US3149378A - Apparatus for assembling impeller elements - Google Patents

Apparatus for assembling impeller elements Download PDF

Info

Publication number
US3149378A
US3149378A US61021A US6102160A US3149378A US 3149378 A US3149378 A US 3149378A US 61021 A US61021 A US 61021A US 6102160 A US6102160 A US 6102160A US 3149378 A US3149378 A US 3149378A
Authority
US
United States
Prior art keywords
impeller
bore
impeller element
shaft
fixture
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.)
Expired - Lifetime
Application number
US61021A
Inventor
Francis H Thelen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Fuller Co
Original Assignee
Fuller 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 Fuller Co filed Critical Fuller Co
Priority to US61021A priority Critical patent/US3149378A/en
Priority to GB29106/61D priority patent/GB936986A/en
Priority to GB3639/63A priority patent/GB936987A/en
Priority to CH984861A priority patent/CH375570A/en
Application granted granted Critical
Publication of US3149378A publication Critical patent/US3149378A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/84Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks by moulding material on preformed parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P19/00Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B11/00Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D1/00Couplings for rigidly connecting two coaxial shafts or other movable machine elements
    • F16D1/06Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49885Assembling or joining with coating before or during assembling

Definitions

  • the present invention relates to an apparatus for assembling impeller assemblies in which the drive shaft is adhesively bonded to the impeller element.
  • the apparatus of the invention is particularly adapted for use in assembling impeller elements onto drive shafts where the portion of the drive shaft on which the impeller is mounted is relieved, or is of slightly less diameter than the diameter of the bore of the impeller element except for lands adjacent the opposite sides of the impeller element. Such portion of less diameter provides a space between the lands for receiving a layer of the adhesive agent of appreciable thickness.
  • the apparatus for assembling the impeller element and driving shaft comprises a fixture having a base having one face to be attached to the impeller element and an extension or bushing extending from the other face.
  • the extension or bushing has a bore to receive the relieved portion of the shaft.
  • An injection fitting for injecting an adhesive agent into the relieved portion of the shaft, while it is in the bore of the bushing, passes through the wall of the fixture and has its inner end communicating with the bore of the fixture.
  • the fixture In assembling the impeller element and drive shaft, the fixture is secured to one side of the impeller element with its bore in exact axial registry with the bore of the impeller element.
  • the shaft is then placed in the fixture in such position that the lands thereon are located at opposite sides of the injection fitting.
  • the adhesive for bonding the impeller element to the shaft is then forced under high pressure through the injection fitting until the space around the shaft, between the lands, is completely filled with the adhesive under pressure.
  • the shaft is then forced axially through the fixture and into the bore of the impeller element until the space containing the adhesive is centrally positioned, axially, in the bore of the impeller element In this position the lands at the opposite ends of the layer of adhesive lie witlnn the end portions of the bore of the impeller element and prevent leakage of the adhesive axially along the shaft.
  • the adhesive is then allowed to set, or is cured, if it is of the heat-curable type, to form a strong bond between the impeller element and the drive shaft.
  • FIG. 1 is an elevational view, partly in section, of an impeller element-driving shaft assembly assembled using the apparatus of the present invention
  • FIG. 2 is a vertical sectional view of the assembly of FIG. 1 taken on line 22 of FIG. 1;
  • FIG. 3 is a sectional view showing the assembling fixture attached to an impeller element, with the drive shaft positioned therein;
  • FIG. 4 is a plan View of the assembling fixture
  • FIG. 5 is a detailed sectional view taken on line 5-5 of FIG. 3.
  • the impeller element-drive shaft assembly comprises an impeller element 1, which may be of any type, but as shown is a lobe of a conventional type of a two-lobe impeller. It generally is of a figure 8 shape in transverse section and has a central bore 2 for a conventional drive shaft 3 and axially extending bores 4 and 5 in each end.
