CA2559618A1 - Pneumatic press vane lift installation tool - Google Patents
Pneumatic press vane lift installation tool Download PDFInfo
- Publication number
- CA2559618A1 CA2559618A1 CA002559618A CA2559618A CA2559618A1 CA 2559618 A1 CA2559618 A1 CA 2559618A1 CA 002559618 A CA002559618 A CA 002559618A CA 2559618 A CA2559618 A CA 2559618A CA 2559618 A1 CA2559618 A1 CA 2559618A1
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- CA
- Canada
- Prior art keywords
- tube
- tool
- inflatable
- vanes
- array
- 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
Links
- 238000009434 installation Methods 0.000 title abstract description 21
- 239000012530 fluid Substances 0.000 claims description 5
- 239000000463 material Substances 0.000 claims description 4
- 229920002457 flexible plastic Polymers 0.000 claims description 3
- 238000000034 method Methods 0.000 description 8
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000004677 Nylon Substances 0.000 description 1
- 238000003491 array Methods 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
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- Turbine Rotor Nozzle Sealing (AREA)
Abstract
The present invention relates to a pneumatic press vane lift installation tool. The tool is formed by two inflatable, substantially semi-circular tubes which are placed between a rotor assembly and a vane assembly during the installation of the vane assembly. The tubes are each positioned adjacent an inner end of the vanes in the vane assembly and are each inflated to apply a lifting force to the vanes. The vanes are then attached to the engine case.
Description
PNEUMATIC PRESS VANE LIFT INSTALLATION TOOL
BACKGROUND OF THE INVENTION
The present invention relates to a tool for installing stator vanes in a turbine engine and a method of using same.
Turbine engines are typically formed by stacking rotor and stator vane assemblies one on top of another and by attaching the stator vanes to an engine case. Newer engines utilize a one-piece engine case rather than the previous split-case design. This has resulted in a blind operation during the attachment of the stator vanes to the engine case which can impact how well the stator vanes are attached to the engine case. It is important that the stator vanes be held tightly against the case during installation to prevent unwanted vibration during engine operation. Prior tools which have been used to install the stator vanes can not be used with the one-piece engine case. Thus, there is a need for an installation tool which will help insure the proper installation of stator vanes in a one-piece engine case.
SUMMARY OF THE INVENTION
Accordingly, it is an object of the present invention to provide an installation tool which can be used to properly position stator vanes for attachment to an engine case.
It is a further object of the present invention to provide an improved method for installing stator vanes in an engine case.
The foregoing objects are attained by the installation tool and the method of the present invention.
In accordance with the present invention, a pneumatic press vane lift installation tool is described. The tool is formed by two inflatable, semi-circular tubes which are placed between a rotor assembly and a stator vane assembly during the installation of the stator vane assembly. The tubes are each positioned adjacent an inner end of the stator vanes in the vane assembly and are inflated to apply a lifting force to the vanes.
While being supported in this manner, the vanes are attached to the engine case.
The method for installing stator vanes in accordance with the present invention broadly comprises installing a first rotor assembly within a case, placing a first inflatable tool over a portion of the first rotor assembly, positioning a first vane array having at least one vane on a surface of the tool; inflating the tool so that a portion of each vane in the first vane array is loaded against the case, and connecting each vane in the first vane array to the case.
In accordance with one aspect of the present invention there is provided a method for assembling an engine comprising: installing a first rotor assembly within an engine case; placing a first inflatable tool over a portion of said first rotor assembly; placing a first vane array having at least one vane on a surface of said inflatable tool; inflating said inflatable tool so that a portion of each vane in said first vane array is loaded against said engine case; and connecting each said vane in said first vane array to said engine case while said tool is in said inflated condition.
In accordance with another aspect of the present invention there is provided a tool for installing vanes in an engine comprising at least one inflatable tube for applying a lift force to a portion of a vane array to be installed in said engine, wherein said at least one inflatable tube is sized to fit between a rotor assembly and said vane array portion to be installed when said tube is in a deflated condition.
In accordance with yet another aspect of the present invention there is provided a tool for installing vanes on an engine having a casing and a layer of blades, said tool comprising: at least one inflatable tube having a first surface which overlies and contacts said layer of blades and a second surface, opposed to said first surface, for contacting surfaces of an array of vanes; and said at least one inflatable tube in an inflated condition lifting said surfaces of said array of vanes and loading a forward foot of each said vane in said array against said casing.
BACKGROUND OF THE INVENTION
The present invention relates to a tool for installing stator vanes in a turbine engine and a method of using same.
