Blade outer air seal cooling enhanced with inter-segment film slot

• US 5,374,161 A
• Filed: 12/13/1993
• Issued: 12/20/1994
• Est. Priority Date: 12/13/1993
• 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: Auxier, Thomas A., Kelch, George W.
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): VERDIER, CHRISTOPHER M
• Application Number:
  US08/166,426
• Time in Patent Office: 372 Days
• Field of Search: 415/115, 415/116, 415/117, 415/135, 415/138, 415/139, 415/173.1, 415/173.3, 415/173.4, 415/180, 277/192, 277/199, 277/222
• US Class Current: 415/139
• CPC Class Codes: F01D 11/005 Sealing means between non relatively rotating elements
• CPC Class Codes: F01D 11/08 for sealing space between rotor blade tips and stator specially-shaped blade tips therefor F01D5/20
• CPC Class Codes: F01D 25/12 Cooling
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A cooling enhancement for a gas turbine engine blade outer air seal is made up of a plurality of arcuate seal segments, and each one has one or more internal cooling passages. Each segment has a supply surface opposite and in spaced relation to a sealing surface, and first and second end surfaces extending from the sealing surface to the supply surface. Each of the end surfaces includes a substantially planar perpendicular surface and a substantially planar canted surface intersecting at an included angle of between 100 degrees and 140 degrees, and the supply surface has a plurality of cooling orifices adjacent the second end surface. At least one cooling passage extends from the first end surface towards the second end surface, and each cooling passage intersects the first end surface and terminates short of the second end surface. Each cooling passage communicates with the supply surface through at least one of the cooling orifices. Protruding from at least one of the substantially canted surfaces is a plurality of stand-off pedestals that are integral with the canted surface.

Claims

1. An engine seal for an axial flow gas turbine engine having an axis of rotation defined therethrough, an annular flow path concentric with said axis for working fluid flowing through at least one turbine stage of said engine, said one turbine stage including a plurality of turbine blades extending outward from said axis, and said flow path bounded by a static structure, and an annular seal secured to said static structure radially outward of said one turbine stage, said seal absorbing heat from said working fluid, said turbine blades rotating in a first direction relative to said seal, said seal comprising:

a plurality of arcuate seal segments extending circumferentially about the flow path, each segment spaced radially outward from said turbine blades, each seal segment including

an arcuate sealing surface having a first end, a second end opposite the first end, and a radius of curvature equal to the distance between the sealing surface and the axis,

a supply surface opposite and in spaced relation to the sealing surface and having a plurality of cooling orifices extending therethrough,

a first end surface extending along the entire first end, and a second end surface extending along the entire second end, said first and second end surfaces extending from said sealing surface to said supply surface, each of said first and second end surfaces including a substantially planar perpendicular surface and a substantially planar canted surface intersecting at an included angle of between 100 degrees and 140 degrees, and each canted surface is canted in the first direction,

a first side surface and a second side surface, each of said side surfaces extending from said sealing surface to said supply surface and from said first end surface to said second end surface,

at least one cooling passage extending from the first end surface toward the second end surface, said cooling passage located between said sealing surface, said supply surface, and said side surfaces, said cooling passage intersecting the first end surface and terminating short of said second end surface, and said cooling passage communicating with the supply surface through at least one of the cooling orifices,

wherein each segment is spaced circumferentially from each adjacent segment defining an inter-segment gap therebetween, cooling air from said supply enters said passage through one of said orifices, flows through said passage in a second direction and exits said cooling passage into one of said inter-segment gaps at said first end supply and discharges from the inter-segment gap into the working fluid of the engine.

2. The engine seal of claim 1 wherein each segment includes

a plurality of said cooling passages that communicate with said orifices, each of said orifices is adjacent said second end surface, each said cooling passage communicates with the first surface of said segment through at least one passage outlet, each of said cooling passages is separated from adjacent cooling passages by a wall therebetween, the cooling air flows through each passage in the second direction, and the second direction is opposite said first direction.

3. The seal of claim 2 wherein the second surface of each segment includes a quantity of cooling air feed pockets equal to the quantity of passage outlets in the first surface of the same segment, and each feed pocket is aligned with one of the passage outlets of one of the adjacent segments, said feed pockets for receiving and turning air flowing into the inter-segment gaps.

4. The seal of claim 3 wherein each segment further includes a plurality of stand-off pedestals protruding from one of the substantially canted surfaces thereof toward one of the canted surfaces of one of the adjacent segments, and said pedestals are integral with one of the substantially canted surfaces.

5. The seal of claim 4 wherein the pedestals of each segment are aligned in a row extending between the first side surface and the second side surface thereof.

6. The seal of claim 5 wherein the sealing surface of each segment is radiused where it joins the second substantially canted surface thereof, thereby providing a smooth transition between the second substantially canted surface and the sealing surface thereof.