  • the portions of these bores remote from the bore for the drive shaft are undercut to provide inner shoulders 4 and 5 (FIG. 3).
  • the opposite sides of the impeller element have projections 6 and 6 extending radially outwardly for a slight distance.
  • the lobe cooperates in meshing engagement with a like lobe in the impeller housing in a well known manner, the projections 6 and 6' making a close fit with the impeller housing and the surface of the cooperating lobe.
  • the drive shaft is provided with lands 7 and 7' which are spaced apart a distance slightly less than the length of the impeller element at the hub thereof so that, when assembled, the lands will extend into the bore of the impeller element a slight distance at each end, as shown in FIG. 1.
  • the lands 7 and 7' extend outwardly from the main diameter of the drive shaft a distance of from about 0.001 to 0.003 inch, and preferably about 0.002 inch. This provides a space or relieved portion on the shaft of that width between the drive shaft and the im peller element for an annular layer of an adhesive bonding agent 8 of that thickness.
  • the diameter of the lands is slightly greater, up to about 0.002 inch greater, than the diameter of the bore 2 of the impeller element so that it has a pressed fit with the impeller element.
  • Example I Parts by wt. Furane Epocast No. 17A Furane Hardener No. 909 8 This is a viscous liquid mixture having slow setting characteristics at room temperature. It was cured for 12 hours at a temperature between 375 and 400 F.
  • Example 11 Parts by volume Devcon A 9 Hardener 1 This composition has the consistency of heavy putty. It was cured at room temperature, approximately 70 F.
  • Example 111 Parts by wt. Epocast No.295 100 Hardener No. 909 5 This is a thixotropic mixture. It was cured for 19 hours at a temperature between 375 and 400 F.
  • the fixture F for assembling the impeller element onto the drive shaft comprises a base member 10 adapted to be clamped against one side of the impeller element during the assembling operation.
  • the base member has extending therefrom at the side thereof opposite the side which is to be clamoed 3 to the impeller element, an extension or bushing 11.
  • the bore of the bushing is lined with a material 12 having good wearing qualities and preferably having a low surface-friction coefiicient.
  • the diameter of bore 13 is 0.002 to 0.004 inch larger than the diameter of the lands 7 and 7' of the shaft 3.
  • the end of the bore 13 is flared outwardly at 12' to facilitate insertion of the driving shaft during an assembling operation, as hereinafter described.
  • the opposite ends of the base members 10 have unthreaded openings 14 and 14' through which extend clamping bolts 15 and 15 having laterally extending toe pieces 16 and 16' extending therefrom at one end.
  • Pins 17 and 17 extend through the other or outer ends of the clamping bolts and form handles enabling the bolts to be located in proper position to engage behind the shoulders 4' and when the assembling fixture is to be clamped to an impeller element.
  • the outer ends of the bolts are threaded and clamping nuts 18 and 18 are threaded onto them. These nuts preferably have laterally extending protuberances so that they may readily be turned by ones hand to thread them along the bolts.
  • the surface of the base 10, which is adapted to be clamped against the impeller element during an assembling operation, has crescent-shaped recesses 19 and 19 circumjacent the openings 14 and 14'. These recesses provide spaces for locating pins 20 and 20 which protrude radially from the bolts 15 and 15'.
  • the bushing 11 and its liner 12 have a radially extending opening 21 into the outer end of which is fitted an injection fitting 22, preferably of the check-valve type.
  • a guide or locating member 23 is secured to the face of the base member which is secured to the end of the impeller by machine screws 24.
  • This locating member has a projecting stud 25 to be received in an opening in the face of the base member to assure that the locating member is properly located to be received in one of the bores 4 or 5 of the impeller element.
  • the sides 26 and 26 of the member 23 are curved lengthwise and transversely.
  • the width of the locating member transversely of the base member is substantially equal to the diameter of the'bores 4 and 5, being just sufficiently less to enable easy insertion of the member into one of the bores.
  • the radius of curvature lengthwise of the sides 26 and 26' is slightly less than the radius of curvature of the bores 4 and 5 so that there is only substantially linear contact between those edges of the locating member and bore 4 or 5.
  • the bolts 15 and 15 are rotated to a position where their respective clamping toe pieces 16 and 16' extend to positions permitting the bolts to pass into the bores 4 and 5 of the impeller.
