US20100232939A1 - Machine Seal Assembly - Google Patents

Machine Seal Assembly Download PDF

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Publication number
US20100232939A1
US20100232939A1 US12/402,808 US40280809A US2010232939A1 US 20100232939 A1 US20100232939 A1 US 20100232939A1 US 40280809 A US40280809 A US 40280809A US 2010232939 A1 US2010232939 A1 US 2010232939A1
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United States
Prior art keywords
seal
wheel
machine
bucket
coverplate
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US12/402,808
Inventor
Matthew Robert Piersall
John Wesley Harris, JR.
Brian Denver Potter
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General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US12/402,808 priority Critical patent/US20100232939A1/en
Assigned to GENERAL ELECTRIC COMPANY reassignment GENERAL ELECTRIC COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: Piersall, Matthew Robert, HARRIS, JOHN WESLEY, JR., Potter, Brian Denver
Priority to EP10155312.1A priority patent/EP2236768A3/en
Priority to JP2010052474A priority patent/JP5475511B2/en
Priority to CN2010101468881A priority patent/CN101893001A/en
Publication of US20100232939A1 publication Critical patent/US20100232939A1/en
Abandoned legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • F01D5/081Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • F01D5/082Cooling fluid being directed on the side of the rotor disc or at the roots of the blades on the side of the rotor disc
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005Sealing means between non relatively rotating elements
    • F01D11/006Sealing the gap between rotor blades or blades and rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/04Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/55Seals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/55Seals
    • F05D2240/57Leaf seals

