US3764226A - Piloting device for split housings having different thermal coefficients of expansion - Google Patents
Piloting device for split housings having different thermal coefficients of expansion Download PDFInfo
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- US3764226A US3764226A US00241252A US3764226DA US3764226A US 3764226 A US3764226 A US 3764226A US 00241252 A US00241252 A US 00241252A US 3764226D A US3764226D A US 3764226DA US 3764226 A US3764226 A US 3764226A
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- housings
- tabs
- common plane
- housing
- recesses
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/26—Double casings; Measures against temperature strain in casings
- F01D25/265—Vertically split casings; Clamping arrangements therefor
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S285/00—Pipe joints or couplings
- Y10S285/913—Interdigitating
Definitions
- the present invention relates to a device for holding a pair of annular housings concentric.
- Gas turbine engines generally comprise a series of annular housings secured to one another in end-to-end relationship.
- the housings have radial struts that journal a rotor assembly within the several housings. It is apparent that if the housings are out of alignment with one another the rotor and housings can rub and cause appreciable wear.
- housings have been piloted with respect to one another by providing on one housing a series of spaced radial grooves and on the adjacent housing a series of aligned radial tabs. With this arrangement the tabs seat in the grooves. When one housing expands or contracts relative to the other the tabs move outward or inward in the grooves but still maintain the housings concentric.
- a piloting device for a pair of housings split in halves and secured together in an end-to-end relationship so that their parting lines lie in a common plane.
- a means is provided for maintaining the axes of the housings in this common plane.
- Interfitting tabs and recesses between the end-to-end housings have a first set of radially inwardly facing surfaces on the tabs that abut surfaces in the recesses and align the axes for a first temperature.
- a second set of radially outwardly facing surfaces on the tabs abut respective surfaces in the recesses to align the housings for a second temperature different from the first.
- FIG. 1 is an exploded perspective view of a pair of split housing assemblies embodying the piloting device of the present invention
- FIG. 2 is an assembled plan view in a different scale of the split housing assembly of FIG. 1;
- FIG. 3 is an exploded perspective view of a housing assembly showing another embodiment of the present invention.
- first and second generally annular housings 10 and 12 each comprised of halves 14, 16 and 18, 20, respectively.
- the housings 10 and 12 are adapted to be placed in end-to-end relationship so that housing 14 is adjacent housing half 18 and half 16 is adjacent housing half 20.
- split line of the housings lies along a common plane.
- Each of the housing halves have pilot surfaces 22 parallel to the common plane and adjacent the end-to-end junction between the housings.
- the pilot surfaces 22 of the respective halves abut at the common plane.
- the pilot surfaces 22 are illustrated as formed on radial extensions 24 to facilitate the discussion of the invention. It should be apparent, however, that in many cases the surfaces 22 would be formed substantially on the split line of the housing half.
- the housing halves each have radial flanges 32 at the end-to-end junction. These flanges have a series of aligned holes 34 which receive a bolt and nut assembly 38 to hold the housings in end-to-end relation.
- the housing halves are secured together by a suitable arrangement, such as bolt assemblies 40 extending through openings or holes 42 in the radial extensions 24.
- Housing 14 has a pair of tabs 26 on opposite sides of its axis. These tabs extend across the end-to-end junction between the housings and are received within recesses 28 of the adjacent housing half 18.
- Tabs 26 have pilot surfaces 30 that are parallel to the common plane and which abut pilot surfaces 22 of housing 20 when the housings are secured together. In the assembled form, the pilot surface 30 on the tabs 26 abut the pilot surface 22 to maintain the axes of the housings 10 and 12 both within the common plane.
- Tabs 26 have radially inwardly facing pilot surfaces 44 which abut radially outwardly facing pilot surfaces 46 and recesses 28 for a first temperature. This is accomplished by a predetermined positional relationship between the tab 26 and the recesses 28.
- the differential thermal expansion or contraction of the housings causes a relative displacement of the tabs within the recesses to abut the pilot surfaces.
- the tabs 26 each have a radially outwardly facing pilot surface 48 which abuts a radially inwardly facing pilot surface 50 in recess 28 for a second temperature different from the first temperature. When the tabs abut the pilot surfaces they align the axes of the housings 10 and 12.
- either the housing containing the tabs or the housing containing the recesses may be selected as the housing with the higher coefficient of expansion.