Turbine engines are typically formed by stacking rotor and stator vane assemblies one on top of another and by attaching the stator vanes to an engine case. Newer engines utilize a one-piece engine case rather than the previous split-case design. This has resulted in a blind operation during the attachment of the stator vanes to the engine case which can impact how well the stator vanes are attached to the engine case. It is important that the stator vanes be held tightly against the case during installation to prevent unwanted vibration during engine operation. Prior tools which have been used to install the stator vanes can not be used with the one-piece engine case. Thus, there is a need for an installation tool which will help insure the proper installation of stator vanes in a one-piece engine case.
SUMMARY OF THE INVENTION
Accordingly, it is an object of the present invention to provide an installation tool which can be used to properly position stator vanes for attachment to an engine case.
It is a further object of the present invention to provide an improved method for installing stator vanes in an engine case.
The foregoing objects are attained by the installation tool and the method of the present invention.
In accordance with the present invention, a pneumatic press vane lift installation tool is described. The tool is formed by two inflatable, semi-circular tubes which are placed between a rotor assembly and a stator vane assembly during the installation of the stator vane assembly. The tubes are each positioned adjacent an inner end of the stator vanes in the vane assembly and are inflated to apply a lifting force to the vanes.
While being supported in this manner, the vanes are attached to the engine case.
The method for installing stator vanes in accordance with the present invention broadly comprises installing a first rotor assembly within a case, placing a first inflatable tool over a portion of the first rotor assembly, positioning a first vane array having at least one vane on a surface of the tool; inflating the tool so that a portion of each vane in the first vane array is loaded against the case, and connecting each vane in the first vane array to the case.
In accordance with one aspect of the present invention there is provided a method for assembling an engine comprising: installing a first rotor assembly within an engine case; placing a first inflatable tool over a portion of said first rotor assembly; placing a first vane array having at least one vane on a surface of said inflatable tool; inflating said inflatable tool so that a portion of each vane in said first vane array is loaded against said engine case; and connecting each said vane in said first vane array to said engine case while said tool is in said inflated condition.
In accordance with another aspect of the present invention there is provided a tool for installing vanes in an engine comprising at least one inflatable tube for applying a lift force to a portion of a vane array to be installed in said engine, wherein said at least one inflatable tube is sized to fit between a rotor assembly and said vane array portion to be installed when said tube is in a deflated condition.
In accordance with yet another aspect of the present invention there is provided a tool for installing vanes on an engine having a casing and a layer of blades, said tool comprising: at least one inflatable tube having a first surface which overlies and contacts said layer of blades and a second surface, opposed to said first surface, for contacting surfaces of an array of vanes; and said at least one inflatable tube in an inflated condition lifting said surfaces of said array of vanes and loading a forward foot of each said vane in said array against said casing.
Other details of the installation tool and the method of the present invention, as well as other objects and advantages attendant thereto, are set forth in the following detailed description and the accompanying drawings wherein like reference numerals depict like elements.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a sectional view of a portion of a turbine engine;
FIG. 2 is a top view of an installation tool in accordance with the present invention; and FIG. 3 is a sectional view illustrating the method of assembling an engine in accordance with the present invention.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS) Referring now to the drawings, FIG. 1 illustrates a portion of a turbine engine 10. The engine 10 has a one-piece outer case 12. Mounted to the engine case 12 are a plurality of stator vanes 14. The engine 10 further has a rotor assembly 16 formed by a plurality of layers of rotors 18. The rotor layers are joined together by pin and bolt assemblies 20 which are also used to join the rotor assembly 16 to an output shaft 22.
The stator vanes 14 are cantilevered structures which are held against the case 12 by a groove and bracket mount assembly. It is important for proper assembly of the engine 10 that the stator vanes 14 be held tight against the case 12 during their installation so as to prevent unwanted vibrations during engine operation. A pneumatic press lift tool is needed to assure 2a proper installation of the stator vanes 14.
Referring now to FIG. 2, a tool 40 for assuring proper installation of the vanes 14 is illustrated. The tool 40 is formed by two inflatable tubes or bladders 42 each formed from a flexible plastic material, such as nylon, or a rubber material.
Each inflatable tube 92 is sized to fit between a rotor assembly and an adjacent vane array to be installed. Further, each inflatable tube 42 has a substantially semi-circular configuration to allow it to be properly positioned within the engine case 12 during installation. Each inflatable tube 42 has a stem 43 with an air valve 49 at its tip. The stem 93 and the air valve 94 allow a respective tube 42 to be connected to a source (not shown) of an inflating fluid. The valve 44 also allow the respective tube 42 to be easily deflated after installation of the stator vanes 14 has been completed.
Referring now to FIG. 3, an engine is fabricated by first orienting the case 12 nose down. Thereafter, a first layer 50 of rotors is installed within the case 12. An inflatable installation tool 40 comprising two inflatable tubes 42 is positioned over a surface of the rotor layer 50 while the tubes 42 are in a deflated state. The tool 40 is positioned on the rotor layer 50 so that each tube 42 will be adjacent an inner edge 52 of an array of stator vanes 14 to be installed.
