimed in claim 10 , further comprising the annular block bonded to the forward retaining portion of the arcuate shield.

12. The system as claimed in claim 11 , further comprising the retaining portion being substantially perpendicular to the centerline.

13. The system as claimed in claim 10 , further comprising the retaining portion being substantially perpendicular to the centerline.

14. The system as claimed in claim 1 , further comprising:
a casing flange extending radially outwardly from the compressor inner casing,
the downstream portion including a downstream retaining portion and a fastener slot extending therethrough,
a lip flange attached to the lip at an aft end of the lip,
a fastener disposed in forward serial progression through the fastener slot, the casing flange, and
the fastener threaded into an internally and externally threaded insert threaded in an internally threaded hole in the lip flange.

15. The system as claimed in claim 14 , further comprising:
the clip portion including an annular clip having a forward annular portion attached to an annular aft flange,
the aft flange substantially perpendicular to the centerline, and
the forward annular portion disposed in an annular slot extending into the inner slot wall.

16. The system as claimed in claim 15 , further comprising the retaining portion being substantially perpendicular to the centerline.

17. The system as claimed in claim 16 , further comprising the forward annular portion and the annular slot being cylindrical or the forward annular portion and the annular slot being conical.

18. The system as claimed in claim 14 , further comprising:
the clip portion including an annular clip including an aft conical portion aft of and radially offset from a forward conical portion,
a transition portion therebetween connecting the aft conical portion to the forward conical portion, and
the forward conical portion disposed in an annular slot extending into the inner slot wall.

19. The system as claimed in claim 18 , further comprising the forward retaining portion of the arcuate shield bonded to the aft conical portion of the annular clip.

20. The system as claimed in claim 18 , further comprising the forward retaining portion and the forward and aft conical portions being congruent having the same conical angle.

21. The system as claimed in claim 14 , further comprising:
the clip portion including an annular clip including an annular block radially inwardly resting on a step machined into the inner slot wall,
the annular block clipping the retaining portion to the aft facing radial wall of the annular lip, and
the forward retaining portion radially inwardly restrained by the step.

22. The system as claimed in claim 21 , further comprising the annular block bonded to the forward retaining portion of the arcuate shield.

23. The system as claimed in claim 22 , further comprising the retaining portion being substantially perpendicular to the centerline.

24. The system as claimed in claim 20 , further comprising the retaining portion being substantially perpendicular to the centerline.

25. A gas turbine engine bleed air system comprising:
a bleed port in a compressor inner casing surrounding a compressor flowpath of a high pressure compressor circumscribing a centerline;
the bleed port including an annular bleed slot in the compressor inner casing;
inner and outer slot walls radially inwardly and outwardly respectively bounding a bleed flow passage through the bleed slot;
an annular lip on the inner slot wall;
an annular array of arcuate shields radially inwardly bounding the bleed flow passage downstream and aft of the inner slot wall;
each of the shields including an integrally-formed axially forward retaining portion, a downstream portion, and an upstream portion therebetween;
the retaining portion being a free end having a radially inner annular edge; and
a clipping means for clipping the forward retaining portion to an aft facing radial wall of the annular lip, wherein the clipping means includes an annular clip having an aft conical portion aft of and radially offset from a forward conical portion, a transition portion therebetween connecting the aft conical portion to the forward conical portion, and the forward conical portion disposed in an annular slot extending into the inner slot wall.

Assignees

• Gen Electric

Inventors

• Thomas Michael Anthony
• Patil Abhishek Jayant
• Singhal Manish

Classifications

• F04D29/522 Primary

  especially adapted for elastic fluid pumps · CPC title

• F04D29/545

  Ducts · CPC title

• F02C9/18

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

• F04D19/02

  Multi-stage pumps · CPC title