Definitions

  • the subject matter disclosed herein relates generally to machines and a seal assembly for machines and more specifically to a seal assembly to improve the operation, performance and efficiency of a machine.
  • Machine performance is degraded by the loss of pressurized cooling air and ingestion of hot gas flow.
  • a first aspect of the invention provides a machine comprising: a rotating shaft, a wheel coupled to the rotating shaft, the wheel including a bucket coupled to the wheel, and a seal that extends along a side of the bucket and the wheel, covering an interface there between.
  • a second aspect of the invention provides a seal assembly for a machine having a rotating shaft, the seal assembly comprising: a wheel coupled to the rotating shaft, the wheel including a bucket coupled to the wheel; and a seal that extends along a side of the bucket and the wheel, covering an interface there between.
  • FIG. 1 shows a cross-sectional view of a bucket and wheel from a machine.
  • FIG. 2 shows a cross-sectional view of a bucket and wheel from a machine with an enlarged view from an area of FIG. 1 illustrating a coverplate and seal.
  • FIG. 3 shows a cross-sectional view of a machine showing gas and air flow movement.
  • FIG. 4 shows a 360-degree single coil seal with a single split.
  • FIG. 5 shows a 360-degree single coil seal with a single split wherein the ends of the split are mechanically coupled and there is a segmented coverplate over the mechanically coupled ends of the single coil seal.
  • FIG. 6 shows a 720-degree multi-coil seal.
  • FIG. 7 shows a portion of a segmented seal.
  • FIG. 8 shows a portion of a segmented seal with a segmented coverplate over the segmented seal.
  • FIG. 9 shows a cross sectional view of a bucket and wheel from a machine.
  • the invention discussed herein includes a coverplate that is fastened to a wheel and bucket of a machine and a seal positioned between the coverplate and the wheel and the bucket.
  • a coverplate and seal on the machine is that it reduces the loss of pressurized air from the system.
  • the coverplate and seal may prevent the inflow of hot gas into the wheelspace and aid in the secondary air flow of the machine.
  • the coverplate and seal discussed herein may facilitate maintenance on the machine.
  • coverplate and seal may facilitate assembly and disassembly of the machine as the coverplate and seal can be installed and removed while the rotating shaft is on the half shell.
  • the coverplate and seal may also improve the machine's performance by acting as a heat shield and reduce vibration through the addition of damping.
  • the coverplate and seal can be installed on a forward side or an aft side of the wheel. Alternatively, the coverplate and seal can be installed on the forward side and the aft side of the wheel.
  • FIG. 1 shows a cross-sectional view of a relevant portion of a machine 100 including seal assembly 101 .
  • Machine 100 includes a bucket 102 , a wheel 104 and a rotating shaft 106 .
  • at least one wheel 104 is coupled to rotating shaft 106 of machine 100 .
  • Each wheel 104 may include a plurality of buckets 102 upon which gas acts to turn rotating shaft 106 .
  • FIG. 2 shows an enlarged view of a relevant portion of FIG. 1 .
  • Seal assembly 101 includes a seal 108 , a coverplate 110 and an angel wing 112 .
  • coverplate 110 fastens to wheel 104 of machine 100 using a hook 206 .
  • Alternative embodiments for fastening coverplate 110 to wheel 104 may include, for example: a bolt, a pin, a stack or a bayonet retaining ring.
  • coverplate 110 can include an outer edge 208 that engages a slot 210 in bucket 102 of machine 100 .
  • FIG. 3 shows a cross-sectional view of machine 100 showing gas and air flow movement.
  • FIG. 3 shows a nozzle 302 of machine 100 .
  • nozzle 302 is located on both sides of bucket 102 . It is understood, however, that nozzle 302 would be present only on a forward side of bucket 102 where the bucket is a last stage bucket.
  • a hot gas flow 308 moves across bucket 102 .
  • nozzle support ring 304 Immediately below nozzle 302 on the forward (left) or upstream side of machine 100 is a nozzle support ring 304 .
  • a diaphragm 306 Immediately below nozzle 302 on the aft (right) or downstream side of machine 100 is a diaphragm 306 .
  • Nozzle 302 includes on both the forward and aft sides, a part 305 that extends from nozzle 302 towards wheel 104 .
  • a wheelspace 314 exists on the forward and aft side of bucket 102 .
  • wheelspace 314 is between nozzle supporting ring 304 and wheel 104 .
  • wheelspace 314 is between diaphragm 306 and wheel 104 .
  • Wheelspace purge air 312 moves through wheelspace 314 . Additionally, bucket supply cooling air (not shown) moves from wheel 104 towards bucket 102 . An illustration of the movement of wheelspace purge air 312 is shown as it moves through wheelspace 314 and across wheel 104 .
  • Coverplate 110 aids in reducing the amount of wheelspace purge air 312 that is able to move between wheel 104 and nozzle support ring 304 on the forward side and wheel 104 and diaphragm 306 on the aft side. Additionally, coverplate 110 aids in the bucket supply cooling air reaching bucket 102 and not entering wheelspace 314 . As described above, in one embodiment coverplate 110 and seal 108 can be installed on a forward side or an aft side of wheel 104 ( FIG. 1 ).
  • coverplate 110 and seal 108 can be installed on the forward side and the aft side of wheel 104 .
  • Angel wing 112 may aid in preventing the hot flowpath gas from entering wheelspace 314 .
  • wheelspace purge air 312 is able to enter perforation 316 in wheel 104 .
  • coverplate 110 and seal 108 it may reduce or eliminate the amount of wheelspace purge air 312 entering or moving through wheel 104 into wheelspace 314 .
  • wheelspace purge air 310 would be able to move between wheel 104 and wheelspace 314 .
  • Coverplate 110 and seal 108 aid in preventing the loss of wheelspace purge air 312 .
  • bucket supply cooling air may enter wheelspace 314 .
  • coverplate 110 may be segmented.
  • seal 108 may be segmented.
  • both coverplate 110 and seal 108 may be segmented.
  • seal 108 is positioned to overlap an interface 804 on segment coverplate 806 to eliminate a gap between adjacent circumferentially positioned coverplate segments 802 .
  • Coverplate 110 and seal 108 can also be used to aid in the secondary flow design of machine 100 .
  • coverplate 110 and seal 108 can be installed and positioned to aid in the movement of air and gas flow to directed locations.
  • coverplate 110 and seal 108 can be installed and positioned to prevent leakages of pressurized air (e.g., wheelspace purge air and bucket supply cooling air) and ingestion of hot gas.
  • coverplate 110 and seal 108 can be used as a heat shield for wheel 104 by reducing the amount of hot gas flow 308 that contacts or comes in proximity to wheel 104 or by providing an additional barrier between bucket 102 and wheel 104 .
  • coverplate 110 and seal 108 can be used to dampen vibration on wheel 104 and bucket 102 and for machine 100 as a whole.
  • coverplate 110 and seal 108 can provide an additional mechanical connection between wheel 104 and bucket 102 .
  • the additional connection between bucket 102 and wheel 104 may provide increased rigidity and reduce the vibration while machine 100 is in operation.
  • a 360-degree single coil seal with a single split (“single coil seal”) 402 is shown.
  • the single coil seal 402 allows for installation and maintenance, including assembly and disassembly, on machine 100 both at the factory and when machine 100 is at a customer's site.
  • the single coil seal 402 allows for the seal to be spread apart allowing for maintenance and repair of machine 100 .
  • by single coil seal 402 having a break in its circumference it provides the flexibility so that it may be maneuvered on and off of machine 100 .
  • single coil seal 402 with its single split retains the rigidity and durability where it can perform as described in detail above, and be installed and removed from machine 100 .
  • single coil seal 502 can be mechanically coupled by, for example, a tongue and groove, a lap joint, a dovetail, a butt joint, a weld or a braze. Additionally, a coverplate 504 can be placed over the joint in the single coil seal 502 when it is mechanically coupled. In one embodiment, a mechanically coupled single coil seal with a coverplate 504 will have the single coil seal 402 positioned on the coverplate 504 to eliminate a gap 506 between adjacent circumferentially positioned coverplate segments 504 .
  • FIG. 6 illustrates a 720-degree multi coil seal (“multi coil seal”) 602 .
  • the ends of the multi coil seal are not mechanically coupled to one another. This allows for flexibility in the seal during installation and maintenance of machine 100 in addition to installation and removal of multi coil seal 602 on machine 100 .
  • Other embodiments may include a multi coil seal having more than 720 degrees, if desired.
  • Segmented seal 700 includes a joint 702 where segments 704 connect.
  • a coverplate 110 can be installed over a segmented seal 700 .
  • FIG. 8 shows a segmented seal 700 with a segmented coverplate 806 over segmented seal 700 .
  • a coverplate joint 804 can be staggered from joint 702 of segmented seal 700 where the segmented seal 700 is positioned on the coverplate segment 804 to eliminate a gap between adjacent circumferentially positioned coverplate segments.
  • FIG. 9 this figure illustrates an alternative embodiment wherein a seal 904 extends along a side of bucket 102 and wheel 104 covering an interface therebetween.
  • Seal 904 may attach to bucket 102 by a hook 902 on bucket 102 and seal 904 may attach to wheel 104 by a hook 906 on wheel 104 .
  • Seal 904 may be on the forward or aft side of wheel 104 .
  • seal 904 may be may be on the forward and aft side of wheel 104 .
  • Seal 904 may take the form of any of the above-described seals.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A machine and a seal assembly for a machine having a rotating shaft, a wheel coupled to the rotating shaft, the wheel including a bucket coupled to the wheel comprising a seal that extends along a side of the bucket and the wheel, covering an interface there between.