Following placement of the tool 90, a first array of stator vanes 14 is positioned within the case 12. The array of stator vanes typically is an annular array of a plurality of stator vanes. After the array of stator vanes has been positioned in the case 10, a second rotor layer 54 is positioned over the first stator vane array. The tubes 42 are then each inflated to lift the inner edges of the vanes 14 in the first stator vane array and load the forward foot 46 of each vane 20 against the case 12. Each stator vane 19 is then connected to the case 12 using any suitable connection system (not shown) known in the art. Following the installation of the stator vanes 20 in the first array, the rotor layers and vane arrays are stacked as previously discussed with one or more of the tools 90 being positioned between a surface of each rotor layer and an adjacent surface of each vane in an adjacent vane array.
After all of the stator vanes 14 have been installed, the tools 90 have their respective tubes 92 deflated. Once the tubes 42 have been deflated, they can be easily removed from between each rotor layer and an adjacent vane array.
In accordance with the method of the present invention, the inflatable tubes 42 may be inflated sequentially or concurrently. One of the primary advantages to the tool 90 is its simplicity. Other tools used to assemble turbine engines use many hooks to grab the vanes being installed. The result is that the vanes are lifted into place in a cumbersome, expensive and time consuming manner. The tool of the present invention also has the advantage that it provides more freedom for vane/case designers so that hardware is assemblable. The tool also resolves the assembly of single piece case stacking. The tool can be used both in engine assembly and in engine overhaul.
It is apparent that there has been provided in accordance with the present invention a pneumatic press vane lift installation tool which fully satisfies the means, objects, and advantages set forth hereinbefore. While the present invention has been described in the context of specific embodiments thereof, other alternatives, variations, and modifications will become apparent to those skilled in the art having read the foregoing description. Therefore, it is intended to embrace those alternatives, modifications, and variations which fall within the broad scope of the appended claims.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a sectional view of a portion of a turbine engine;
FIG. 2 is a top view of an installation tool in accordance with the present invention; and FIG. 3 is a sectional view illustrating the method of assembling an engine in accordance with the present invention.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS) Referring now to the drawings, FIG. 1 illustrates a portion of a turbine engine 10. The engine 10 has a one-piece outer case 12. Mounted to the engine case 12 are a plurality of stator vanes 14. The engine 10 further has a rotor assembly 16 formed by a plurality of layers of rotors 18. The rotor layers are joined together by pin and bolt assemblies 20 which are also used to join the rotor assembly 16 to an output shaft 22.
The stator vanes 14 are cantilevered structures which are held against the case 12 by a groove and bracket mount assembly. It is important for proper assembly of the engine 10 that the stator vanes 14 be held tight against the case 12 during their installation so as to prevent unwanted vibrations during engine operation. A pneumatic press lift tool is needed to assure 2a proper installation of the stator vanes 14.
Referring now to FIG. 2, a tool 40 for assuring proper installation of the vanes 14 is illustrated. The tool 40 is formed by two inflatable tubes or bladders 42 each formed from a flexible plastic material, such as nylon, or a rubber material.
Each inflatable tube 92 is sized to fit between a rotor assembly and an adjacent vane array to be installed. Further, each inflatable tube 42 has a substantially semi-circular configuration to allow it to be properly positioned within the engine case 12 during installation. Each inflatable tube 42 has a stem 43 with an air valve 49 at its tip. The stem 93 and the air valve 94 allow a respective tube 42 to be connected to a source (not shown) of an inflating fluid. The valve 44 also allow the respective tube 42 to be easily deflated after installation of the stator vanes 14 has been completed.
Referring now to FIG. 3, an engine is fabricated by first orienting the case 12 nose down. Thereafter, a first layer 50 of rotors is installed within the case 12. An inflatable installation tool 40 comprising two inflatable tubes 42 is positioned over a surface of the rotor layer 50 while the tubes 42 are in a deflated state. The tool 40 is positioned on the rotor layer 50 so that each tube 42 will be adjacent an inner edge 52 of an array of stator vanes 14 to be installed.
Following placement of the tool 90, a first array of stator vanes 14 is positioned within the case 12. The array of stator vanes typically is an annular array of a plurality of stator vanes. After the array of stator vanes has been positioned in the case 10, a second rotor layer 54 is positioned over the first stator vane array. The tubes 42 are then each inflated to lift the inner edges of the vanes 14 in the first stator vane array and load the forward foot 46 of each vane 20 against the case 12. Each stator vane 19 is then connected to the case 12 using any suitable connection system (not shown) known in the art. Following the installation of the stator vanes 20 in the first array, the rotor layers and vane arrays are stacked as previously discussed with one or more of the tools 90 being positioned between a surface of each rotor layer and an adjacent surface of each vane in an adjacent vane array.
