US2360383A - Method of assembling fluid couplings - Google Patents

Method of assembling fluid couplings Download PDF

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US2360383A
US2360383A US389285A US38928541A US2360383A US 2360383 A US2360383 A US 2360383A US 389285 A US389285 A US 389285A US 38928541 A US38928541 A US 38928541A US 2360383 A US2360383 A US 2360383A
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shell
vane
vanes
slots
tab
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US389285A
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Reinhold C Zeidler
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Borg Warner Corp
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Borg Warner Corp
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    • 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
    • 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
    • Y10T29/49316Impeller making
    • Y10T29/4933Fluid coupling device

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  • This invention relates to hydraulic couplings of the vaned type and to a method of fabricating such couplings.
  • the principal object of this invention is to provide a fluid coupling element which possesses the necessary strength to withstand the forces to which it will be subjected, and which nevertheless will be very inexpensive to fabricate.
  • Another object of this invention is to provide a method of fabricating hydraulic coupling elements, which method will require a minimum of special equipment.
  • Fig. 1 is a fragmentary section of a fluid coupling element showing a vane about to be inserted into a shell;
  • Fig. 2 shows the vane in place and about to be locked mechanically to the shell
  • Fig. 3 shows the vane locked. in place in the shell, and a drive-transmitting hub secured to the shell;
  • Fig. 4 is a fragmentary front elevation of an assembled vane element
  • Fig. 5 is a fragmentary elevation in sectio showing a modification of the vane which may be used with the method shown in Figs. 1 to 3;
  • Fig. 6 shows the vane of Fig. 5 in place
  • Fig. 7 is a fragmentary section taken through line 'I! of Fig. 6 showing how the vane of Fig. 5 is locked in place.
  • the method comprises forming a shell in the shape of a semitoroid, forming a vane which departs from the shape of the torus over at least a portion of its periphery, forming a tab or extension in the nonconforming portion of the vane, and finally deforming the shell over the non-conforming region to make it conform to the outline of the vane, the act of deforming the shell resulting in a mechanical lock between the shell and tab which prevents the vane from being withdrawn.
  • III is a shell which may be in the form of a semi-toroid as shown in Fig. 1. It is preferably made from sheet metal, but it may also be made from any other sheet material, or it may also be made from cast material.
  • the cross-section may be a semi-circle, or it may be of any desired contour.
  • the shell is apertured at II and I2 as shown, the apertures being substantially in the same radial plane and being spaced from one another approximately as shown in Fig. 1.
  • aperture I2 is located near the inner edge of shell I0 and aperture II is located approximately 30 away from the vertical axis, the point of reference being roughly the center of curvature of the shell III.
  • a plurality of vanes I3 are stamped from sheet metal or other material into the form shown in Fig/1.
  • Edge I4 of vane I3 conforms to the shape of shell II).
  • a hook-shaped tab I5 is provided at the upper e d of edge I4, and a substantially rectangular tab 6 is formed at the lower end of edge I4, said tab IB being substantially parallel to and extending from a straight edge I1, which is at right angles to a second straight edge I8 extending across the open side of the vanes.
  • Vane I3 is relieved at I9, and hook-shaped tab I5 is relieved. at 20 as shown for the purpose hereinafter to be described.
  • each vane is tilted substantially as shown to insert tab I5 into aperture II. Therelief at I9 and 20 allows the hook to be erted into its slot while tab I6 is slid into the shell.
  • the vane is then rotated clockwise (Fig. 1) so that tab I5 hooks over the upper edge of aperture II and at the same time tab I6 will be moved to the left until edge I4 strikes shell III.
  • the shell and vane then appear as shown in Fig. 2.
  • edge I1 is at this stage spaced from shell III, thereby providing considerable relief. It will also be apparent that the corner 2
  • the deformation may be brought about by placing the assembled vanes and shell against a plate 22 and then by means of a suitable reciprocable punch 23 forcing a hub member 24 toward the plate, the hub member having an outside diameter which is just large enough to force the shell against edge II.