  • the fixture then is placed against one end face of the impeller element, with the bore 13 thereof in exact axial registry with the bore 2 of the impeller element.
  • the bolts are then turned in the opposite direction until the locating pins 20 and 20' engage the outer ends of the respective crescent-shapedrecesses 19 and 19'. This positions the toe pieces 16 and 16' of the bolts bebind the shoulders 4' and 5' of the bores 4 and 5.
  • the clamping nuts 18 and 18' are then turned to cause the bolts to move in a direction away from the impeller element and to cause the toe pieces to clamp tightly against the shoulders 4' and 5'. This effectively clamps the fixture tightly against the end face of the impeller.
  • the drive shaft 3 With the fixture clamped tightly against the end face of the impeller, and with the bore 13 of the fixture in exact axial registry with the bore 2 of the impeller element, the drive shaft 3 is inserted into the outer end of the bore 13 until the space between the lands 7 and 7' of the shaft is wholly within the bore 13, with the lands located at opposite sides of the injection fitting, as shown in FIG. 3.
  • the adhesive composition is forced through the injection fitting 21 under high pressure into the space defined by the driving shaft, the liner 12 and the lands 7 and 7, until the adhesive composition begins to leak out between the bushing liner and lands on the shaft. At this time all air will have been forced from the space and the space completely filled with the adhesive composition under high pressure.
  • the shaft is then forced axially through the bushing and into the bore 2 of the impeller element until it reaches the position shown in dotted lines in FIG. 3, and in full lines in FIG. 1.
  • a suitable tool may be used for this purpose.
  • the diameter of the lands 7 and 7 is slightly greater than the diameter of the bore 2 of the impeller element, a concentric, interference fit will be obtained between the lands and the impeller element.
  • the adhesive composition forms an annular layer, under pressure, between the drive shaft and the impeller element and is prevented from escaping by the interference engagement of the lands 7 and 7' with the impeller element. This assures that there will be intimate bonding throughout substantially the entire area of the opposing faces of the impeller element and the shaft throughout the distance between the lands.
  • the adhesive composition is now permitted to set, or if it is of the heat-curable type, is subjected to the proper degree of heat for an adequate length of time to thoroughly cure it. If the adhesive composition is of the heatcurable type, and also is one which expands when heated, the expansion will cause an even more intimate and stronger bond between the impeller element and the drive shaft.
  • a fixture for assembling an impeller element onto a shaft which comprises a base member having a face to be secured tightly to one end of an impeller element, an extension or bushing having a bore extending therethrough in a direction normal to said face of the base member extending from the opposite face of the base member through which a shaft to be attached to the impeller may be passed, means at opposite sides of said extension or bushing for securing the fixture to an impeller element, said extension or bushing having an opening extending through its wall and terminating at the bore thereof, and an injection fitting attached to the extension or bore and having the opening thereof communicating with the opening through the wall of the extension or bushing through which an adhesive to secure the impeller to the shaft may be passed.
  • a fixture as defined in claim 1, in which the means for securing the fixture to an impeller element comprises clamping bolts extending through openings in the base member, each of said bolts having a laterally extending portion adapted to engage behind a portion of an impeller element to be assembled onto the shaft, and means for moving the bolts longitudinally through the holes in the base member in a direction to move said laterally extending portions towards said base member.
  • said locating means comprises an arcuate-shaped recess in the base member circumjacent each of the openings through which the clamping shoulders pass and a projection extending laterally from said bolts and adapted to be located in the respective recesses, the ends of the respective recesses acting as stops for the projections when the projections are located in said recesses and the bolts are turned in opposite directions.
  • a fixture as defined in claim 1 including a locating member protruding from the face of the base member which is to be secured to an impeller element, said locating member being adapted to be received in an opening in the impeller element.