Description

    CROSS-REFERENCE TO RELATED APPLICATION
  • The current application is related to U.S. patent application Ser. No. ______, titled “GAS TURBINE HAVING SEAL ASSEMBLY WITH COVERPLATE AND SEAL,” filed on Mar. , 2009.
  • BACKGROUND OF THE INVENTION
  • The subject matter disclosed herein relates generally to machines and a seal assembly for machines and more specifically to a seal assembly to improve the operation, performance and efficiency of a machine. Machine performance is degraded by the loss of pressurized cooling air and ingestion of hot gas flow.
  • BRIEF DESCRIPTION OF THE INVENTION
  • A machine and a seal assembly for a machine having a rotating shaft, a wheel coupled to the rotating shaft, the wheel including a bucket coupled to the wheel comprising: a seal that extends along a side of the bucket and the wheel, covering an interface there between.
  • A first aspect of the invention provides a machine comprising: a rotating shaft, a wheel coupled to the rotating shaft, the wheel including a bucket coupled to the wheel, and a seal that extends along a side of the bucket and the wheel, covering an interface there between.
  • A second aspect of the invention provides a seal assembly for a machine having a rotating shaft, the seal assembly comprising: a wheel coupled to the rotating shaft, the wheel including a bucket coupled to the wheel; and a seal that extends along a side of the bucket and the wheel, covering an interface there between.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • These and other features of the disclosure will be more readily understood from the following detailed description of the various aspects of the invention taken in conjunction with the accompanying drawings that depict various aspects of the invention, in which:
  • FIG. 1 shows a cross-sectional view of a bucket and wheel from a machine.
  • FIG. 2 shows a cross-sectional view of a bucket and wheel from a machine with an enlarged view from an area of FIG. 1 illustrating a coverplate and seal.
  • FIG. 3 shows a cross-sectional view of a machine showing gas and air flow movement.
  • FIG. 4 shows a 360-degree single coil seal with a single split.
  • FIG. 5 shows a 360-degree single coil seal with a single split wherein the ends of the split are mechanically coupled and there is a segmented coverplate over the mechanically coupled ends of the single coil seal.
  • FIG. 6 shows a 720-degree multi-coil seal.
  • FIG. 7 shows a portion of a segmented seal.
  • FIG. 8 shows a portion of a segmented seal with a segmented coverplate over the segmented seal.
  • FIG. 9 shows a cross sectional view of a bucket and wheel from a machine.
  • It is noted that the drawings are not to scale. The drawings are intended to depict only typical aspects of the invention, and therefore should not be considered as limiting the scope of the invention. In the drawings, like numbering represents like elements between the drawings.
  • DETAILED DESCRIPTION OF THE INVENTION
  • As indicated above, aspects of the invention provide improved operation, performance and efficiency of a machine. As used throughout this application, reference to machine is to include: a gas turbine, a steam turbine or a compressor. In one embodiment, the invention discussed herein includes a coverplate that is fastened to a wheel and bucket of a machine and a seal positioned between the coverplate and the wheel and the bucket. One feature of the coverplate and seal on the machine is that it reduces the loss of pressurized air from the system. Additionally, the coverplate and seal may prevent the inflow of hot gas into the wheelspace and aid in the secondary air flow of the machine. Moreover, the coverplate and seal discussed herein may facilitate maintenance on the machine. Furthermore, the coverplate and seal may facilitate assembly and disassembly of the machine as the coverplate and seal can be installed and removed while the rotating shaft is on the half shell. The coverplate and seal may also improve the machine's performance by acting as a heat shield and reduce vibration through the addition of damping. The coverplate and seal can be installed on a forward side or an aft side of the wheel. Alternatively, the coverplate and seal can be installed on the forward side and the aft side of the wheel.
  • Turning to the drawings, FIG. 1 shows a cross-sectional view of a relevant portion of a machine 100 including seal assembly 101. Machine 100 includes a bucket 102, a wheel 104 and a rotating shaft 106. As understood, at least one wheel 104 is coupled to rotating shaft 106 of machine 100. Each wheel 104 may include a plurality of buckets 102 upon which gas acts to turn rotating shaft 106.
  • FIG. 2 shows an enlarged view of a relevant portion of FIG. 1. Seal assembly 101 includes a seal 108, a coverplate 110 and an angel wing 112. In one embodiment, coverplate 110 fastens to wheel 104 of machine 100 using a hook 206. Alternative embodiments for fastening coverplate 110 to wheel 104 may include, for example: a bolt, a pin, a stack or a bayonet retaining ring. In another embodiment, coverplate 110 can include an outer edge 208 that engages a slot 210 in bucket 102 of machine 100.
  • FIG. 3 shows a cross-sectional view of machine 100 showing gas and air flow movement. FIG. 3 shows a nozzle 302 of machine 100. As illustrated, nozzle 302 is located on both sides of bucket 102. It is understood, however, that nozzle 302 would be present only on a forward side of bucket 102 where the bucket is a last stage bucket. A hot gas flow 308 moves across bucket 102. Immediately below nozzle 302 on the forward (left) or upstream side of machine 100 is a nozzle support ring 304. Immediately below nozzle 302 on the aft (right) or downstream side of machine 100 is a diaphragm 306. Nozzle 302 includes on both the forward and aft sides, a part 305 that extends from nozzle 302 towards wheel 104. A wheelspace 314 exists on the forward and aft side of bucket 102. On the forward side, wheelspace 314 is between nozzle supporting ring 304 and wheel 104. On the aft side, wheelspace 314 is between diaphragm 306 and wheel 104.
