Turbine engine rotor blade platform sealing and vibration damping device

• US 5,803,710 A
• Filed: 12/24/1996
• Issued: 09/08/1998
• Est. Priority Date: 12/24/1996
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Wiebe, David J., Stoner, Alan W., Dietrich, Douglas J.
• Primary Examiner(s): KWON, JOHN
• Application Number:
  US08/772,838
• Time in Patent Office: 623 Days
• Field of Search: 416/190, 416/193 A, 416/248, 416/500
• US Class Current: 416/248
• CPC Class Codes: F01D 11/006 Sealing the gap between rotor blades or blades and rotor
• CPC Class Codes: F01D 5/22 Blade-to-blade connections, e.g. for damping vibrations
• CPC Class Codes: F04D 29/083 especially adapted for elastic fluid pumps
• CPC Class Codes: F04D 29/34 Blade mountings for axial flow compressors F04D29/322
• CPC Class Codes: F04D 29/668 damping or preventing mechanical vibrations
• CPC Class Codes: Y10S 416/50 Vibration damping features

Abstract

A device for sealing between and damping of adjacent rotor blade platforms is provided which includes a forward seal member, a compliant center seal member, an aft seal member, a first damper, and a second damper. The first damper is disposed between the forward and compliant center seal members, and the second damper is disposed between the compliant center and aft seal members. The compliant center seal member is disposed between the first and second dampers. The compliant center seal member accommodates misalignment between adjacent rotor blade platforms by deflecting in response to centrifugal forces acting on the dampers.

Claims

1. An apparatus for sealing between and damping adjacent rotor blade platforms, comprising:

a forward seal member, having a width;

a compliant center seal member, having a width;

a first damper, disposed between said forward and compliant center seal members;

an aft seal member, having a width; and

a second damper, disposed between said center seal member and said aft seal member;

wherein said compliant center seal member is disposed between said first and second dampers; and

wherein said compliant center seal member selectively deflects to accommodate misalignment between the adjacent rotor blade platforms, thereby enabling said first and second dampers to remain in contact and damp said misaligned adjacent rotor blade platforms.

2. An apparatus according to claim 1, wherein said forward seal member is sufficiently compliant to accommodate said misaligned adjacent rotor blade platforms.

3. An apparatus according to claim 2, wherein said aft seal member is sufficiently compliant to accommodate said misaligned adjacent rotor blade platforms.

4. An apparatus according to claim 3, wherein first and second dampers extend across said width of said compliant seal member.

5. An apparatus for sealing between and damping adjacent rotor blade platforms, comprising:

compliant seal member, having a width and a length;

a first damper, attached to said compliant seal member; and

a second damper, attached to said compliant seal member;

wherein said first and second dampers are spaced apart from one another along said length of said compliant seal member; and

wherein said compliant seal member selectively deflects to accommodate misalignment between the adjacent rotor blade platforms, thereby enabling said first and second dampers to remain in contact and damp said misaligned adjacent rotor blade platforms.

6. An apparatus according to claim 5, wherein said first and second dampers are attached to a first side of said compliant seal member.

7. An apparatus according to claim 6, wherein first and second dampers extend across said width of said compliant seal member.

8. A gas turbine rotor assembly, comprising:

a plurality of rotor blades, each blade having an airfoil, a root and a platform extending out laterally between said airfoil and said root;

a disk, for rotation around a rotational axis, having a plurality of recesses positioned around a circumference of said disk, wherein each said rotor blade root is received within one of said recesses;

a plurality of sealing and damping devices, each device having

a forward seal member;

a compliant center seal member;

a first damper, disposed between said forward and compliant center seal members;

an aft seal member; and

second damper, disposed between said center seal member and said aft seal member;

wherein said compliant center seal member is disposed between said first and second dampers; and

wherein said compliant center seal member selectively deflects to accommodate misalignment between the adjacent rotor blade platforms, thereby enabling said first and second dampers to remain in contact and damp the misaligned adjacent rotor blade platforms.