Description

FIG.4.
INVENTOR FRANCIS H. THELEN F. H. THELEN APPARATUS FOR ASSEMBLING IMPELLER ELEMENTS Filed Oct. 6, 1960 Pie. 5.
@5401. BY f//%/ Sept. 22, 1964 ATTORNEYS United States Patent Ofiice 7 Patented Sept. 22, 1964 3,149,378 APEARATUS F83 ASSENBLENG WELLER ELEMENTS Francis H. Thelen, Tuiunga, (laiii, assignor to Fuller Company, Catasauqua, Pa, a corporation of Delaware Filed Oct. 6, 1960, Ser. No. 61,021 6 Claims. (CI. 18-36) The present invention relates to an apparatus for assembling impeller assemblies in which the drive shaft is adhesively bonded to the impeller element. Heretofore it has been common practice to secure the impeller element to the driving shaft by a so-called interference fit in which a shaft of slightly greater diameter than the bore of the impeller element is forced into the bore of the impeller element, and the impeller element then keyed to the shaft. However with the use of larger shafts, such as those used in a high-pressure, high-speed impeller, such means of securing the imr-eller element is not satisfactory since the increase in the shaft diameter necessarily requires an increase in the bore diameter through the impeller. This reduces the wall thickness of the impeller at the shaft bore and weakens the impeller at that point so that the stress resulting from the usual interference type of assembly will either break the impeller or stretch the metal beyond its elastic limit.
The apparatus of the invention is particularly adapted for use in assembling impeller elements onto drive shafts where the portion of the drive shaft on which the impeller is mounted is relieved, or is of slightly less diameter than the diameter of the bore of the impeller element except for lands adjacent the opposite sides of the impeller element. Such portion of less diameter provides a space between the lands for receiving a layer of the adhesive agent of appreciable thickness.
The apparatus for assembling the impeller element and driving shaft comprises a fixture having a base having one face to be attached to the impeller element and an extension or bushing extending from the other face. The extension or bushing has a bore to receive the relieved portion of the shaft. An injection fitting for injecting an adhesive agent into the relieved portion of the shaft, while it is in the bore of the bushing, passes through the wall of the fixture and has its inner end communicating with the bore of the fixture.
In assembling the impeller element and drive shaft, the fixture is secured to one side of the impeller element with its bore in exact axial registry with the bore of the impeller element. The shaft is then placed in the fixture in such position that the lands thereon are located at opposite sides of the injection fitting. The adhesive for bonding the impeller element to the shaft is then forced under high pressure through the injection fitting until the space around the shaft, between the lands, is completely filled with the adhesive under pressure. The shaft is then forced axially through the fixture and into the bore of the impeller element until the space containing the adhesive is centrally positioned, axially, in the bore of the impeller element In this position the lands at the opposite ends of the layer of adhesive lie witlnn the end portions of the bore of the impeller element and prevent leakage of the adhesive axially along the shaft. The adhesive is then allowed to set, or is cured, if it is of the heat-curable type, to form a strong bond between the impeller element and the drive shaft.
The invention will be further described in connection with the accompanying drawings in which:
FIG. 1 is an elevational view, partly in section, of an impeller element-driving shaft assembly assembled using the apparatus of the present invention;
FIG. 2 is a vertical sectional view of the assembly of FIG. 1 taken on line 22 of FIG. 1;
FIG. 3 is a sectional view showing the assembling fixture attached to an impeller element, with the drive shaft positioned therein;
FIG. 4 is a plan View of the assembling fixture; and
FIG. 5 is a detailed sectional view taken on line 5-5 of FIG. 3.
Referring to the drawings, and first to FIGS. 1 and 2, the impeller element-drive shaft assembly comprises an impeller element 1, which may be of any type, but as shown is a lobe of a conventional type of a two-lobe impeller. It generally is of a figure 8 shape in transverse section and has a central bore 2 for a conventional drive shaft 3 and axially extending bores 4 and 5 in each end. In order to facilitate the assembly of the impeller element onto the drive shaft, as herein described, the portions of these bores remote from the bore for the drive shaft are undercut to provide inner shoulders 4 and 5 (FIG. 3).
The opposite sides of the impeller element have projections 6 and 6 extending radially outwardly for a slight distance. In operation the lobe cooperates in meshing engagement with a like lobe in the impeller housing in a well known manner, the projections 6 and 6' making a close fit with the impeller housing and the surface of the cooperating lobe.
The drive shaft is provided with lands 7 and 7' which are spaced apart a distance slightly less than the length of the impeller element at the hub thereof so that, when assembled, the lands will extend into the bore of the impeller element a slight distance at each end, as shown in FIG. 1. The lands 7 and 7' extend outwardly from the main diameter of the drive shaft a distance of from about 0.001 to 0.003 inch, and preferably about 0.002 inch. This provides a space or relieved portion on the shaft of that width between the drive shaft and the im peller element for an annular layer of an adhesive bonding agent 8 of that thickness. The diameter of the lands is slightly greater, up to about 0.002 inch greater, than the diameter of the bore 2 of the impeller element so that it has a pressed fit with the impeller element.