  • Wheelspace purge air 312 moves through wheelspace 314. Additionally, bucket supply cooling air (not shown) moves from wheel 104 towards bucket 102. An illustration of the movement of wheelspace purge air 312 is shown as it moves through wheelspace 314 and across wheel 104. Coverplate 110 aids in reducing the amount of wheelspace purge air 312 that is able to move between wheel 104 and nozzle support ring 304 on the forward side and wheel 104 and diaphragm 306 on the aft side. Additionally, coverplate 110 aids in the bucket supply cooling air reaching bucket 102 and not entering wheelspace 314. As described above, in one embodiment coverplate 110 and seal 108 can be installed on a forward side or an aft side of wheel 104 (FIG. 1). In another embodiment, coverplate 110 and seal 108 can be installed on the forward side and the aft side of wheel 104. Additionally, there may be one or more angel wings 112 on coverplate 110. Angel wing 112 may aid in preventing the hot flowpath gas from entering wheelspace 314.
  • When there is no coverplate 110 and seal 108 present, wheelspace purge air 312 is able to enter perforation 316 in wheel 104. When coverplate 110 and seal 108 are present, it may reduce or eliminate the amount of wheelspace purge air 312 entering or moving through wheel 104 into wheelspace 314. If no coverplate 110 and seal 108 are installed, wheelspace purge air 310 would be able to move between wheel 104 and wheelspace 314. Coverplate 110 and seal 108 aid in preventing the loss of wheelspace purge air 312. Moreover, when there is no coverplate 110 and seal 108 present, bucket supply cooling air may enter wheelspace 314.
  • In one embodiment, coverplate 110 may be segmented. In another embodiment, seal 108 may be segmented. In a further embodiment, both coverplate 110 and seal 108 may be segmented. In an alternative embodiment, shown in FIG. 8, where there is a segmented coverplate 806 and a segmented seal 700 or either segmented coverplate 806 or segmented seal 700, seal 108 is positioned to overlap an interface 804 on segment coverplate 806 to eliminate a gap between adjacent circumferentially positioned coverplate segments 802.
  • Coverplate 110 and seal 108 can also be used to aid in the secondary flow design of machine 100. Specifically, coverplate 110 and seal 108 can be installed and positioned to aid in the movement of air and gas flow to directed locations. Moreover, coverplate 110 and seal 108 can be installed and positioned to prevent leakages of pressurized air (e.g., wheelspace purge air and bucket supply cooling air) and ingestion of hot gas. Additionally, coverplate 110 and seal 108 can be used as a heat shield for wheel 104 by reducing the amount of hot gas flow 308 that contacts or comes in proximity to wheel 104 or by providing an additional barrier between bucket 102 and wheel 104. In a further embodiment, coverplate 110 and seal 108 can be used to dampen vibration on wheel 104 and bucket 102 and for machine 100 as a whole. For example, coverplate 110 and seal 108 can provide an additional mechanical connection between wheel 104 and bucket 102. The additional connection between bucket 102 and wheel 104 may provide increased rigidity and reduce the vibration while machine 100 is in operation.
  • Turning to FIG. 4, a 360-degree single coil seal with a single split (“single coil seal”) 402 is shown. The single coil seal 402 allows for installation and maintenance, including assembly and disassembly, on machine 100 both at the factory and when machine 100 is at a customer's site. In one embodiment, the single coil seal 402 allows for the seal to be spread apart allowing for maintenance and repair of machine 100. In a further embodiment, by single coil seal 402 having a break in its circumference, it provides the flexibility so that it may be maneuvered on and off of machine 100. In another embodiment, single coil seal 402 with its single split retains the rigidity and durability where it can perform as described in detail above, and be installed and removed from machine 100.
  • Turning to FIG. 5, and with continuing reference to FIG. 4, the ends of single coil seal 502 can be mechanically coupled by, for example, a tongue and groove, a lap joint, a dovetail, a butt joint, a weld or a braze. Additionally, a coverplate 504 can be placed over the joint in the single coil seal 502 when it is mechanically coupled. In one embodiment, a mechanically coupled single coil seal with a coverplate 504 will have the single coil seal 402 positioned on the coverplate 504 to eliminate a gap 506 between adjacent circumferentially positioned coverplate segments 504.
  • FIG. 6 illustrates a 720-degree multi coil seal (“multi coil seal”) 602. In one embodiment, the ends of the multi coil seal are not mechanically coupled to one another. This allows for flexibility in the seal during installation and maintenance of machine 100 in addition to installation and removal of multi coil seal 602 on machine 100. Other embodiments may include a multi coil seal having more than 720 degrees, if desired.
  • Turning to FIG. 7, a portion of a segmented seal 700 is illustrated. Segmented seal 700 includes a joint 702 where segments 704 connect. In one embodiment, a coverplate 110 can be installed over a segmented seal 700. FIG. 8 shows a segmented seal 700 with a segmented coverplate 806 over segmented seal 700. Examining FIG. 8, with continuing reference to FIG. 7, in one embodiment a coverplate joint 804 can be staggered from joint 702 of segmented seal 700 where the segmented seal 700 is positioned on the coverplate segment 804 to eliminate a gap between adjacent circumferentially positioned coverplate segments.
  • Turning to FIG. 9, this figure illustrates an alternative embodiment wherein a seal 904 extends along a side of bucket 102 and wheel 104 covering an interface therebetween. Seal 904 may attach to bucket 102 by a hook 902 on bucket 102 and seal 904 may attach to wheel 104 by a hook 906 on wheel 104. Seal 904 may be on the forward or aft side of wheel 104. In an additional embodiment, seal 904 may be may be on the forward and aft side of wheel 104. Seal 904 may take the form of any of the above-described seals.
  • While various embodiments are described herein, it will be appreciated from the specification that various combinations of elements, variations or improvements therein may be made by those skilled in the art, and are within the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.