- the housing 10 containing the tabs 26 has the higher coefficient of thermal expansion. Therefore for the first temperature the pilot surfaces 44 and 46 abut and for the second elevated temperature the thermal growth of the housing 10 relative to 12 causes the tabs 26 to move radially outward in the recesses 28 so that pilot surfaces 48 and 50 abut.
- FIGS. 1 and 2 incorporates piloting surfaces on opposite sides of a single pair of tabs.
- the piloting device of FIG. 3 utilizes several pairs of tabs to accomplish the piloting function.
- housings and 12' each made up of halves 14', 16 and 18, 20', respectively.
- the housings have flanges 32' and openings 34 for the bolt assemblies. They also have pilot surfaces 22 parallel to the common plane in which the housings are joined, these pilot surfaces being formed on radial extensions 24'.
- housing 18 has a pair of tabs 52 which extend across the end-to-end junction between the housings and are received in recesses 54 on the adjacent housing half 14'.
- Tabs 52 have radially inwardly facing pilot surfaces 56 which abut radially outwardly facing pilot surfaces 58 in recesses 54 for the first temperature.
- Housing half 20 has a pair of tabs 60 extending across the end-to-end junction between the housings and into recesses 62 in adjacent housing half 16'.
- Tabs 60 have radially outwardly facing pilot surfaces 64 which abut radially inwardly facing pilot surfaces 66 in the recesses 62.
- pilot surfaces 56 and 54 abut for a cold temperature and pilot surfaces 64 and 66 abut for the elevated tem perature to align the axes of the housings within the common plane.
- tabs 52 and 60 each have pilot surfaces parallel to the common plane which abut the pilot surfaces 22' to maintain the axes of the housings within the common plane.
- piloting devices described above permit the radially outward removal of one of the housings for inspection of its inside. There are no grooves or projections which impair the radial removal of the housings.
- this assembly has great utility in the gas turbine art, for example, compressor housings, where one of the housings would be between a series of end-to-end housings. With this arrangement, the housing half can be removed to facilitate inspection of the interior without major disassembly of the engine.
- the first temperature described above would be selected as the temperature during which the engine is shut down and the second would be the normal operat- V ing temperature.
- the housings are piloted relative to one another by the one set of pilot surfaces when the engine is started up to insure that there will be no rubbing between the housings and the rotor journaled within the housings.
- the other set of pilot surfaces aligns the axes.
- the housings can float relative to one another.
- the clearances between the tabs and the recesses are small enough and the transient condition short enough to minimize any potential misalignment.
- tab means forming interfitting tabs extending from one of said housings axially across the interface between said annular housings and forming recesses in the other of said end-to-end housings for receiving said tabs, said tab means having a first set of radially inwardly facing surfaces having predetermined dimensional relationships relative to said recess means so that they abut and align the axes of said housings within said common plane for a first temperature, said tab means having a second set of radially outwardly facing surfaces having predetermined dimensional relationships relative to said recess means so that they abut and align the axes of said housings within said common plane for a second temperature different from said first temperature.
- a piloting device as in claim 1 wherein said means for maintaining said axes in said common plane comprises:
- pilot surfaces on said halves parallel to said common plane adjacent the end-to-end junction between said housings and positioned so that the pilot surfaces of the halves abut at said common plane;
- pilot surfaces on said tabs parallel to said common plane and positioned to abut the pilot surfaces parallel to said common plane on said housings.
- a piloting device as in claim 5 wherein a pair of tabs are formed on the casing having the higher thermal coefficient of expansion and the inwardly facing surfaces of said tab abut the side wall of said recesses for said first temperature and the outer facing surfaces of said tabs abut the opposite side wall of said recesses for said second temperature elevated from said first temperature.
- a housing assembly comprising:
- each of said housings having pilot surfaces on the first and second halves parallel to said common plane adjacent the end-to-end junction between said housings and positioned so that the pilot surfaces on the first half abut the pilot surfaces on the second half generally at said common plane;
- said tab means having said radially inwardly facing pilot surfaces comprise a pair of tabs extending from the first half of one of said housings, the first half of the adjacent housing forming said recesses into which said tabs extend;
- said tab means having said radially outwardly facing surfaces comprise a pair of tabs on the second half of the housing having the first-mentioned tabs and extending into recesses formed in the second half of the adjacent housing.