After all of the stator vanes 14 have been installed, the tools 90 have their respective tubes 92 deflated. Once the tubes 42 have been deflated, they can be easily removed from between each rotor layer and an adjacent vane array.
In accordance with the method of the present invention, the inflatable tubes 42 may be inflated sequentially or concurrently. One of the primary advantages to the tool 90 is its simplicity. Other tools used to assemble turbine engines use many hooks to grab the vanes being installed. The result is that the vanes are lifted into place in a cumbersome, expensive and time consuming manner. The tool of the present invention also has the advantage that it provides more freedom for vane/case designers so that hardware is assemblable. The tool also resolves the assembly of single piece case stacking. The tool can be used both in engine assembly and in engine overhaul.
It is apparent that there has been provided in accordance with the present invention a pneumatic press vane lift installation tool which fully satisfies the means, objects, and advantages set forth hereinbefore. While the present invention has been described in the context of specific embodiments thereof, other alternatives, variations, and modifications will become apparent to those skilled in the art having read the foregoing description. Therefore, it is intended to embrace those alternatives, modifications, and variations which fall within the broad scope of the appended claims.
Claims (13)
1. A tool for installing vanes in an engine comprising at least one inflatable tube far applying a lift force to a portion of a vane array to be installed in said engine, wherein said at least one inflatable tube is sized to fit between a rotor assembly and said vane array portion to be installed when said tube is in a deflated condition.
2. A tool according to claim 1, wherein said at least one tube has a substantially semi-circular configuration.
3. A tool according to claim 1 or 2, wherein said at least one tube is formed from a flexible plastic material.
4. A tool according to claim 1, 2 or 3, further comprising said at least one tube having a stem with a valve for connecting said inflatable tube to a source of inflating fluid to inflate said tool and for releasing said inflating fluid from said tube so as to deflate said tool.
5. A tool according to claim 1, 2, 3 or 4, further comprising first and second inflatable tubes for applying a lift force to said vane array to be installed and each of said inflatable tubes having a substantially semi-circular configuration.
6. A tool for installing vanes on an engine having a easing and a layer of blades, said tool comprising:
at least one inflatable tube having a first surface which overlies and contacts said layer of blades and a second surface, opposed to said first surface, for contacting surfaces of an array of vanes; and said at least one inflatable tube in an inflated condition lifting said surfaces of said array of vanes and loading a forward foot of each said vane in said array against said casing.
at least one inflatable tube having a first surface which overlies and contacts said layer of blades and a second surface, opposed to said first surface, for contacting surfaces of an array of vanes; and said at least one inflatable tube in an inflated condition lifting said surfaces of said array of vanes and loading a forward foot of each said vane in said array against said casing.
7. A tool according to claim 6, further comprising said at least one inflatable tube being positioned on said layer of blades adjacent an inner edge of said array of vanes.
8. A tool according to claim 6 or 7, wherein said at least one tube has a substantially semi-circular configuration..
9. A tool according to claim 6, 7 or 6, wherein said at least one tube is formed from a flexible plastic material.
10. A tool according to Claim 5, 7, 8 or 9, wherein said at least one tube is sized to fit between said rotor assembly and said array of vanes when said at least one tube is in a deflated condition.
11. A tool according to claim 6, 7, 8, 9 or 10, further comprising said at least one tube having a stem with a valve for connecting said at least one inflatable tube to a source of inflating fluid to inflate said tool and for releasing said inflating fluid from said at least one tube so as to deflate said tool.
12. A tool according to any one of claims 6 to 11, further comprising first and second inflatable tubes for applying a lift force to said array of vanes and each of said inflatable tubes having a substantially semi-circular configuration.a
13. A tool according to claim 12, wherein at least one end of said first inflatable tube is spaced from at least one end of said second inflatable tube.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/749,319 US6671938B2 (en) | 2000-12-27 | 2000-12-27 | Pneumatic press vane lift installation tool |
| US09/749,319 | 2000-12-27 | ||
| CA002364758A CA2364758C (en) | 2000-12-27 | 2001-12-12 | Pneumatic press vane lift installation tool |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002364758A Division CA2364758C (en) | 2000-12-27 | 2001-12-12 | Pneumatic press vane lift installation tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2559618A1 true CA2559618A1 (en) | 2002-06-27 |
Family
ID=37451513
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002559618A Abandoned CA2559618A1 (en) | 2000-12-27 | 2001-12-12 | Pneumatic press vane lift installation tool |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA2559618A1 (en) |
-
2001
- 2001-12-12 CA CA002559618A patent/CA2559618A1/en not_active Abandoned
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| FZDE | Dead |