Claims (18)

1. A machine comprising:
a rotating shaft;
a wheel coupled to the rotating shaft;
a bucket coupled to the wheel; and
a seal that extends along a side of the bucket and the wheel, covering an interface therebetween.
2. The machine of claim 1, wherein the bucket includes a hook for fastening the seal to the bucket of the machine.
3. The machine of claim 1, wherein the wheel includes a hook for fastening the seal to the wheel of the machine.
4. The machine of claim 1, wherein the seal includes a 360-degree seal with a single split.
5. The machine of claim 1, wherein the seal includes a 720-degree multi-coil seal.
6. The machine of claim 1, wherein the seal includes a segmented seal.
7. The machine of claim 1, wherein the seal is installed on a forward side of the wheel.
8. The machine of claim 1, wherein the seal is installed on an aft side of the wheel.
9. The machine of claim 1, wherein the seal is installed on the forward side and the aft side of the wheel.
10. A seal assembly for a machine having a rotating shaft, the seal assembly comprising:
a wheel coupled to the rotating shaft;
a bucket coupled to the wheel; and
a seal that extends along a side of the bucket and the wheel, covering an interface therebetween.
11. The seal assembly of claim 10, wherein the bucket includes a hook for fastening the seal to the bucket of the machine.
12. The seal assembly of claim 10, wherein the wheel includes a hook for fastening the seal to the wheel of the machine.
13. The seal assembly of claim 10, wherein the seal includes a 360-degree seal with a single split.
14. The seal assembly of claim 10, wherein the seal includes a 720-degree multi-coil seal.
15. The seal assembly of claim 10, wherein the seal includes a segmented seal.
16. The seal assembly of claim 10, wherein the seal is installed on a forward side of the wheel.
17. The seal assembly of claim 10, wherein the seal is installed on an aft side of the wheel.
18. The seal assembly of claim 10, wherein the seal is installed on the forward side and the aft side of the wheel.
US12/402,808 2009-03-12 2009-03-12 Machine Seal Assembly Abandoned US20100232939A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US12/402,808 US20100232939A1 (en) 2009-03-12 2009-03-12 Machine Seal Assembly
EP10155312.1A EP2236768A3 (en) 2009-03-12 2010-03-03 Turbomachine seal assembly
JP2010052474A JP5475511B2 (en) 2009-03-12 2010-03-10 Mechanical seal assembly
CN2010101468881A CN101893001A (en) 2009-03-12 2010-03-12 Turbomachine seal assembly

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Application Number Priority Date Filing Date Title
US12/402,808 US20100232939A1 (en) 2009-03-12 2009-03-12 Machine Seal Assembly

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US20100232939A1 true US20100232939A1 (en) 2010-09-16

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EP (1) EP2236768A3 (en)
JP (1) JP5475511B2 (en)
CN (1) CN101893001A (en)

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US20100239413A1 (en) * 2009-03-23 2010-09-23 General Electric Company Apparatus for turbine engine cooling air management
US20100239414A1 (en) * 2009-03-23 2010-09-23 General Electric Company Apparatus for turbine engine cooling air management
US20130094969A1 (en) * 2011-10-17 2013-04-18 General Electric Company System for sealing a shaft
US8845284B2 (en) 2010-07-02 2014-09-30 General Electric Company Apparatus and system for sealing a turbine rotor
US8864453B2 (en) 2012-01-20 2014-10-21 General Electric Company Near flow path seal for a turbomachine
US9080456B2 (en) 2012-01-20 2015-07-14 General Electric Company Near flow path seal with axially flexible arms
US9217334B2 (en) 2011-10-26 2015-12-22 General Electric Company Turbine cover plate assembly
US20170107837A1 (en) * 2015-10-20 2017-04-20 General Electric Company Turbine slotted arcuate leaf seal
US10337344B2 (en) * 2014-05-27 2019-07-02 Siemens Aktiengesellschaft Turbomachine with an ingestion shield and use of the turbomachine

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FR2999641B1 (en) * 2012-12-17 2014-12-26 Snecma TURBOMACHINE FLOOR
EP3438410B1 (en) 2017-08-01 2021-09-29 General Electric Company Sealing system for a rotary machine
FI129562B (en) * 2019-06-24 2022-04-29 Flaektgroup Sweden Ab Method of forming a sealing between ventilation pipes and/or terminals thereof, and sealing