- said tab means comprise a pair of tabs on opposite sides of the axis of one of said housings extending into recesses in the adjacent housing, the radially inwardly and radially outwardly facing surfaces of said tabs forming said pilot surfaces;
- said pair of tabs form said pilot surfaces parallel to said common plane for abutting the pilot surfaces of said housing to maintain the axes of the housings within said common plane.
- a housing assembly as in claim 12 wherein said means for securing said housings together comprise:
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Abstract
A pair of annular split housings with different coefficients of thermal expansion are secured in end-to-end relationship so that their parting lines lie in a common plane. A series of tabs on one housing extends across the end-to-end junction into recesses in the adjacent housing. The dimensional relationship between the tabs and certain walls of the recesses are predetermined so that the axes of the housings are aligned within the common plane for different temperatures.
Description
United States Patent [191 Matto PILOTING DEVICE FOR SPLIT HOUSINGS HAVING DIFFERENT THERMAL COEFFICIENTS OF EXPANSION Lawrence R. Matto, Shelton, Conn.
Avco Corporation, Stratford, Conn.
Apr. 5, 1972 Inventor:
Assignee:
Filed:
Appl. No.:
[1.8. CI. 415/219 R, 285/DIG. 14 Int. Cl. F04d 29/40 Field of Search 415/219 R, 219 C,
415/199 R; 285/D1G. l4; 220/5 A [56] References Cited UNITED STATES PATENTS 3,628,884 12/1971 Mierley, Sr. 415/219 R FOREIGN PATENTS OR APPLICATIONS 903,160 8/1962 Great Britain 415/219 R Oct. 9, 1973 571,011 2/1933 Germany 415/219 R Primary Examiner-Henry F. Raduazo AttorneyCharles M. Hogan et a1.
[57] ABSTRACT 13 Claims, 3 Drawing Figures 4a so, 24 ,42
PATENTED 91973 3 764 226 SHEET 1 [1F 2 PILO'IING DEVICE FOR SPLIT I-IOUSINGS HAVING DIFFERENT THERMAL COEFFICIENTS OF EXPANSION The present invention relates to a device for holding a pair of annular housings concentric.
There are many instances in which it is desirable to secure two annular housings in end-to-end relationship and maintain their axes concentric in spite of differential thermal expansion of the housings. One of the more important situations in which this is necessary is in the gas turbine art. Gas turbine engines generally comprise a series of annular housings secured to one another in end-to-end relationship. The housings have radial struts that journal a rotor assembly within the several housings. It is apparent that if the housings are out of alignment with one another the rotor and housings can rub and cause appreciable wear. In the past, housings have been piloted with respect to one another by providing on one housing a series of spaced radial grooves and on the adjacent housing a series of aligned radial tabs. With this arrangement the tabs seat in the grooves. When one housing expands or contracts relative to the other the tabs move outward or inward in the grooves but still maintain the housings concentric.
This approach, when used for split housings, makes it necessary that the housings must be pulled apart to facilitate separation into the halves.
The copending application of Killmann and Matto, entitled Split Housing Piloting Device, Ser. No. 241,281, filed on Apr. 5, 1972, and of common assignment with the present invention, illustrates an arrangement that pilots split housings while permitting easy removal of one of the housings.
For housings having different coefficients of thermal expansion the above application provides cooperating tabs at the top and/or bottom of the housing to align the axes of the housings over a range of temperature. There are some instances in the gas turbine art where space would not permit the provisions of the tabs and the top or bottom of the housings.
Therefore it is an object of the present invention to pilot several split housing assemblies having different coefficients of thermal expansion in a greatly simplified and effective way, permitting them to be readily disassembled.
These ends are achieved by a piloting device for a pair of housings split in halves and secured together in an end-to-end relationship so that their parting lines lie in a common plane. A means is provided for maintaining the axes of the housings in this common plane. Interfitting tabs and recesses between the end-to-end housings have a first set of radially inwardly facing surfaces on the tabs that abut surfaces in the recesses and align the axes for a first temperature. A second set of radially outwardly facing surfaces on the tabs abut respective surfaces in the recesses to align the housings for a second temperature different from the first.
The above and other related objects and features of the present invention will be apparent from a reading of the description of the disclosure shown in the accompanying drawing and the novelty thereof pointed out in the appended claims.
In the drawings:
FIG. 1 is an exploded perspective view of a pair of split housing assemblies embodying the piloting device of the present invention;
FIG. 2 is an assembled plan view in a different scale of the split housing assembly of FIG. 1; and
FIG. 3 is an exploded perspective view of a housing assembly showing another embodiment of the present invention.
