TOOLS AND METHODS FOR ASSEMBLING A SEAL DEVICE OF A GAS TURBINE ENGINE
20230201979 ยท 2023-06-29
Inventors
Cpc classification
F05D2300/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D11/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2240/55
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2230/70
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2230/68
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D11/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2300/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B23P19/027
PERFORMING OPERATIONS; TRANSPORTING
F01D11/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2230/60
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2240/55
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2230/68
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D11/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A seal device includes a first sidewall, a second sidewall and a carbon seal element. The first sidewall is arranged with a first tool die which centers the first sidewall about an axis. The first sidewall axially contacts the first tool die along the axis. The carbon seal element is arranged with a centering element which centers the carbon seal element about the axis. The carbon seal element circumscribes and radially contacts the centering element. The second sidewall is arranged with a second tool die which centers the second sidewall about the axis. The second sidewall axially contacts the second tool die along the axis. The first tool die and the second tool die are moved axially together along the axis to press fit the second sidewall into a bore of the first sidewall and axially capture the carbon seal element between the first sidewall and the second sidewall.
Claims
1. A tool for assembling a seal device of a gas turbine engine, the tool comprising: a first tool die including a first die base, a first die curb and a first die bumper, the first die curb projecting axially out from the first die base along an axis, the first die curb extending circumferentially about the axis, the first die bumper spaced radially outward from the first die curb by a first die channel, the first die bumper projecting axially out from the first die base along the axis, and the first die bumper extending circumferentially about the axis; a second tool die including a second die base, a second die curb and a second die bumper, the second die curb projecting axially out from the second die base along the axis, the second die curb extending circumferentially about the axis, the second die bumper spaced radially outward from the second die curb by a second die channel, the second die bumper projecting axially out from the second die base along the axis, and the second die bumper extending circumferentially about the axis; a centering element extending axially along and circumferentially about the axis; a receptacle configured to receive the seal device, the receptacle extending axially along the axis within the tool between the first tool die and the second tool die, and the receptacle projecting radially inward into the tool to the centering element; and an actuator configured to axially press the seal device between the first tool die and the second tool die.
2. The tool of claim 1, wherein the first die curb is configured to radially engage and locate a first sidewall of the seal device within the receptacle, and the first die bumper is configured to axially engage and press against the first sidewall; the second die curb is configured to radially engage and locate a second sidewall of the seal device within the receptacle, and the second die bumper is configured to axially engage and press against the second sidewall; and the centering element is configured to radially engage and locate a seal element of the seal device disposed between the first sidewall and the second sidewall.
3. The tool of claim 1, wherein the first die curb comprises an outer cylindrical surface configured to radially contact the seal device within the receptacle; and the first die bumper comprises an annular planar surface configured to axially contact the seal device within the receptacle.
4. The tool of claim 1, wherein the second die curb comprises an outer cylindrical surface configured to radially contact the seal device within the receptacle; and the second die bumper comprises an annular planar surface configured to axially contact the seal device within the receptacle.
5. The tool of claim 1, wherein the centering element comprises an outer cylindrical surface configured to radially contact a carbon seal element of the seal device within the receptacle.
6. The tool of claim 1, wherein an axial distal end of the first die bumper is axially recessed inward towards the first die base from an axial distal end of the first die curb.
7. The tool of claim 1, wherein the first die base projects radially outward to a first base distal end; and the first die bumper is spaced radially inward from the first base distal end.
8. The tool of claim 1, wherein the centering element is attached to the first die base; and the centering element radially abuts and is circumscribed by the first die curb.
9. The tool of claim 1, wherein an axial distal end of the second die bumper is axially recessed inward towards the second die base from an axial distal end of the second die curb.
10. The tool of claim 1, wherein the second die base projects radially outward to a second base distal end; and the second die bumper is disposed at the second base distal end.
11. The tool of claim 1, wherein at least one of the first die bumper has a rectangular sectional geometry; or the second die bumper has a triangular sectional geometry.
12. The tool of claim 1, wherein the actuator is configured to move the first tool die and the second tool die towards one another from an open position to a closed position to axially press the seal device between the first tool die and the second tool die; and the centering element is axially spaced from the second tool die by a gap at the closed position.
13. The tool of claim 1, wherein the first tool die and the second tool die each comprise a metal; and the centering element comprises a polymer.