While any suitable adhesive may be used to obtain an adhesive bond between the impeller element and the drive shaft, it has been found that heat-curable resinous epoxy compositions give an excellent bond. Examples of such compositions which have been used are as follows:
Example I Parts by wt. Furane Epocast No. 17A Furane Hardener No. 909 8 This is a viscous liquid mixture having slow setting characteristics at room temperature. It was cured for 12 hours at a temperature between 375 and 400 F.
Example 11 Parts by volume Devcon A 9 Hardener 1 This composition has the consistency of heavy putty. It was cured at room temperature, approximately 70 F.
Example 111 Parts by wt. Epocast No.295 100 Hardener No. 909 5 This is a thixotropic mixture. It was cured for 19 hours at a temperature between 375 and 400 F.
Referring now to FIGS' 3 to 5, the fixture F for assembling the impeller element onto the drive shaft comprises a base member 10 adapted to be clamped against one side of the impeller element during the assembling operation. The base member has extending therefrom at the side thereof opposite the side which is to be clamoed 3 to the impeller element, an extension or bushing 11. The bore of the bushing is lined with a material 12 having good wearing qualities and preferably having a low surface-friction coefiicient. The diameter of bore 13 is 0.002 to 0.004 inch larger than the diameter of the lands 7 and 7' of the shaft 3. The end of the bore 13 is flared outwardly at 12' to facilitate insertion of the driving shaft during an assembling operation, as hereinafter described.
The opposite ends of the base members 10 have unthreaded openings 14 and 14' through which extend clamping bolts 15 and 15 having laterally extending toe pieces 16 and 16' extending therefrom at one end. Pins 17 and 17 extend through the other or outer ends of the clamping bolts and form handles enabling the bolts to be located in proper position to engage behind the shoulders 4' and when the assembling fixture is to be clamped to an impeller element.
The outer ends of the bolts are threaded and clamping nuts 18 and 18 are threaded onto them. These nuts preferably have laterally extending protuberances so that they may readily be turned by ones hand to thread them along the bolts.
The surface of the base 10, which is adapted to be clamped against the impeller element during an assembling operation, has crescent- shaped recesses 19 and 19 circumjacent the openings 14 and 14'. These recesses provide spaces for locating pins 20 and 20 which protrude radially from the bolts 15 and 15'. When the bolts are rotated in one direction until the locating pins engage one end of the crescent-shaped recesses, as shown in FIG. 3, the toe pieces of the bolts are brought behind the shoulders 4' and 5' of the bores 4 and 5 of the impeller element. When the bolts are rotated in the opposite direction, the toe pieces of the bolts are removed from behind the shoulders so that the fixture may be removed from the impeller element.
The bushing 11 and its liner 12 have a radially extending opening 21 into the outer end of which is fitted an injection fitting 22, preferably of the check-valve type.
To assist in locating the fixture in proper position on one end of the impeller element, a guide or locating member 23 is secured to the face of the base member which is secured to the end of the impeller by machine screws 24. This locating member has a projecting stud 25 to be received in an opening in the face of the base member to assure that the locating member is properly located to be received in one of the bores 4 or 5 of the impeller element. The sides 26 and 26 of the member 23 are curved lengthwise and transversely. The width of the locating member transversely of the base member is substantially equal to the diameter of the'bores 4 and 5, being just sufficiently less to enable easy insertion of the member into one of the bores. The radius of curvature lengthwise of the sides 26 and 26' is slightly less than the radius of curvature of the bores 4 and 5 so that there is only substantially linear contact between those edges of the locating member and bore 4 or 5.
In assembling an impeller element onto a driving shaft, the bolts 15 and 15 are rotated to a position where their respective clamping toe pieces 16 and 16' extend to positions permitting the bolts to pass into the bores 4 and 5 of the impeller. The fixture then is placed against one end face of the impeller element, with the bore 13 thereof in exact axial registry with the bore 2 of the impeller element. The bolts are then turned in the opposite direction until the locating pins 20 and 20' engage the outer ends of the respective crescent-shapedrecesses 19 and 19'. This positions the toe pieces 16 and 16' of the bolts bebind the shoulders 4' and 5' of the bores 4 and 5. The clamping nuts 18 and 18' are then turned to cause the bolts to move in a direction away from the impeller element and to cause the toe pieces to clamp tightly against the shoulders 4' and 5'. This effectively clamps the fixture tightly against the end face of the impeller. With the fixture clamped tightly against the end face of the impeller, and with the bore 13 of the fixture in exact axial registry with the bore 2 of the impeller element, the drive shaft 3 is inserted into the outer end of the bore 13 until the space between the lands 7 and 7' of the shaft is wholly within the bore 13, with the lands located at opposite sides of the injection fitting, as shown in FIG. 3. With the drive shaft in this position, the adhesive composition is forced through the injection fitting 21 under high pressure into the space defined by the driving shaft, the liner 12 and the lands 7 and 7, until the adhesive composition begins to leak out between the bushing liner and lands on the shaft. At this time all air will have been forced from the space and the space completely filled with the adhesive composition under high pressure. The shaft is then forced axially through the bushing and into the bore 2 of the impeller element until it reaches the position shown in dotted lines in FIG. 3, and in full lines in FIG. 1. A suitable tool may be used for this purpose.