Referring to FIG. 1 there is shown first and second generally annular housings 10 and 12, each comprised of halves 14, 16 and 18, 20, respectively. The housings 10 and 12 are adapted to be placed in end-to-end relationship so that housing 14 is adjacent housing half 18 and half 16 is adjacent housing half 20. In addition, split line of the housings lies along a common plane.
Each of the housing halves have pilot surfaces 22 parallel to the common plane and adjacent the end-to-end junction between the housings. When the housings are assembled the pilot surfaces 22 of the respective halves abut at the common plane. As shown herein, the pilot surfaces 22 are illustrated as formed on radial extensions 24 to facilitate the discussion of the invention. It should be apparent, however, that in many cases the surfaces 22 would be formed substantially on the split line of the housing half.
The housing halves each have radial flanges 32 at the end-to-end junction. These flanges have a series of aligned holes 34 which receive a bolt and nut assembly 38 to hold the housings in end-to-end relation. The housing halves are secured together by a suitable arrangement, such as bolt assemblies 40 extending through openings or holes 42 in the radial extensions 24.
The axes are aligned within the common plane by the pilot surfaces on the tabs 26 and recesses 28, particularly shown in FIG. 2. Tabs 26 have radially inwardly facing pilot surfaces 44 which abut radially outwardly facing pilot surfaces 46 and recesses 28 for a first temperature. This is accomplished by a predetermined positional relationship between the tab 26 and the recesses 28.
The differential thermal expansion or contraction of the housings causes a relative displacement of the tabs within the recesses to abut the pilot surfaces.
The tabs 26 each have a radially outwardly facing pilot surface 48 which abuts a radially inwardly facing pilot surface 50 in recess 28 for a second temperature different from the first temperature. When the tabs abut the pilot surfaces they align the axes of the housings 10 and 12.
It should be pointed out that either the housing containing the tabs or the housing containing the recesses may be selected as the housing with the higher coefficient of expansion. As illustrated, the housing 10 containing the tabs 26 has the higher coefficient of thermal expansion. Therefore for the first temperature the pilot surfaces 44 and 46 abut and for the second elevated temperature the thermal growth of the housing 10 relative to 12 causes the tabs 26 to move radially outward in the recesses 28 so that pilot surfaces 48 and 50 abut.
During this expansion the entire circumference of the housings grow. For this reason the holes 34 in the flanges 32 have sufficient clearance relative to the bolt assemblies to permit relative radial movement of the flanges to minimize stresses.
The embodiment of FIGS. 1 and 2 incorporates piloting surfaces on opposite sides of a single pair of tabs. The piloting device of FIG. 3 utilizes several pairs of tabs to accomplish the piloting function. In this figure there is shown housings and 12', each made up of halves 14', 16 and 18, 20', respectively. The housings have flanges 32' and openings 34 for the bolt assemblies. They also have pilot surfaces 22 parallel to the common plane in which the housings are joined, these pilot surfaces being formed on radial extensions 24'.
In this embodiment housing 18 has a pair of tabs 52 which extend across the end-to-end junction between the housings and are received in recesses 54 on the adjacent housing half 14'. Tabs 52 have radially inwardly facing pilot surfaces 56 which abut radially outwardly facing pilot surfaces 58 in recesses 54 for the first temperature.
Assuming that housing 12' has the greater coefficient of thermal expansion, the dimensions are selected so that pilot surfaces 56 and 54 abut for a cold temperature and pilot surfaces 64 and 66 abut for the elevated tem perature to align the axes of the housings within the common plane.
It should be noted also that the tabs 52 and 60 each have pilot surfaces parallel to the common plane which abut the pilot surfaces 22' to maintain the axes of the housings within the common plane.
The piloting devices described above permit the radially outward removal of one of the housings for inspection of its inside. There are no grooves or projections which impair the radial removal of the housings. Thus this assembly has great utility in the gas turbine art, for example, compressor housings, where one of the housings would be between a series of end-to-end housings. With this arrangement, the housing half can be removed to facilitate inspection of the interior without major disassembly of the engine.
If the housings are incorporated in a gas turbine engine the first temperature described above would be selected as the temperature during which the engine is shut down and the second would be the normal operat- V ing temperature. Thus the housings are piloted relative to one another by the one set of pilot surfaces when the engine is started up to insure that there will be no rubbing between the housings and the rotor journaled within the housings. When the engine heats up, the other set of pilot surfaces aligns the axes.
