Flanged component for a gas turbine engine

Patent metadata

Field	Value
Publication number	US-10190641-B2
Application number	US-201615344129-A
Country	US
Kind code	B2
Filing date	Nov 4, 2016
Priority date	Nov 4, 2016
Publication date	Jan 29, 2019
Grant date	Jan 29, 2019

Abstract

A flanged component for a gas turbine engine is disclosed herein. The flanged component includes a flange body with a flange mating surface and a plurality of threaded features. Each threaded feature includes a threaded portion and a relief portion. The threaded portion has threads and extends into the flange body from the flange mating surface. The relief portion extends into the flange body from the flange mating surface located outward from the threaded portion forming a rim portion therebetween. The rim portion includes an upper rim surface having an annular shape. The relief portion includes an inner surface extending from the rim and tapering outward from the upper rim surface.

First claim

What is claimed is:

1. A flanged component for a gas turbine engine, the flanged component comprising:
a flange body including a flange mating surface that mates with a second mating surface of a second flanged component;
a threaded feature including
a threaded portion with threads for receiving a threaded fastener, the threaded portion extending into the flange body from the flange mating surface along a feature axis, and
a relief portion extending into the flange body from the flange mating surface located outward from the threaded portion relative to the feature axis forming a rim portion therebetween, the rim portion including an upper rim surface having an annular shape parallel to the flange mating surface, and the relief portion including an inner surface on the rim portion extending from the upper rim surface and away from the flange mating surface, the inner surface having a frustoconical shape that tapers outward from the upper rim surface.

2. The flanged component of claim 1 , wherein the upper rim surface is recessed into the flange body relative to the flange mating surface.

3. The flanged component of claim 1 , wherein the relief portion extends into the flange body at a depth of 2 to 3 times a pitch of the threads from the flange mating surface.

4. The flanged component of claim 3 , wherein the threaded portion extends through the flange body.

5. The flanged component of claim 1 , wherein the relief portion extends into the flange body at a depth of 2 to 3 times a pitch of the threads from a first engaged thread that is the thread closest to the flange mating surface.

6. The flanged component of claim 1 , further comprising:
a seal portion;
a sealing element extending from the seal portion; and
wherein the flange body extends radially from the seal portion, and the sealing element extends in a direction opposite the flange body.

7. The flanged component of claim 6 , wherein the flanged component is a turbine seal and the sealing element is formed of radially projecting annular flanges extending radially outward from the seal portion.

8. A flanged component for a gas turbine engine, the flanged component comprising:
a flange body including a flange mating surface;
a plurality of threaded features, each threaded feature including
a threaded portion with threads for receiving a threaded fastener, the threaded portion extending into the flange body from the flange mating surface along a feature axis normal to the flange mating surface, and
a relief portion extending into the flange body from the flange mating surface located radially outward from the threaded portion relative to the feature axis, the relief portion including an inner surface having a frustoconical shape that tapers outward as the inner surface extends in a direction opposite the flange mating surface; and
the threaded portion and the relief portion form a rim portion therebetween.

9. The flanged component of claim 8 , wherein the rim portion includes an upper rim surface that is recessed into the flange body relative to the flange mating surface.

10. The flanged component of claim 9 , wherein the inner surface extends from the upper rim surface, wherein the relief portion further includes an outer surface located radially outward from the inner surface and extending into the flange body from the flange mating surface, the outer surface having a right circular cylinder shape.

11. The flanged component of claim 10 , wherein the inner surface and the outer surface extend to a recess base that is rounded between the inner surface and the outer surface.

12. The flanged component of claim 8 , wherein the relief portion extends into the flange body at a relief portion depth of 2 to 3 times a pitch of the threads from the flange mating surface.

13. The flanged component of claim 8 , wherein the relief portion extends into the flange body at a relief portion depth of 2 to 3 times a pitch of the threads from a first engaged thread that is the thread closest to the flange mating surface.

14. The flanged component of claim 8 , wherein the flanged component is a turbine seal, the flanged component further including a seal portion and seal teeth extending from the seal portion, and wherein the flange body extends radially from the seal portion.

15. A fastened joint of a gas turbine engine, the fastened joint comprising:
a first flanged component including
a flange body including a flange mating surface,
a plurality of threaded features, each threaded feature including
a threaded portion including threads, the threaded portion extending into the flange body from the flange mating surface along a feature axis normal to the flange mating surface, and
a relief portion extending into the flange body from the flange mating surface located outward from the threaded portion relative to the feature axis forming a rim portion therebetween, the rim portion including an upper rim surface with an annular shape parallel to the flange mating surface, and the relief portion including an inner surface on the rim portion extending from the upper rim surface and away from the flange mating surface, the inner surface having a frustoconical shape that tapers outward from the upper rim surface;

a second flanged component including a second mating surface adjoining the flange mating surface and a plurality of second flange through holes; and
a plurality of fasteners, each including a fastener head and a fastener shank extending through one of the plurality of second flange through holes and threaded into the threaded portion of one of the plurality of threaded features.

16. The fastened joint of claim 15 , wherein the upper rim surface is recessed into the flange body relative to the flange mating surface and is adjacent to the second mating surface.

17. The fastened joint of claim 15 , wherein the relief portion extends into the flange body at a relief portion depth of 2 to 3 times a pitch of the threads from the flange mating surface.

18. The fastened joint of claim 15 , wherein the relief portion extends into the flange body at a relief portion depth of 2 to 3 times a pitch of the threads from a first engaged thread that is the thread closest to the flange mating surface and closest to the fastener head.

19. The fastened joint of claim 15 , wherein the first flanged component further comprises:
a seal portion;
a sealing element extending from the seal portion; and
wherein the flange body extends radially from the seal portion.

20. The fastened joint of claim 15 , wherein the inner surface extends from the upper rim surface, wherein the relief portion further includes an outer surface located radially outward from the inner surface and extending into the flange body from the flange mating surface, the outer surface including a right circular cylinder shape, and wherein the inner surface and the outer surface extend to a recess base that is rounded between the inner surface and the outer surface.

Assignees

• Solar Turbines Inc

Inventors

• Struck Bruno E

Classifications

• F01D11/02

  by non-contact sealings, e.g. of labyrinth type (for sealing space between rotor blade tips and stator F01D11/08) · CPC title

• F01D5/025

  Fixing blade carrying members on shafts (attachment of a member on a shaft in general F16D1/06; for non-positive displacement pumps F04D29/00) · CPC title

• F05D2240/55

  Seals · CPC title

• F01D11/003

  by packing rings; Mechanical seals · CPC title

• F01D11/001

  for sealing space between stator blade and rotor · CPC title