Reversible blade rotor seal

Patent metadata

Field	Value
Publication number	US-10030530-B2
Application number	US-201514804894-A
Country	US
Kind code	B2
Filing date	Jul 21, 2015
Priority date	Jul 31, 2014
Publication date	Jul 24, 2018
Grant date	Jul 24, 2018

Abstract

A rotatable sealing structure for a gas turbine engine includes a first blade and a second blade. A seal is arranged between the blades and has a body that is configured for operative association with the first and second blades in a first orientation and in a second orientation to seal a gap defined between the blades.

First claim

What is claimed is:

1. A rotatable sealing structure for a gas turbine engine, comprising:
a first blade having a first shelf;
a second blade including a second shelf; and
a seal including:
a first side and a second side, each including tapered surfaces meeting at a first apex on the first side and a second apex on the second side,
the seal is arranged between the blades and has a body that is configured for operative association with the first and second blades in either of a first orientation and a second orientation to seal a gap defined between the blades,
the first and second sides are configured to engage the shelves respectively in the first and second orientations and present a structural orientation that is the same as one another,
the seal has first, second and third axes that are orthogonal relative to one another, the first axis is a longitudinal axis, the second axis is a radial axis and the third axis is a circumferential axis,
the first apex is canted at an angle relative to the first axis,
the second apex is canted at an angle relative to the first axis such that when the seal is rotated 180° about one of the first, second, or third axes, the canted angle of the second apex is the same as the canted angle of the first apex.

2. The rotatable sealing structure according to claim 1 , further comprising a rotor having slots, each configured to receive a respective one of the first and second blades, wherein the shelves define a gap therebetween, and wherein the seal is configured for engagement with the shelves between the shelves and the rotor to seal the gap.

3. The rotatable sealing structure according to claim 1 , wherein the angles are between 0° and 20°.

4. The rotatable sealing structure according to claim 1 , wherein the seal includes first and second opposing ends spaced apart along the first axis, each having a substantially parallelogram shape.

5. The rotatable sealing, structure according to claim 4 , wherein the first and second opposing ends are parallel to one another.

6. The rotatable sealing structure according to claim 1 , wherein the first and second apexes are flat.

7. The rotatable sealing structure according to claim 1 , wherein in the first orientation, the first side faces the gap, and in the second orientation, the second side faces the gap.

8. The rotatable sealing structure according to claim 1 , wherein the blades are turbine blades.

9. The rotatable sealing structure according to claim 1 , further comprising a pocket between the first and second blades and a retainer secured relative to the rotor over the pocket and configured to maintain the seal within the pocket.

10. A seal for a gas turbine engine rotatable stage, the seal comprising:
a body having a first side and a second side, that is reversible 180° about first, second and third axes that are orthogonal relative to one another such that the seal body is installable in four unique orientations,
the first axis is a longitudinal seal axis, the second axis is a radial axis and the third axis is a circumferential axis,
the first side and the second side of the body each includes tapered surfaces meeting at a first apex on the first side and a second apex on the second side,
the first apex is canted at an angle relative to the first axis, and
the second apex is canted at an angle relative to the first axis such that the body has first and second orientations that present a structural orientation that is the same as one another when the seal rotated 180° about the first, second and third axes.

11. The seal according to claim 10 , wherein the angles are between 0° and 20°.

12. The seal according to claim 11 , wherein the angles are between 5° to 10°.

13. The seal according to claim 10 , wherein the body includes first and second opposing ends spaced apart along the first axis and having a substantially parallelogram shape.

14. The seal according to claim 13 , wherein the first and second opposing ends are parallel to one another.

15. The seal according to claim 10 , wherein the first and second apexes are flat.

Assignees

• United Technologies Corp

Inventors

• Snyder Daniel A

Classifications

• F01D5/3007

  of axial insertion type · CPC title

• F01D5/12

  Blades ({specially adapted for radial flow machines or engines F01D5/04}; blade roots F01D5/30; rotors with blades adjustable in operation F01D7/00; stator blades F01D9/02) · CPC title

• F16J15/0887

  the sealing effect being obtained by elastic deformation of the packing · CPC title

• F01D5/22

  Blade-to-blade connections, {e.g. for damping vibrations} · CPC title

• F05D2250/22

  parallelepipedal · CPC title