During the transient period between the cold and hot alignment the housings can float relative to one another. However, in practice, the clearances between the tabs and the recesses are small enough and the transient condition short enough to minimize any potential misalignment.
The relationships between the tabs and recesses have been set forth as preferred embodiments of the present invention. It should be apparent, however, that the relative positioning of the tabs and recesses may be varied without departing from the spirit and scope of the present invention.
Having thus described the invention, what is claimed as novel and desired to be secured by Letters Patent of the United States is: Y
1. A piloting device for a pair of coaxial annular housings having different thermal coefficients of expansion, split in halves along a common plane and secured in end-to-end relationship, said piloting device comprising:
means for maintaining the axes of said housings in said common plane;
means forming interfitting tabs extending from one of said housings axially across the interface between said annular housings and forming recesses in the other of said end-to-end housings for receiving said tabs, said tab means having a first set of radially inwardly facing surfaces having predetermined dimensional relationships relative to said recess means so that they abut and align the axes of said housings within said common plane for a first temperature, said tab means having a second set of radially outwardly facing surfaces having predetermined dimensional relationships relative to said recess means so that they abut and align the axes of said housings within said common plane for a second temperature different from said first temperature.
2. A piloting device as in claim 1 wherein said means for maintaining said axes in said common plane comprises:
pilot surfaces on said halves parallel to said common plane adjacent the end-to-end junction between said housings and positioned so that the pilot surfaces of the halves abut at said common plane;
pilot surfaces on said tabs parallel to said common plane and positioned to abut the pilot surfaces parallel to said common plane on said housings.
3. A piloting device as in claim 1 wherein said tabs and recesses comprise:
a first pair of tabs on opposite sides of the axis of said housing extending into corresponding recesses in the adjacent housings and forming said radially inwardly facing surfaces abutting the outer facing sides of the recesses into which they project for said first temperature;
a second pair of tabs offset from said first tabs and extending into recesses in the adjacent housings and forming said radially outwardly facing surfaces abutting the inwardly facing surfaces of said recesses into which the second tabs project for said second temperature.
4. A piloting device as in claim 3 wherein said tabs extend from the housing having a higher coefficient of thermal expansion.
5. A piloting device as in claim 1 wherein said tabs and recesses comprise a pair of tabs on opposite sides of the axis of said housing into corresponding recesses in the adjacent housing, each tab having both said radially inwardly facing surface and said radially outwardly facing surfaces, said tabs abutting one side wall of said recess for said first temperature and the opposite side wall of said recess for said second temperature.
6. A piloting device as in claim 5 wherein a pair of tabs are formed on the casing having the higher thermal coefficient of expansion and the inwardly facing surfaces of said tab abut the side wall of said recesses for said first temperature and the outer facing surfaces of said tabs abut the opposite side wall of said recesses for said second temperature elevated from said first temperature.
7. A housing assembly comprising:
a pair of coaxial annular housings split in first and second halves along a common plane, said housings having different coefficients of thermal expansion;
means for securing said halves together and said housings together so that the first halves of said housings are in end-to-end alignment and the second halves are in end-to-end alignment;
each of said housings having pilot surfaces on the first and second halves parallel to said common plane adjacent the end-to-end junction between said housings and positioned so that the pilot surfaces on the first half abut the pilot surfaces on the second half generally at said common plane;
means on the first half of one of said housings extending through said end-to-end junction and having pilot surfaces abutting the pilot surfaces of the second half of the other housing thereby maintaining the axes of said housings within said common plane;
means forming a set of pilot surfaces normal to said common plane on one of said halves and facing radially outward;
means forming a set of pilot surfaces normal to said common plane on one of said halves and facing radially inward;
tab means on the half in end-to-end relationship with the half having the radially outwardly facing pilot surfaces extending across the end-to-end junction and having radially inwardly facing pilot surfaces in a predetermined position relative to said radially outwardly facing pilot surfaces abutting the radially outwardly facing pilot surfaces at a first temperature to align the axes of said housings within said common plane; and
tab means on the half in end-to-end relationship with the half having the radially inwardly facing pilot surfaces extending across the end-to-end junction and having radially outwardly facing pilot surfaces in a predetermined position relative to said radially inwardly facing pilot surfaces abutting said radially inwardly facing pilot surfaces at a second temperature different from the first temperature to align the axes of said housings within said common plane.