Citations (55)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3043562A (en) * 1961-04-10 1962-07-10 Gen Electric Combination sealing and restraining member for long-shank turbo-machine buckets
US3137478A (en) * 1962-07-11 1964-06-16 Gen Electric Cover plate assembly for sealing spaces between turbine buckets
US3501249A (en) * 1968-06-24 1970-03-17 Westinghouse Electric Corp Side plates for turbine blades
US3751183A (en) * 1971-12-02 1973-08-07 Gen Electric Interblade baffle and damper
US3768924A (en) * 1971-12-06 1973-10-30 Gen Electric Boltless blade and seal retainer
US3814539A (en) * 1972-10-04 1974-06-04 Gen Electric Rotor sealing arrangement for an axial flow fluid turbine
US3829233A (en) * 1973-06-27 1974-08-13 Westinghouse Electric Corp Turbine diaphragm seal structure
US3853425A (en) * 1973-09-07 1974-12-10 Westinghouse Electric Corp Turbine rotor blade cooling and sealing system
US4019833A (en) * 1974-11-06 1977-04-26 Rolls-Royce (1971) Limited Means for retaining blades to a disc or like structure
US4021138A (en) * 1975-11-03 1977-05-03 Westinghouse Electric Corporation Rotor disk, blade, and seal plate assembly for cooled turbine rotor blades
US4088421A (en) * 1976-09-30 1978-05-09 General Electric Company Coverplate damping arrangement
US4218189A (en) * 1977-08-09 1980-08-19 Rolls-Royce Limited Sealing means for bladed rotor for a gas turbine engine
US4265594A (en) * 1978-03-02 1981-05-05 Bbc Brown Boveri & Company Limited Turbine blade having heat localization segments
US4326835A (en) * 1979-10-29 1982-04-27 General Motors Corporation Blade platform seal for ceramic/metal rotor assembly
US4480958A (en) * 1983-02-09 1984-11-06 The United States Of America As Represented By The Secretary Of The Air Force High pressure turbine rotor two-piece blade retainer
US4500098A (en) * 1983-12-22 1985-02-19 United Technologies Corporation Gas seal for rotating components
US4507052A (en) * 1983-03-31 1985-03-26 General Motors Corporation End seal for turbine blade bases
US4523890A (en) * 1983-10-19 1985-06-18 General Motors Corporation End seal for turbine blade base
US4645424A (en) * 1984-07-23 1987-02-24 United Technologies Corporation Rotating seal for gas turbine engine
US4659285A (en) * 1984-07-23 1987-04-21 United Technologies Corporation Turbine cover-seal assembly
US4659289A (en) * 1984-07-23 1987-04-21 United Technologies Corporation Turbine side plate assembly
US4743164A (en) * 1986-12-29 1988-05-10 United Technologies Corporation Interblade seal for turbomachine rotor
US4781534A (en) * 1987-02-27 1988-11-01 Westinghouse Electric Corp. Apparatus and method for reducing windage and leakage in steam turbine incorporating axial entry blade
US5222742A (en) * 1990-12-22 1993-06-29 Rolls-Royce Plc Seal arrangement
US5236302A (en) * 1991-10-30 1993-08-17 General Electric Company Turbine disk interstage seal system
US5257909A (en) * 1992-08-17 1993-11-02 General Electric Company Dovetail sealing device for axial dovetail rotor blades
US5275534A (en) * 1991-10-30 1994-01-04 General Electric Company Turbine disk forward seal assembly
US5277548A (en) * 1991-12-31 1994-01-11 United Technologies Corporation Non-integral rotor blade platform
US5338154A (en) * 1993-03-17 1994-08-16 General Electric Company Turbine disk interstage seal axial retaining ring
US5429478A (en) * 1994-03-31 1995-07-04 United Technologies Corporation Airfoil having a seal and an integral heat shield
US5503528A (en) * 1993-12-27 1996-04-02 Solar Turbines Incorporated Rim seal for turbine wheel
US5803710A (en) * 1996-12-24 1998-09-08 United Technologies Corporation Turbine engine rotor blade platform sealing and vibration damping device
US5954477A (en) * 1996-09-26 1999-09-21 Rolls-Royce Plc Seal plate
US5967745A (en) * 1997-03-18 1999-10-19 Mitsubishi Heavy Industries, Ltd. Gas turbine shroud and platform seal system
US5993160A (en) * 1997-12-11 1999-11-30 Pratt & Whitney Canada Inc. Cover plate for gas turbine rotor
US6086329A (en) * 1997-03-12 2000-07-11 Mitsubishi Heavy Industries, Ltd. Seal plate for a gas turbine moving blade
US6106234A (en) * 1997-12-03 2000-08-22 Rolls-Royce Plc Rotary assembly
US6120249A (en) * 1994-10-31 2000-09-19 Siemens Westinghouse Power Corporation Gas turbine blade platform cooling concept
US6189891B1 (en) * 1997-03-12 2001-02-20 Mitsubishi Heavy Industries, Ltd. Gas turbine seal apparatus
US6190131B1 (en) * 1999-08-31 2001-02-20 General Electric Co. Non-integral balanced coverplate and coverplate centering slot for a turbine
US6220814B1 (en) * 1998-07-16 2001-04-24 Siemens Westinghouse Power Corporation Turbine interstage sealing arrangement
US6273683B1 (en) * 1999-02-05 2001-08-14 Siemens Westinghouse Power Corporation Turbine blade platform seal
US6315298B1 (en) * 1999-11-22 2001-11-13 United Technologies Corporation Turbine disk and blade assembly seal
US6506016B1 (en) * 2001-11-15 2003-01-14 General Electric Company Angel wing seals for blades of a gas turbine and methods for determining angel wing seal profiles
US6561764B1 (en) * 1999-03-19 2003-05-13 Siemens Aktiengesellschaft Gas turbine rotor with an internally cooled gas turbine blade and connecting configuration including an insert strip bridging adjacent blade platforms
US6776573B2 (en) * 2000-11-30 2004-08-17 Snecma Moteurs Bladed rotor disc side-plate and corresponding arrangement
US6945749B2 (en) * 2003-09-12 2005-09-20 Siemens Westinghouse Power Corporation Turbine blade platform cooling system
US20060021218A1 (en) * 2002-08-23 2006-02-02 Mcmillan Alison J Seals and a method of making seals
US7121800B2 (en) * 2004-09-13 2006-10-17 United Technologies Corporation Turbine blade nested seal damper assembly
US7189055B2 (en) * 2005-05-31 2007-03-13 Pratt & Whitney Canada Corp. Coverplate deflectors for redirecting a fluid flow
US7241109B2 (en) * 2004-06-04 2007-07-10 Rolls-Royce Plc Seal system
US7264448B2 (en) * 2004-10-06 2007-09-04 Siemens Power Corporation, Inc. Remotely accessible locking system for turbine blades
US7264447B2 (en) * 2003-12-05 2007-09-04 Honda Motor Co., Ltd. Sealing arrangement for an axial turbine wheel
US20070258816A1 (en) * 2005-09-26 2007-11-08 Pratt & Whitney Canada Corp. Blades for a gas turbine engine with integrated sealing plate and method
US20100196164A1 (en) * 2009-02-05 2010-08-05 General Electric Company Turbine Coverplate Systems