As the shaft 3 and its coating of adhesive are forced into the impeller, both frictional resistance and the shearing action of the edge of the impeller through which the shaft passes, will peel-01f a certain amount of the adhesive. However, since the bore 13 of the fixture is about 0.003 inch greater in diameter than the bore of the impeller, a slight excess of adhesive is available to prevent this peeling from robbing the required adhesive from the 0.002 inch relieved portion of the shaft.
Since the diameter of the lands 7 and 7 is slightly greater than the diameter of the bore 2 of the impeller element, a concentric, interference fit will be obtained between the lands and the impeller element. The adhesive composition forms an annular layer, under pressure, between the drive shaft and the impeller element and is prevented from escaping by the interference engagement of the lands 7 and 7' with the impeller element. This assures that there will be intimate bonding throughout substantially the entire area of the opposing faces of the impeller element and the shaft throughout the distance between the lands.
The adhesive composition is now permitted to set, or if it is of the heat-curable type, is subjected to the proper degree of heat for an adequate length of time to thoroughly cure it. If the adhesive composition is of the heatcurable type, and also is one which expands when heated, the expansion will cause an even more intimate and stronger bond between the impeller element and the drive shaft.
It is to be understood that various changes may be made in the specific form of the fixture described herein without departing from the invention or sacrificing any of the advantages thereof.
I claim:
1. A fixture for assembling an impeller element onto a shaft which comprises a base member having a face to be secured tightly to one end of an impeller element, an extension or bushing having a bore extending therethrough in a direction normal to said face of the base member extending from the opposite face of the base member through which a shaft to be attached to the impeller may be passed, means at opposite sides of said extension or bushing for securing the fixture to an impeller element, said extension or bushing having an opening extending through its wall and terminating at the bore thereof, and an injection fitting attached to the extension or bore and having the opening thereof communicating with the opening through the wall of the extension or bushing through which an adhesive to secure the impeller to the shaft may be passed.
2. A fixture as defined in claim 1, in which the means for securing the fixture to an impeller element comprises clamping bolts extending through openings in the base member, each of said bolts having a laterally extending portion adapted to engage behind a portion of an impeller element to be assembled onto the shaft, and means for moving the bolts longitudinally through the holes in the base member in a direction to move said laterally extending portions towards said base member.
3. A fixture as defined in claim 2, in which the laterally extending portions of the bolts are toe pieces extending from the clamping bolts at one side thereof, and which includes means for locating said toe pieces in a predetermined position to engage behind a portion of the impeller element.
4. A fixture as defined in claim 3, in which said locating means comprises an arcuate-shaped recess in the base member circumjacent each of the openings through which the clamping shoulders pass and a projection extending laterally from said bolts and adapted to be located in the respective recesses, the ends of the respective recesses acting as stops for the projections when the projections are located in said recesses and the bolts are turned in opposite directions.
5. A fixture as defined in claim 4, in which the clamping bolts are mounted for rectilinear movement through the openings in the base member and for turning movement only to the extent of the free movement of the projections in said arcuate-shaped recesses, the end portions of the bolts extending from the face of the base member opposite the face which engages the impeller element being threaded, and clamping nuts mounted on said threaded portions of the respective bolts.
6. A fixture as defined in claim 1 including a locating member protruding from the face of the base member which is to be secured to an impeller element, said locating member being adapted to be received in an opening in the impeller element.
References Cited in the file of this patent UNITED STATES PATENTS 421,089 Wood Feb. 11, 1890 1,283,947 Steinle Nov. 5, 1918 1,368,449 Myers Feb. 15, 1921 2,082,379 Brittain June 1, 1937 2,226,777 Martin Dec. 31, 1940 2,336,159 Bent Dec. 7, 1943 2,423,869 Blessing July 15, 1947 2,512,230 Greaves et a1. June 20, 1950 2,618,579 Brajer Nov. 18, 1952 2,688,159 Swartz et al. Sept. 7, 1954 2,724,864 Krotz Nov. 29, 1955 2,923,579 Scheel Feb. 2, 1960 3,061,887 Clarke Nov. 6, 1962