8. A housing assembly as in claim 6 wherein:
said tab means having said radially inwardly facing pilot surfaces comprise a pair of tabs extending from the first half of one of said housings, the first half of the adjacent housing forming said recesses into which said tabs extend;
said tab means having said radially outwardly facing surfaces comprise a pair of tabs on the second half of the housing having the first-mentioned tabs and extending into recesses formed in the second half of the adjacent housing.
9. A housing assembly as in claim 8 wherein said pairs of tabs are offset from one another and have pilot surfaces parallel to said common plane for abutting said pilot surfaces on the first and second halves.
10. A housing assembly as in claim 7 wherein:
said tab means comprise a pair of tabs on opposite sides of the axis of one of said housings extending into recesses in the adjacent housing, the radially inwardly and radially outwardly facing surfaces of said tabs forming said pilot surfaces;
the radially inwardly and outwardly facing walls of said recesses form said pilot surfaces that are abutted by said tab means.
11. A housing assembly as in claim 10 wherein said pilot surfaces on said first and second halves parallel to said common plane are adjacent said pair of tabs;
said pair of tabs form said pilot surfaces parallel to said common plane for abutting the pilot surfaces of said housing to maintain the axes of the housings within said common plane.
12. A housing assembly as in claim 11 wherein the tabs are on the housing having a higher coefficient of thermal expansion.
13. A housing assembly as in claim 12 wherein said means for securing said housings together comprise:
radially extending flanges positioned at the end-toend junction between said housing assemblies, said flanges having a series of generally aligned holes around the circumference thereof;
bolt means extending through said holes for securing said flanges together, the opening of said holes having sufficient clearance relative to said bolt means to permit relative radial expansion of said flanges.
Claims (13)
1. A piloting device for a pair of coaxial annular housings having different thermal coefficients of expansion, split in halves along a common plane and secured in end-to-end relationship, said piloting device comprising: means for maintaining the axes of said housings in said common plane; means forming interfitting tabs extending from one of said housings axially across the interface between said annular housings and forming recesses in the other of said end-to-end housings for receiving said tabs, said tab means having a first sEt of radially inwardly facing surfaces having predetermined dimensional relationships relative to said recess means so that they abut and align the axes of said housings within said common plane for a first temperature, said tab means having a second set of radially outwardly facing surfaces having predetermined dimensional relationships relative to said recess means so that they abut and align the axes of said housings within said common plane for a second temperature different from said first temperature.
2. A piloting device as in claim 1 wherein said means for maintaining said axes in said common plane comprises: pilot surfaces on said halves parallel to said common plane adjacent the end-to-end junction between said housings and positioned so that the pilot surfaces of the halves abut at said common plane; pilot surfaces on said tabs parallel to said common plane and positioned to abut the pilot surfaces parallel to said common plane on said housings.
3. A piloting device as in claim 1 wherein said tabs and recesses comprise: a first pair of tabs on opposite sides of the axis of said housing extending into corresponding recesses in the adjacent housings and forming said radially inwardly facing surfaces abutting the outer facing sides of the recesses into which they project for said first temperature; a second pair of tabs offset from said first tabs and extending into recesses in the adjacent housings and forming said radially outwardly facing surfaces abutting the inwardly facing surfaces of said recesses into which the second tabs project for said second temperature.
4. A piloting device as in claim 3 wherein said tabs extend from the housing having a higher coefficient of thermal expansion.
5. A piloting device as in claim 1 wherein said tabs and recesses comprise a pair of tabs on opposite sides of the axis of said housing into corresponding recesses in the adjacent housing, each tab having both said radially inwardly facing surface and said radially outwardly facing surfaces, said tabs abutting one side wall of said recess for said first temperature and the opposite side wall of said recess for said second temperature.
6. A piloting device as in claim 5 wherein a pair of tabs are formed on the casing having the higher thermal coefficient of expansion and the inwardly facing surfaces of said tab abut the side wall of said recesses for said first temperature and the outer facing surfaces of said tabs abut the opposite side wall of said recesses for said second temperature elevated from said first temperature.