14. The tool of claim 1, wherein the actuator comprises a linear actuator.
15. The tool of claim 1, wherein the actuator comprises a shaft, a piston and a housing; and the shaft is connected to the first die base, and the shaft projects axially along the axis through the centering element and the second tool die into the housing to the piston.
16. The tool of claim 15, wherein the housing comprises a portion of the second tool die.
17. A manufacturing method, comprising: providing a seal device of a gas turbine engine, the seal device including a first sidewall, a second sidewall and a carbon seal element; arranging the first sidewall with a first tool die, the first tool die including a first die curb and a first die bumper, the first sidewall radially engaging and centered about an axis by the first die curb, and the first sidewall axially engaging the first die bumper; arranging the carbon seal element with a centering element, the carbon seal element circumscribing the centering element, and the carbon seal element radially engaging and centered about the axis by the centering element; arranging the second sidewall with a second tool die, the second tool die including a second die curb and a second die bumper, the second sidewall radially engaging and centered about the axis by the second die curb, and the second sidewall axially engaging the second die bumper; and moving the first tool die and the second tool die axially together along the axis to assembly the seal device.
18. The manufacturing method of claim 17, wherein the carbon seal element is captured axially between the first sidewall and the second sidewall; the first sidewall includes a rim; and the second sidewall is press fit into the rim during the moving of the first tool die and the second tool die axially together along the axis.
19. The manufacturing method of claim 17, wherein the first tool die further includes a first die base, the first die curb projects axially out from the first die base along the axis, the first die curb extends circumferentially about the axis, the first die bumper is spaced radially outward from the first die curb by a first die channel, the first die bumper projects axially out from the first die base along the axis, and the first die bumper extends circumferentially about the axis; and the second tool die further includes a second die base, the second die curb projects axially out from the second die base along the axis, the second die curb extends circumferentially about the axis, the second die bumper is spaced radially outward from the second die curb by a second die channel, the second die bumper projects axially out from the second die base along the axis, and the second die bumper extends circumferentially about the axis.
20. A manufacturing method, comprising: providing a seal device of a gas turbine engine, the seal device including a first sidewall, a second sidewall and a carbon seal element; arranging the first sidewall with a first tool die comprising metal, the first tool die centering the first sidewall about an axis, and the first sidewall axially contacting the first tool die along the axis; arranging the carbon seal element with a centering element comprising polymer, the centering element centering the carbon seal element about the axis, and the carbon seal element circumscribing and radially contacting the centering element; arranging the second sidewall with a second tool die comprising metal, the second tool die centering the second sidewall about the axis, and the second sidewall axially contacting the second tool die along the axis; and moving the first tool die and the second tool die axially together along the axis to press fit the second sidewall into a bore of the first sidewall and axially capture the carbon seal element between the first sidewall and the second sidewall.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0025]
[0026]
[0027]
[0028]
[0029]
[0030]
DETAILED DESCRIPTION
[0031]
[0032] Referring to
[0033] The bottom die base 42 is disposed at (e.g., on, adjacent or proximate) the bottom die bottom side 34. The bottom die base 42 of
[0034] The bottom die curb 43 is connected to (e.g., formed integral with) the bottom die base 42. The bottom die curb 43 is disposed at the bottom die top side 36. The bottom die curb 43 of
[0035] The bottom die curb 43 and its bottom curb inner side 53 are radially spaced from a hub 58 of the bottom die base 42 by an inner channel 60 of the bottom tool die 24. This inner bottom die channel 60 projects axially along the centerline axis 32 into the bottom die tool from the bottom die top side 36 to a channel end 62. The inner bottom die channel 60 extends radially within the bottom tool die 24 between and to the bottom curb inner side 53 and an outer side 64 of the bottom die hub 58. The inner bottom die channel 60 extends within the bottom tool die 24 circumferentially about (e.g., completely around) the centerline axis 32.
[0036] The bottom die bumper 44 is connected to (e.g., formed integral with) the bottom die base 42. The bottom die bumper 44 is disposed towards the bottom die top side 36. The bottom die bumper 44 of
[0037] The bottom die bumper 44 and its bottom bumper outer side 72 are spaced radially inward from the bottom die base distal end 46. The bottom die bumper 44 and its bottom bumper inner side 70 are radially spaced from the bottom curb outer side 54 by an outer channel 74 of the bottom tool die 24. This outer bottom die channel 74 projects axially along the centerline axis 32 into the bottom tool die 24 from the bottom die top side 36 to a channel end 76. The outer bottom die channel 74 extends radially within the bottom tool die 24 between and to the bottom curb outer side 54 and bottom bumper inner side 70. The outer bottom die channel 74 extends within the bottom tool die 24 circumferentially about (e.g., completely around) the centerline axis 32.