Claims (1)

1. A FIXTURE FOR ASSEMBLING AN IMPELLER ELEMENT ONTO A SHAFT WHICH COMPRISES A BASE MEMBER HAVING A FACE TO BE SECURED TIGHTLY TO ONE END OF AN IMPELLER ELEMENT, AN EXTENSION OR BUSHING HAVING A BORE EXTENDING THERETHROUGH IN A DIRECTION NORMAL TO SAID FACE OF THE BASE MEMBER EXTENDING FROM THE OPPOSITE FACE OF THE BASE MEMBER THROUGH WHICH A SHAFT TO BE ATTACHED TO THE IMPELLER MAY BE PASSED, MEANS AT OPPOSITE SIDES OF SAID EXTENSION OR BUSHING FOR SECURING THE FIXTURE TO AN IMPELLER ELEMENT, SAID EXTENSION OR BUSHING HAVING AN OPENING EXTENDING THROUGH ITS WALL AND TERMINATING AT THE BORE THEREOF, AND AN INJECTION FITTING ATTACHED TO THE EXTENSION OR BORE AND HAVING THE OPENING THEREOF COMMUNICATING WITH THE OPENING THROUGH THE WALL OF THE EXTENSION OR BUSHING THROUGH WHICH AN ADHESIVE TO SECURE THE IMPELLER TO THE SHAFT MAY BE PASSED.
US61021A 1960-10-06 1960-10-06 Apparatus for assembling impeller elements Expired - Lifetime US3149378A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US61021A US3149378A (en) 1960-10-06 1960-10-06 Apparatus for assembling impeller elements
GB29106/61D GB936986A (en) 1960-10-06 1961-08-11 Method for assembling impeller elements onto shafts
GB3639/63A GB936987A (en) 1960-10-06 1961-08-11 Apparatus for assembling impeller assemblies
CH984861A CH375570A (en) 1960-10-06 1961-08-23 Drive assembly, method of manufacturing the assembly and device for implementing this method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US61021A US3149378A (en) 1960-10-06 1960-10-06 Apparatus for assembling impeller elements

Publications (1)

Publication Number Publication Date
US3149378A true US3149378A (en) 1964-09-22

Family

ID=22033140

Family Applications (1)

Application Number Title Priority Date Filing Date
US61021A Expired - Lifetime US3149378A (en) 1960-10-06 1960-10-06 Apparatus for assembling impeller elements

Country Status (3)

Country Link
US (1) US3149378A (en)
CH (1) CH375570A (en)
GB (2) GB936987A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1022056A (en) * 1963-12-04 1966-03-09 Ici Ltd Riveting
CN106002822B (en) * 2016-06-20 2018-03-09 中国航空动力机械研究所 It is interference fitted the extracting tool of part