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1291302A (en) * 1970-03-14 1972-10-04 Sec Dep For Defendence Improvements in bladed rotor assemblies
JPS61205303A (en) * 1985-03-06 1986-09-11 Mitsubishi Heavy Ind Ltd Stopper in axial direction for turbine moving blade
JPH0723524Y2 (en) * 1988-03-29 1995-05-31 川崎重工業株式会社 Axial turbine
US6669443B2 (en) * 2001-11-16 2003-12-30 General Electric Company Rotor platform modification and methods using brush seals in diaphragm packing area of steam turbines to eliminate rotor bowing
US6884028B2 (en) * 2002-09-30 2005-04-26 General Electric Company Turbomachinery blade retention system
US6779972B2 (en) * 2002-10-31 2004-08-24 General Electric Company Flowpath sealing and streamlining configuration for a turbine
JP2006009576A (en) * 2004-06-22 2006-01-12 Matsushita Electric Ind Co Ltd Scroll compressor
JP2006266454A (en) * 2005-03-25 2006-10-05 Matsumura Koki Kk Ring and sealing structure
JP4035140B2 (en) * 2005-07-22 2008-01-16 川崎重工業株式会社 Turbine rotor seal ring
US7465152B2 (en) * 2005-09-16 2008-12-16 General Electric Company Angel wing seals for turbine blades and methods for selecting stator, rotor and wing seal profiles
US20070114727A1 (en) * 2005-11-21 2007-05-24 General Electric Company Seal member, assembly and method
DE602006006452D1 (en) * 2006-09-25 2009-06-04 Siemens Ag Turbine rotor with closure plates and corresponding assembly process