7. A housing assembly comprising: a pair of coaxial annular housings split in first and second halves along a common plane, said housings having different coefficients of thermal expansion; means for securing said halves together and said housings together so that the first halves of said housings are in end-to-end alignment and the second halves are in end-to-end alignment; each of said housings having pilot surfaces on the first and second halves parallel to said common plane adjacent the end-to-end junction between said housings and positioned so that the pilot surfaces on the first half abut the pilot surfaces on the second half generally at said common plane; means on the first half of one of said housings extending through said end-to-end junction and having pilot surfaces abutting the pilot surfaces of the second half of the other housing thereby maintaining the axes of said housings within said common plane; means forming a set of pilot surfaces normal to said common plane on one of said halves and facing radially outward; means forming a set of pilot surfaces normal to said common plane on one of said halves and facing radially inward; tab means on the half in end-to-end relationship with the half having the radially outwardly facing pilot surfaces extending across the end-to-end junction and having radially inwardly facing pilot surfaces in a predetermined position relatiVe to said radially outwardly facing pilot surfaces abutting the radially outwardly facing pilot surfaces at a first temperature to align the axes of said housings within said common plane; and tab means on the half in end-to-end relationship with the half having the radially inwardly facing pilot surfaces extending across the end-to-end junction and having radially outwardly facing pilot surfaces in a predetermined position relative to said radially inwardly facing pilot surfaces abutting said radially inwardly facing pilot surfaces at a second temperature different from the first temperature to align the axes of said housings within said common plane.
8. A housing assembly as in claim 6 wherein: said tab means having said radially inwardly facing pilot surfaces comprise a pair of tabs extending from the first half of one of said housings, the first half of the adjacent housing forming said recesses into which said tabs extend; said tab means having said radially outwardly facing surfaces comprise a pair of tabs on the second half of the housing having the first-mentioned tabs and extending into recesses formed in the second half of the adjacent housing.
9. A housing assembly as in claim 8 wherein said pairs of tabs are offset from one another and have pilot surfaces parallel to said common plane for abutting said pilot surfaces on the first and second halves.
10. A housing assembly as in claim 7 wherein: said tab means comprise a pair of tabs on opposite sides of the axis of one of said housings extending into recesses in the adjacent housing, the radially inwardly and radially outwardly facing surfaces of said tabs forming said pilot surfaces; the radially inwardly and outwardly facing walls of said recesses form said pilot surfaces that are abutted by said tab means.
11. A housing assembly as in claim 10 wherein said pilot surfaces on said first and second halves parallel to said common plane are adjacent said pair of tabs; said pair of tabs form said pilot surfaces parallel to said common plane for abutting the pilot surfaces of said housing to maintain the axes of the housings within said common plane.
12. A housing assembly as in claim 11 wherein the tabs are on the housing having a higher coefficient of thermal expansion.
13. A housing assembly as in claim 12 wherein said means for securing said housings together comprise: radially extending flanges positioned at the end-to-end junction between said housing assemblies, said flanges having a series of generally aligned holes around the circumference thereof; bolt means extending through said holes for securing said flanges together, the opening of said holes having sufficient clearance relative to said bolt means to permit relative radial expansion of said flanges.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US24125272A | 1972-04-05 | 1972-04-05 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3764226A true US3764226A (en) | 1973-10-09 |
Family
ID=22909903
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US00241252A Expired - Lifetime US3764226A (en) | 1972-04-05 | 1972-04-05 | Piloting device for split housings having different thermal coefficients of expansion |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3764226A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4015910A (en) * | 1976-03-09 | 1977-04-05 | The United States Of America As Represented By The Secretary Of The Air Force | Bolted paired vanes for turbine |