7. The seal of claim 6 wherein said each of the substantially perpendicular surfaces of each segment includes a channel, the channels of each segment are substantially parallel to the supply surface thereof, each channel is in spaced relation and opposed to the one of the channels of one of the adjacent segments, and an inter-segment seal extends between each of said opposed channels.

8. A circumferential seal comprising:

a plurality of arcuate seal segments, each seal segment including

an arcuate sealing surface having a first end, and a second end opposite the first end,

a supply surface opposite and in spaced relation to the sealing surface and having a plurality of cooling orifices extending therethrough,

a first end surface extending along the entire first end, and a second end surface extending along the entire second end, said first and second end surfaces extending from said sealing surface to said supply surface, each of said first and second end surfaces including a substantially planar perpendicular surface and a substantially planar canted surface intersecting at an included angle of between 100 degrees and 140 degrees, and said orifices adjacent said second end surface,

a first side surface and a second side surface, each of said side surfaces extending from said sealing surface to said supply surface and from said first end surface to said second end surface,

at least one cooling passage extending from the first surface toward the second surface, each cooling passage located between said sealing surface and said supply surface, each cooling passage intersecting the first surface and terminating short of said second surface, each cooling passage communicating with the supply surface through at least one of the cooling orifices,

wherein each segment is located immediately adjacent two other of said segments, the first surface of each of said segments is in spaced relation to the second surface of one of said two immediately adjacent segments defining an inter-segment gap therebetween, and the second surface of each of said segments is in spaced relation to the first surface of the other of said two adjacent segments, defining another inter-segment gap therebetween.

9. The seal of claim 8 wherein each segment includes

a plurality of said cooling passages, each said cooling passage communicates with the first surface of said segment through at least one passage outlet, and each of said cooling passages is separated from adjacent cooling passages by a wall therebetween.

10. The seal of claim 9 wherein the second surface of each segment includes a quantity of cooling air feed pockets equal to the quantity of passage outlets in the first surface of the same segment, and each feed pocket is aligned with one of the passage outlets of one of the adjacent segments.

11. The seal of claim 10 wherein each segment further includes a plurality of stand-off pedestals protruding from one of the substantially canted surfaces thereof toward one of the canted surfaces of one of the adjacent segments, and said pedestals are integral with one of the substantially canted surfaces.

12. The seal of claim 11 wherein the pedestals of each segment are aligned in a row extending between the first side surface and the second side surface thereof.

13. The seal of claim 12 wherein the sealing surface of each segment is radiused where it joins the second substantially canted surface thereof, thereby providing a smooth transition between the second substantially canted surface and the sealing surface thereof.

14. The seal of claim 13 wherein said each of the substantially perpendicular surfaces of each segment includes a channel, the channels of each segment are substantially parallel to the supply surface thereof, each channel is in spaced relation and opposed to the one of the channels of one of the adjacent segments, and an inter-segment seal extends between each of said opposed channels.

15. A seal segment comprising:

a sealing surface having a width and a length, said length terminating in a first end and a second end opposite the first end, said sealing surface arcuate between said first and second ends,

a supply surface opposite and in spaced relation to the sealing surface and having a plurality of cooling orifices extending therethrough,

a first end surface extending along the entire first end, and a second end surface extending along the entire second end, said first and second end surfaces extending from said sealing surface to said supply surface, each of said first and second end surfaces including a substantially planar perpendicular surface and a substantially planar canted surface intersecting at an included angle of between 100 degrees and 140 degrees, and said orifices adjacent said second end surface,

a first side surface and a second side surface, each of said side surfaces extending from said sealing surface to said supply surface and from said first end surface to said second end surface,

at least one cooling passage extending from the first end surface toward the second end surface, each said cooling passage located between said sealing surface, said supply surface and the first and second side surfaces, each said cooling passage intersecting the first end surface and terminating short of said second end surface, each said cooling passage communicating with the supply surface through at least one of the cooling orifices.

16. The seal segment of claim 15 further comprising

a plurality of said cooling passages, each said cooling passage communicates with the first end surface through at least one passage outlet, and each of said cooling passages is separated from adjacent cooling passages by a wall therebetween.

17. The seal of claim 16 wherein the second end surface includes a quantity of cooling air feed pockets equal to the quantity of passage outlets in the first end surface, and each teed pocket is aligned with one of the passage outlets.

18. The seal of claim 17 further comprising a plurality of stand-off pedestals protruding from one of the substantially canted surfaces thereof, and said pedestals are integral with one of the substantially canted surfaces.

19. The seal of claim 18 wherein said pedestals are aligned in a row extending between the first side surface and the second side surface.

20. The seal of claim 19 wherein the sealing surface is radiused where it joins the second substantially canted surface, thereby providing a smooth transition between the second substantially canted surface and the sealing surface.

21. The seal of claim 20 wherein said each of the substantially perpendicular surfaces includes a channel, each channel is substantially parallel to the supply surface, and each channel is located between the first side surface and the second side surface.