[0038] The bottom tool die 24 may be constructed as a monolithic body from bottom tool die material. This bottom tool die material may be metal such as, but not limited to, steel. The present disclosure, however, is not limited to the foregoing exemplary bottom tool die materials.
[0039] Referring to
[0040] The top die base 86 is disposed at the top die top side 80. The top die base 86 of
[0041] The top die curb 87 is connected to (e.g., formed integral with) the top die base 86. The top die curb 87 is disposed at the top die bottom side 78. The top die curb 87 of
[0042] The top die curb 87 and its top curb inner side 97 is radially spaced from a radial outer edge of the exterior counterbore 96.
[0043] The top die bumper 88 is connected to (e.g., formed integral with) the top die base 86. The top die bumper 88 is disposed towards the top die bottom side 78. The top die bumper 88 of
[0044] The top die bumper 88 and its top bumper inner side 108 are radially spaced from the top curb outer side 99 by a channel 112 of the top tool die 25. This top die channel 112 projects axially along the centerline axis 32 into the top tool die 25 from the top die bottom side 78 to a channel end 114. The top die channel 112 extends radially within the top tool die 25 between and to the top curb outer side 99 and top bumper inner side 108. The top die channel 112 extends within the top tool die 25 circumferentially about (e.g., completely around) the centerline axis 32.
[0045] The top tool die 25 may be constructed as a monolithic body from top tool die material. This top tool die material may be metal such as, but not limited to, steel. The present disclosure, however, is not limited to the foregoing exemplary top tool die materials.
[0046] Referring to
[0047] The element base 124 extends axially along the centerline axis 32 between and to the element bottom side 116 and the element top side 118. The element base 124 extends radially between and to the element inner side 120 and an outer (e.g., cylindrical) surface 128 at or about the element outer side 122. The element base 124 extends circumferentially about (e.g., completely around) the centerline axis 32.
[0048] The element rim 126 is connected to (e.g., formed integral with) the element base 124. The element rim 126 is disposed at the element bottom side 116 and the element outer side 122. The element rim 126 of
[0049] The centering element 26 may be constructed as a monolithic body from centering element material. This centering element material may be relatively soft or compliant material (compared to metal) such as, but not limited to, polymer; e.g., thermoplastic. The present disclosure, however, is not limited to the foregoing exemplary centering element materials.
[0050] Referring to
[0051] The actuator 28 may be configured as a linear actuator. The actuator 28 of
[0052] During operation of the assembly tool 20 of
[0053]
[0054] In step 502, the first sidewall 154 is arranged with the bottom tool die 24. The first sidewall 154, more particularly, is mated with the bottom die curb 43 and the bottom die bumper 44. An inner flange 158 of the first sidewall 154 of
[0055] In step 504, the seal element 156 is arranged with the centering element 26. The centering element 26 of
[0056] In step 506, the second sidewall 155 is arranged with the top tool die 25. The second sidewall 155, more particularly, is mated with the top die curb 87 and the top die bumper 88. An outer portion 160 of the second sidewall 155 of
[0057] In step 508, the seal device 22 is assembled. The actuator 28 of
[0058] In step 510, the assembly seal device 22 is removed from the assembly tool 20. The hydraulic fluid, for example, may be directed out of (e.g., evacuated from) the chamber 140 to place the bottom tool die 24 and the top tool die 25 in their first (e.g., open) position. The actuator 28 may then be disassembled to remove the seal device 22.
[0059] The seal device 22 of
[0060] While various embodiments of the present disclosure have been described, it will be apparent to those of ordinary skill in the art that many more embodiments and implementations are possible within the scope of the disclosure. For example, the present disclosure as described herein includes several aspects and embodiments that include particular features. Although these features may be described individually, it is within the scope of the present disclosure that some or all of these features may be combined with any one of the aspects and remain within the scope of the disclosure. Accordingly, the present disclosure is not to be restricted except in light of the attached claims and their equivalents.