  • the hub member may have axial grooves 25 broached in the outer surface thereof which receive tabs I6 as the hub member is forced toward plate 22.
  • hub 24 and edge I! of vanes l3 have substantially parallel surfaces, that is, substantially concentric cylindrical surfaces, it is not necessary that this be the case.
  • the surfaces may be somewhatbnical if desired and may slope in either direction.
  • the important feature resides in providing a certain amount of relief between the shell and vane in the vicinity of the tabs and then subsequently destroying the relief in order ;to lock the tabs to the shell.
  • the tabs need not be located at the radially innermost region of the shell, but may be located off to one side, the shell being originally deformed and then pressed into semi-circular shape in order to destroy the relief between the vane and shell.
  • tab I5 is shown in Figs. 5, 6 and 7.
  • the tab comprises sim ply a rectangle 21 which, after the vane is in place, is bent over as shown in Figs. 6 and '7.
  • the assembled vanes, shell and hub member comprise an element of a completed coupling, it being understood that the element can be used either as a driving member or as a driven member and that the completed coupling would comprise two such elements in opposed relation to form a completed torus. It is understood further that the foregoing description is merely illustrative of the invention and that the scope of the invention, therefore, is not to be limited thereto but is to be determined by the appended claims.
  • a method of assembling a vaned element of a fluid coupling the steps which comprise forming a semi-toroidal shell, providing pairs of radially spaced slots arranged circumferentially in the shell and spaced from the edges of the shell, forming vanes each having a pair of spaced tabs, said vanes each being such that it may fit inside the shell with its tabs extending through a pair of said slots and provide a relief between the shell and vane between the inner side edge of the shell and the adjacent tab, positioning the vanes to fit inside the shell with the tabs extending through the slots, and then forcing a hub member into the central region of the shell to thereby deform the shell and destroy the relief between each of the vanes and the shell and lock the tabs in the slots and the vanes in the shell.
  • a method of assembling a vaned element of a fluid coupling comprising forming a semi toroidal shell providing pairs of radially spaced slots arranged circumferentially in the shell and spaced from the edges of the shell, forming vanes each having a first tab in the form of a hook and also a second tab spaced from the first tab, said vanes each being such that it may-fit inside the shell with the first tab extending through and engaging the edge of one of a pair of slots which is adjacent the outer edge of the shell and the second tab extending through the other of the pair of slots adjacent the inner edge of the shell and the vane being such to provide a relief between the shell and vane between the second tab and the inner side edge of the shell, positioning each of the vanes to fit inside the shell by first inserting the first tab into its slot, and thereafter inserting the second tab into its slot and engaging the first tab with the edge of its slot, and then forcing a hub member into the central region of the shell to deformthe shell and thereby destroy the relief between
  • a fluid coupling element comprising a shell which is substantially semi-toroidal in shape and is open at one side, said shell having a substantially cylindrical region adjacent its inner edge and being provided with pairs of slots circumferentially arranged about the shell, one of the slots of each of said pairs being in said cylindrical region and the other of the slots being radially spaced therefrom and adjacent the other edge of the shell and each of the slots being spaced from the adjacent edge of the shell by a portion of the shell, and a plurality of vanes each having a pair of spaced tabs with one of the tabs being in the form of a hook, said vanes each fitting in said shell with its hook-like tab extending through and engaging the edge of one of a pair of slots which is adjacent the outer edge of the shell and the other of the tabs extending through the other one of the pair of slots whereby the vanes are held in the shell by the portions thereof between the slots and the edges of the shell.