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US421089A (en) * 1890-02-11 Journal-bearing
US1283947A (en) * 1915-04-24 1918-11-05 Rubber Regenerating Co Treatment of materials.
US1368449A (en) * 1917-08-09 1921-02-15 F E Myers And Brother Power-driven pump
US2082379A (en) * 1934-04-11 1937-06-01 Gen Motors Corp Press fitting
US2226777A (en) * 1937-10-26 1940-12-31 Olympia Buromaschinenfabrik A Means for fastening machine elements on a shaft
US2336159A (en) * 1938-11-30 1943-12-07 Hercules Powder Co Ltd Method of preparing filaments
US2423869A (en) * 1940-09-30 1947-07-15 Rca Corp Composite structure and method of making the same
US2512230A (en) * 1947-02-07 1950-06-20 C D Patents Ltd Joining of carbon bodies to other bodies
US2618579A (en) * 1952-11-18 Method of cementing ceramic
US2688159A (en) * 1951-04-10 1954-09-07 Cons Molded Products Corp Molding apparatus
US2724864A (en) * 1949-04-29 1955-11-29 Goodrich Co B F Apparatus and method for making composite articles
US2923579A (en) * 1954-07-06 1960-02-02 Rockwell Standard Co Shaft support
US3061887A (en) * 1959-07-13 1962-11-06 Autoquip Corp Method of making ram bearing

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2618579A (en) * 1952-11-18 Method of cementing ceramic
US421089A (en) * 1890-02-11 Journal-bearing
US1283947A (en) * 1915-04-24 1918-11-05 Rubber Regenerating Co Treatment of materials.
US1368449A (en) * 1917-08-09 1921-02-15 F E Myers And Brother Power-driven pump
US2082379A (en) * 1934-04-11 1937-06-01 Gen Motors Corp Press fitting
US2226777A (en) * 1937-10-26 1940-12-31 Olympia Buromaschinenfabrik A Means for fastening machine elements on a shaft
US2336159A (en) * 1938-11-30 1943-12-07 Hercules Powder Co Ltd Method of preparing filaments
US2423869A (en) * 1940-09-30 1947-07-15 Rca Corp Composite structure and method of making the same
US2512230A (en) * 1947-02-07 1950-06-20 C D Patents Ltd Joining of carbon bodies to other bodies
US2724864A (en) * 1949-04-29 1955-11-29 Goodrich Co B F Apparatus and method for making composite articles
US2688159A (en) * 1951-04-10 1954-09-07 Cons Molded Products Corp Molding apparatus
US2923579A (en) * 1954-07-06 1960-02-02 Rockwell Standard Co Shaft support
US3061887A (en) * 1959-07-13 1962-11-06 Autoquip Corp Method of making ram bearing

Also Published As

Publication number Publication date
GB936986A (en) 1963-09-18
GB936987A (en) 1963-09-18
CH375570A (en) 1964-02-29

Similar Documents

Publication Publication Date Title
EP1850453B1 (en) Permanent magnet rotor
US3217922A (en) High pressure-low pressure seal assembly
FR2483548B1 (en)
US2372485A (en) Self-staking bushing and the like
EP1896727A1 (en) Assembly and method for mounting a pump bearing in/on plastic coolant pump housings
US3493249A (en) Eccentric bushings for housings
GB1057339A (en) Rotatable shafting
US3149378A (en) Apparatus for assembling impeller elements
DE69819126T2 (en) Elastomer seal
US2459370A (en) Packing assembly
CA1308043C (en) Leak sealing
KR920007063B1 (en) Bicycle frame
US3076159A (en) Waveguide coupling apparatus
US2584133A (en) Insert fastener
EP0086291A1 (en) Engine oil passage seal
EP0476234A1 (en) Spigot for the rotor of a coolant pump
US2157838A (en) Elastic fluid turbine shaft and disk structure and the like
JPS60112877A (en) Manufacture of mechanical part by bonding
GB1196161A (en) Electrically Insulated Pipe Coupling
WO2000005522A1 (en) Method for producing a sealing between two engine parts, especially between an engine block and a cylinder head
DE102011113876B4 (en) Assembly with a shaft-hub connection and method for adhesively bonding a hub to a shaft
US3489934A (en) Dynamo-electric machine end shield arrangement
US2381270A (en) Bearing assembly
JPS5836210B2 (en) How to glue a tubular shaft to an end fitting
DE102016006271A1 (en) Axial error compensation by means of balancing mass