Patent Citations (55)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3043562A (en) * 1961-04-10 1962-07-10 Gen Electric Combination sealing and restraining member for long-shank turbo-machine buckets
US3137478A (en) * 1962-07-11 1964-06-16 Gen Electric Cover plate assembly for sealing spaces between turbine buckets
US3501249A (en) * 1968-06-24 1970-03-17 Westinghouse Electric Corp Side plates for turbine blades
US3751183A (en) * 1971-12-02 1973-08-07 Gen Electric Interblade baffle and damper
US3768924A (en) * 1971-12-06 1973-10-30 Gen Electric Boltless blade and seal retainer
US3814539A (en) * 1972-10-04 1974-06-04 Gen Electric Rotor sealing arrangement for an axial flow fluid turbine
US3829233A (en) * 1973-06-27 1974-08-13 Westinghouse Electric Corp Turbine diaphragm seal structure
US3853425A (en) * 1973-09-07 1974-12-10 Westinghouse Electric Corp Turbine rotor blade cooling and sealing system
US4019833A (en) * 1974-11-06 1977-04-26 Rolls-Royce (1971) Limited Means for retaining blades to a disc or like structure
US4021138A (en) * 1975-11-03 1977-05-03 Westinghouse Electric Corporation Rotor disk, blade, and seal plate assembly for cooled turbine rotor blades
US4088421A (en) * 1976-09-30 1978-05-09 General Electric Company Coverplate damping arrangement
US4218189A (en) * 1977-08-09 1980-08-19 Rolls-Royce Limited Sealing means for bladed rotor for a gas turbine engine
US4265594A (en) * 1978-03-02 1981-05-05 Bbc Brown Boveri & Company Limited Turbine blade having heat localization segments
US4326835A (en) * 1979-10-29 1982-04-27 General Motors Corporation Blade platform seal for ceramic/metal rotor assembly
US4480958A (en) * 1983-02-09 1984-11-06 The United States Of America As Represented By The Secretary Of The Air Force High pressure turbine rotor two-piece blade retainer
US4507052A (en) * 1983-03-31 1985-03-26 General Motors Corporation End seal for turbine blade bases
US4523890A (en) * 1983-10-19 1985-06-18 General Motors Corporation End seal for turbine blade base
US4500098A (en) * 1983-12-22 1985-02-19 United Technologies Corporation Gas seal for rotating components
US4659285A (en) * 1984-07-23 1987-04-21 United Technologies Corporation Turbine cover-seal assembly
US4645424A (en) * 1984-07-23 1987-02-24 United Technologies Corporation Rotating seal for gas turbine engine
US4659289A (en) * 1984-07-23 1987-04-21 United Technologies Corporation Turbine side plate assembly
US4743164A (en) * 1986-12-29 1988-05-10 United Technologies Corporation Interblade seal for turbomachine rotor
US4781534A (en) * 1987-02-27 1988-11-01 Westinghouse Electric Corp. Apparatus and method for reducing windage and leakage in steam turbine incorporating axial entry blade
US5222742A (en) * 1990-12-22 1993-06-29 Rolls-Royce Plc Seal arrangement
US5236302A (en) * 1991-10-30 1993-08-17 General Electric Company Turbine disk interstage seal system
US5275534A (en) * 1991-10-30 1994-01-04 General Electric Company Turbine disk forward seal assembly
US5277548A (en) * 1991-12-31 1994-01-11 United Technologies Corporation Non-integral rotor blade platform
US5257909A (en) * 1992-08-17 1993-11-02 General Electric Company Dovetail sealing device for axial dovetail rotor blades
US5338154A (en) * 1993-03-17 1994-08-16 General Electric Company Turbine disk interstage seal axial retaining ring
US5503528A (en) * 1993-12-27 1996-04-02 Solar Turbines Incorporated Rim seal for turbine wheel
US5429478A (en) * 1994-03-31 1995-07-04 United Technologies Corporation Airfoil having a seal and an integral heat shield
US6120249A (en) * 1994-10-31 2000-09-19 Siemens Westinghouse Power Corporation Gas turbine blade platform cooling concept
US5954477A (en) * 1996-09-26 1999-09-21 Rolls-Royce Plc Seal plate
US5803710A (en) * 1996-12-24 1998-09-08 United Technologies Corporation Turbine engine rotor blade platform sealing and vibration damping device
US6189891B1 (en) * 1997-03-12 2001-02-20 Mitsubishi Heavy Industries, Ltd. Gas turbine seal apparatus
US6086329A (en) * 1997-03-12 2000-07-11 Mitsubishi Heavy Industries, Ltd. Seal plate for a gas turbine moving blade
US5967745A (en) * 1997-03-18 1999-10-19 Mitsubishi Heavy Industries, Ltd. Gas turbine shroud and platform seal system
US6106234A (en) * 1997-12-03 2000-08-22 Rolls-Royce Plc Rotary assembly
US5993160A (en) * 1997-12-11 1999-11-30 Pratt & Whitney Canada Inc. Cover plate for gas turbine rotor
US6220814B1 (en) * 1998-07-16 2001-04-24 Siemens Westinghouse Power Corporation Turbine interstage sealing arrangement
US6273683B1 (en) * 1999-02-05 2001-08-14 Siemens Westinghouse Power Corporation Turbine blade platform seal
US6561764B1 (en) * 1999-03-19 2003-05-13 Siemens Aktiengesellschaft Gas turbine rotor with an internally cooled gas turbine blade and connecting configuration including an insert strip bridging adjacent blade platforms
US6190131B1 (en) * 1999-08-31 2001-02-20 General Electric Co. Non-integral balanced coverplate and coverplate centering slot for a turbine
US6315298B1 (en) * 1999-11-22 2001-11-13 United Technologies Corporation Turbine disk and blade assembly seal
US6776573B2 (en) * 2000-11-30 2004-08-17 Snecma Moteurs Bladed rotor disc side-plate and corresponding arrangement
US6506016B1 (en) * 2001-11-15 2003-01-14 General Electric Company Angel wing seals for blades of a gas turbine and methods for determining angel wing seal profiles
US20060021218A1 (en) * 2002-08-23 2006-02-02 Mcmillan Alison J Seals and a method of making seals
US6945749B2 (en) * 2003-09-12 2005-09-20 Siemens Westinghouse Power Corporation Turbine blade platform cooling system
US7264447B2 (en) * 2003-12-05 2007-09-04 Honda Motor Co., Ltd. Sealing arrangement for an axial turbine wheel
US7241109B2 (en) * 2004-06-04 2007-07-10 Rolls-Royce Plc Seal system
US7121800B2 (en) * 2004-09-13 2006-10-17 United Technologies Corporation Turbine blade nested seal damper assembly
US7264448B2 (en) * 2004-10-06 2007-09-04 Siemens Power Corporation, Inc. Remotely accessible locking system for turbine blades
US7189055B2 (en) * 2005-05-31 2007-03-13 Pratt & Whitney Canada Corp. Coverplate deflectors for redirecting a fluid flow
US20070258816A1 (en) * 2005-09-26 2007-11-08 Pratt & Whitney Canada Corp. Blades for a gas turbine engine with integrated sealing plate and method
US20100196164A1 (en) * 2009-02-05 2010-08-05 General Electric Company Turbine Coverplate Systems

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100239413A1 (en) * 2009-03-23 2010-09-23 General Electric Company Apparatus for turbine engine cooling air management
US20100239414A1 (en) * 2009-03-23 2010-09-23 General Electric Company Apparatus for turbine engine cooling air management
US8142141B2 (en) * 2009-03-23 2012-03-27 General Electric Company Apparatus for turbine engine cooling air management
US8277172B2 (en) 2009-03-23 2012-10-02 General Electric Company Apparatus for turbine engine cooling air management
US8845284B2 (en) 2010-07-02 2014-09-30 General Electric Company Apparatus and system for sealing a turbine rotor
US20130094969A1 (en) * 2011-10-17 2013-04-18 General Electric Company System for sealing a shaft
US9217334B2 (en) 2011-10-26 2015-12-22 General Electric Company Turbine cover plate assembly
US8864453B2 (en) 2012-01-20 2014-10-21 General Electric Company Near flow path seal for a turbomachine
US9080456B2 (en) 2012-01-20 2015-07-14 General Electric Company Near flow path seal with axially flexible arms
US10337344B2 (en) * 2014-05-27 2019-07-02 Siemens Aktiengesellschaft Turbomachine with an ingestion shield and use of the turbomachine
US20170107837A1 (en) * 2015-10-20 2017-04-20 General Electric Company Turbine slotted arcuate leaf seal
US10161257B2 (en) * 2015-10-20 2018-12-25 General Electric Company Turbine slotted arcuate leaf seal

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JP5475511B2 (en) 2014-04-16
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EP2236768A2 (en) 2010-10-06
EP2236768A3 (en) 2014-12-24

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