  • a method of assemblin a vaned element of a power transmitting fiuid coupling comprising: forming a semi-toroidal shell open at one side; providing a plurality of series of slots in said shell with each series including a pair of generally radial slots spaced from each other and with one slot of each pair adjacent to an edge of said shell; forming a plurality of vanes each having a pair of spaced tabs and with the respective vanes substantially semi-circular in shape so that each vane will fit in said shell with the tabs thereof extending through the slots of one of said pairs of slots, whereby the end of the slots nearest the edges of said shell can contact with the adjacent side edge of its associated tab to lock the vane in place, and with a portion of the inner surface of said shell between one of said slots and the adjacent edge of said shell in contact with a peripheral edge portion of said vane, and with the inner surface of said shell and another peripheral edge portion of said vane spaced to provide a relief in a zone between the other slot
  • a method of assembling a vaned element of a power transmitting fluid coupling comprising: forming a semi-toroidal shell open at one side; providing a plurality of series of slots in said shell with each series including a pair of generally radial slots spaced from each other and with one slot of each pair adjacent to an edge of said shell; forming a plurality of vanes each having a pair of spaced tabs and with the respective vanes substantially semi-circular in shape so that each vane will fit in said shell with the tabs thereof extendin through the slots of one of said pairs of slots, whereby the end of the slots near est the edges of said shell can contact with the adjacent side edge of its associated tab to lock the vane in place, and with a portion of the inner surface of said shell between one of said slots and the adjacent edge or said shell in contact with a peripheral edge portion of said vane, and with the inner surface of said shell and another peripheral edge portion of said vane spaced to provide a relief in a zone between the other slot and the edge of
  • a method of assembling a vaned element of a power transmitting fluid coupling comprising: forming a semi-toroidal shell open at one side; providing a plurality of series of slots in said shell with each series including a pair of generally radial slots spaced from each other and with one slot of each pair adjacent to an edge of said shell; forming a plurality of vanes each having a pair of spaced tabs one of which tabs is in the form of a hook and with the respective vanes substantially semi-circular in shape so that each vane will fit in said shell with the tabs thereof extending through the slots of one of said pairs of slots, whereby the end of the slots nearest the edges of said shell can contact with the adjacent side edge of its associated tab to lock the vane in place, and with a portion of the inner surface of said shell between one of said slots and the hook-tab and the adjacent side edge of said shell in contact with a peripheral edge portion of said vane, and with the inner surface of said shell and another peripheral edge portion of said vane space
  • a method of assembling a vaned element of a power transmitting fluid coupling comprising: forming a semi-toroidal shell open at one side; providing a plurality of series of slots in said shell with each series including a pair of generally radial slots spaced from each other and with one slot of each pair adjacent to an edge of said shell; forming a plurality of vanes each having a pair of spaced tabs, one of which tabs is in the form of a hook, and with the respective vanes substantially semi-circular in shape so that each vane will fit in said shell with the tabs thereof extending through one of said pairs of slots, whereby the end of the slots nearest the edges of said shell can contact with the adjacent side edge of its associated tab to lock the vane in place, and with a portion of the inner surface of I said shell between one of said slots and the hooktab and the adjacent side edge of said shell in contact with a peripheral edge portion of said vane, and'with the ixmer surface of said shell and another peripheral edge portion

Description

Oct. 17, 1944. R. c. ZEIDLER METHOD OF ASSEMBLING FLUID COUPLING Filed April 19, 1941 fizz/erzz or'" fein/afa azeiczzer Patented Oct. 17, 1944 METHOD OF ASSEMBLING FLUID COUPLINGS Reinhold C. Zeidler, Detroit, Micln, assignor to Borg-Warner Corporation, Chicago, 111., a corporation of Illinois Application April 19, 1941, Serial No. 389,285
7 Claims.
This invention relates to hydraulic couplings of the vaned type and to a method of fabricating such couplings.
The principal object of this invention is to provide a fluid coupling element which possesses the necessary strength to withstand the forces to which it will be subjected, and which nevertheless will be very inexpensive to fabricate.
Another object of this invention is to provide a method of fabricating hydraulic coupling elements, which method will require a minimum of special equipment.