| US4793770A (en) * | 1987-08-06 | 1988-12-27 | General Electric Company | Gas turbine engine frame assembly |
| US5104288A (en) * | 1990-12-10 | 1992-04-14 | Westinghouse Electric Corp. | Dual plane bolted joint for separately-supported segmental stationary turbine blade assemblies |
| US6267556B1 (en) * | 1998-04-21 | 2001-07-31 | Kabushiki Kaisha Toshiba | Steam turbine |
| US20030047878A1 (en) * | 2000-01-20 | 2003-03-13 | Hans-Thomas Bolms | Thermally stressable wall and method for sealing a gap in a thermally stressed wall |
| US20040107690A1 (en) * | 2002-12-06 | 2004-06-10 | Poccia Nicholas Philip | Gas turbine exhaust diffuser |
| US20120013119A1 (en) * | 2010-07-13 | 2012-01-19 | Johnson Theodore D | Split gxr collar front mounted clamp assembly |
| WO2013082482A1 (en) * | 2011-12-01 | 2013-06-06 | United Technologies Corporation | A structural joint for connecting a first component to a segmented second component |
| US20130230392A1 (en) * | 2012-03-02 | 2013-09-05 | Mitsubishi Heavy Industries, Ltd. | Auxiliary member for assembly/disassembly of gas turbine casing, gas turbine having the same, assembly method of gas turbine casing, and disassembly method of gas turbine casing |
| US20140026585A1 (en) * | 2012-07-24 | 2014-01-30 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE571011C (en) * | 1928-07-14 | 1933-02-27 | Der Maschinenfabriken Escher A | Steam and gas turbines, especially for propellants with high temperatures |
| GB903160A (en) * | 1960-02-05 | 1962-08-15 | Licentia Gmbh | A stationary-blade carrier for axial flow turbines |
| US3628884A (en) * | 1970-06-26 | 1971-12-21 | Westinghouse Electric Corp | Method and apparatus for supporting an inner casing structure |
-
1972
- 1972-04-05 US US00241252A patent/US3764226A/en not_active Expired - Lifetime
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE571011C (en) * | 1928-07-14 | 1933-02-27 | Der Maschinenfabriken Escher A | Steam and gas turbines, especially for propellants with high temperatures |
| GB903160A (en) * | 1960-02-05 | 1962-08-15 | Licentia Gmbh | A stationary-blade carrier for axial flow turbines |
| US3628884A (en) * | 1970-06-26 | 1971-12-21 | Westinghouse Electric Corp | Method and apparatus for supporting an inner casing structure |
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4015910A (en) * | 1976-03-09 | 1977-04-05 | The United States Of America As Represented By The Secretary Of The Air Force | Bolted paired vanes for turbine |
| US4793770A (en) * | 1987-08-06 | 1988-12-27 | General Electric Company | Gas turbine engine frame assembly |
| US5104288A (en) * | 1990-12-10 | 1992-04-14 | Westinghouse Electric Corp. | Dual plane bolted joint for separately-supported segmental stationary turbine blade assemblies |
| US6267556B1 (en) * | 1998-04-21 | 2001-07-31 | Kabushiki Kaisha Toshiba | Steam turbine |
| US6443695B2 (en) | 1998-04-21 | 2002-09-03 | Kabushiki Kaisha Toshiba | Steam turbine |
| US6702551B2 (en) | 1998-04-21 | 2004-03-09 | Kabushiki Kaisha Toshiba | Steam turbine |
| US20030047878A1 (en) * | 2000-01-20 | 2003-03-13 | Hans-Thomas Bolms | Thermally stressable wall and method for sealing a gap in a thermally stressed wall |
| US6807803B2 (en) * | 2002-12-06 | 2004-10-26 | General Electric Company | Gas turbine exhaust diffuser |
| US20040107690A1 (en) * | 2002-12-06 | 2004-06-10 | Poccia Nicholas Philip | Gas turbine exhaust diffuser |
| US20120013119A1 (en) * | 2010-07-13 | 2012-01-19 | Johnson Theodore D | Split gxr collar front mounted clamp assembly |
| US8328244B2 (en) * | 2010-07-13 | 2012-12-11 | Robin Boley-Johnson, legal representative | Split GXR collar front mounted clamp assembly |
| WO2013082482A1 (en) * | 2011-12-01 | 2013-06-06 | United Technologies Corporation | A structural joint for connecting a first component to a segmented second component |
| US9140139B2 (en) | 2011-12-01 | 2015-09-22 | United Technologies Corporation | Structural joint for connecting a first component to a segmented second component |
| US20130230392A1 (en) * | 2012-03-02 | 2013-09-05 | Mitsubishi Heavy Industries, Ltd. | Auxiliary member for assembly/disassembly of gas turbine casing, gas turbine having the same, assembly method of gas turbine casing, and disassembly method of gas turbine casing |
| US9539680B2 (en) * | 2012-03-02 | 2017-01-10 | Mitsubishi Hitachi Power Systems, Ltd. | Auxiliary member for assembly/disassembly of gas turbine casing, gas turbine having the same, assembly method of gas turbine casing, and disassembly method of gas turbine casing |
| US20140026585A1 (en) * | 2012-07-24 | 2014-01-30 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
| US10094288B2 (en) * | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
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