These and other objects and features of the invention will become apparent from the following description when taken together with the accompanying drawing, in which:
Fig. 1 is a fragmentary section of a fluid coupling element showing a vane about to be inserted into a shell;
Fig. 2 shows the vane in place and about to be locked mechanically to the shell;
Fig. 3 shows the vane locked. in place in the shell, and a drive-transmitting hub secured to the shell;
Fig. 4 is a fragmentary front elevation of an assembled vane element;
Fig. 5 is a fragmentary elevation in sectio showing a modification of the vane which may be used with the method shown in Figs. 1 to 3;
Fig. 6 shows the vane of Fig. 5 in place; and
Fig. 7 is a fragmentary section taken through line 'I! of Fig. 6 showing how the vane of Fig. 5 is locked in place.
In its preferred embodiment, the method comprises forming a shell in the shape of a semitoroid, forming a vane which departs from the shape of the torus over at least a portion of its periphery, forming a tab or extension in the nonconforming portion of the vane, and finally deforming the shell over the non-conforming region to make it conform to the outline of the vane, the act of deforming the shell resulting in a mechanical lock between the shell and tab which prevents the vane from being withdrawn.
Referring now tothe drawing, III is a shell which may be in the form of a semi-toroid as shown in Fig. 1. It is preferably made from sheet metal, but it may also be made from any other sheet material, or it may also be made from cast material. The cross-section may be a semi-circle, or it may be of any desired contour. The shell is apertured at II and I2 as shown, the apertures being substantially in the same radial plane and being spaced from one another approximately as shown in Fig. 1. Thus, aperture I2 is located near the inner edge of shell I0 and aperture II is located approximately 30 away from the vertical axis, the point of reference being roughly the center of curvature of the shell III.
A plurality of vanes I3 are stamped from sheet metal or other material into the form shown in Fig/1. Edge I4 of vane I3 conforms to the shape of shell II). A hook-shaped tab I5 is provided at the upper e d of edge I4, and a substantially rectangular tab 6 is formed at the lower end of edge I4, said tab IB being substantially parallel to and extending from a straight edge I1, which is at right angles to a second straight edge I8 extending across the open side of the vanes. Vane I3 is relieved at I9, and hook-shaped tab I5 is relieved. at 20 as shown for the purpose hereinafter to be described.
To assemble vanes I3 into shell I0, each vane is tilted substantially as shown to insert tab I5 into aperture II. Therelief at I9 and 20 allows the hook to be erted into its slot while tab I6 is slid into the shell. The vane is then rotated clockwise (Fig. 1) so that tab I5 hooks over the upper edge of aperture II and at the same time tab I6 will be moved to the left until edge I4 strikes shell III. The shell and vane then appear as shown in Fig. 2.
Referring now to Fig. 2, it will be seen that edge I1 is at this stage spaced from shell III, thereby providing considerable relief. It will also be apparent that the corner 2| of tab I6 just clears the inner edge of aperture I2. This means that the vane is not yet locked in place in the shell and could be worked loose despite the fact that tab I5 is hooked over shell III. In order to lock the vane in place, therefore, shell III is deformed so as to bring it into contact with edge II. Since a drive-transmitting hub must be secured to the element or semi-toroidal shell in any event, the deformation may be brought about by placing the assembled vanes and shell against a plate 22 and then by means of a suitable reciprocable punch 23 forcing a hub member 24 toward the plate, the hub member having an outside diameter which is just large enough to force the shell against edge II. If desired the hub member may have axial grooves 25 broached in the outer surface thereof which receive tabs I6 as the hub member is forced toward plate 22.
The deformed shell is shown in Fig. 3. It will a be observed that since tab I5 is hooked over shell I0, and the shell has been deformed, tab I6 is permanently locked in place and the vane thereshell and hub, the two may be welded together as shown at 26. It will be observed that a portion of the drive will be transmitted through tabs l6 as well as through the weld 28 and the latter, therefore, will be relieved of some of the torque.
It is understood that although hub 24 and edge I! of vanes l3 have substantially parallel surfaces, that is, substantially concentric cylindrical surfaces, it is not necessary that this be the case. The surfaces may be somewhatbnical if desired and may slope in either direction. The important feature resides in providing a certain amount of relief between the shell and vane in the vicinity of the tabs and then subsequently destroying the relief in order ;to lock the tabs to the shell. It is also to be understood that the tabs need not be located at the radially innermost region of the shell, but may be located off to one side, the shell being originally deformed and then pressed into semi-circular shape in order to destroy the relief between the vane and shell.
An alternative form of tab I5 is shown in Figs. 5, 6 and 7. In this form the tab comprises sim ply a rectangle 21 which, after the vane is in place, is bent over as shown in Figs. 6 and '7.
The assembled vanes, shell and hub member comprise an element of a completed coupling, it being understood that the element can be used either as a driving member or as a driven member and that the completed coupling would comprise two such elements in opposed relation to form a completed torus. It is understood further that the foregoing description is merely illustrative of the invention and that the scope of the invention, therefore, is not to be limited thereto but is to be determined by the appended claims.
I claim:
1. In a method of assembling a vaned element of a fluid coupling, the steps which comprise forming a semi-toroidal shell, providing pairs of radially spaced slots arranged circumferentially in the shell and spaced from the edges of the shell, forming vanes each having a pair of spaced tabs, said vanes each being such that it may fit inside the shell with its tabs extending through a pair of said slots and provide a relief between the shell and vane between the inner side edge of the shell and the adjacent tab, positioning the vanes to fit inside the shell with the tabs extending through the slots, and then forcing a hub member into the central region of the shell to thereby deform the shell and destroy the relief between each of the vanes and the shell and lock the tabs in the slots and the vanes in the shell.
2. In a method of assembling a vaned element of a fluid coupling, the steps which comprise forming a semi toroidal shell providing pairs of radially spaced slots arranged circumferentially in the shell and spaced from the edges of the shell, forming vanes each having a first tab in the form of a hook and also a second tab spaced from the first tab, said vanes each being such that it may-fit inside the shell with the first tab extending through and engaging the edge of one of a pair of slots which is adjacent the outer edge of the shell and the second tab extending through the other of the pair of slots adjacent the inner edge of the shell and the vane being such to provide a relief between the shell and vane between the second tab and the inner side edge of the shell, positioning each of the vanes to fit inside the shell by first inserting the first tab into its slot, and thereafter inserting the second tab into its slot and engaging the first tab with the edge of its slot, and then forcing a hub member into the central region of the shell to deformthe shell and thereby destroy the relief between each of the vanes and the shell and lock the tabs in the slots and the vanes in the shell.
3. A fluid coupling element comprising a shell which is substantially semi-toroidal in shape and is open at one side, said shell having a substantially cylindrical region adjacent its inner edge and being provided with pairs of slots circumferentially arranged about the shell, one of the slots of each of said pairs being in said cylindrical region and the other of the slots being radially spaced therefrom and adjacent the other edge of the shell and each of the slots being spaced from the adjacent edge of the shell by a portion of the shell, and a plurality of vanes each having a pair of spaced tabs with one of the tabs being in the form of a hook, said vanes each fitting in said shell with its hook-like tab extending through and engaging the edge of one of a pair of slots which is adjacent the outer edge of the shell and the other of the tabs extending through the other one of the pair of slots whereby the vanes are held in the shell by the portions thereof between the slots and the edges of the shell.
4. In a method of assemblin a vaned element of a power transmitting fiuid coupling, the steps comprising: forming a semi-toroidal shell open at one side; providing a plurality of series of slots in said shell with each series including a pair of generally radial slots spaced from each other and with one slot of each pair adjacent to an edge of said shell; forming a plurality of vanes each having a pair of spaced tabs and with the respective vanes substantially semi-circular in shape so that each vane will fit in said shell with the tabs thereof extending through the slots of one of said pairs of slots, whereby the end of the slots nearest the edges of said shell can contact with the adjacent side edge of its associated tab to lock the vane in place, and with a portion of the inner surface of said shell between one of said slots and the adjacent edge of said shell in contact with a peripheral edge portion of said vane, and with the inner surface of said shell and another peripheral edge portion of said vane spaced to provide a relief in a zone between the other slot and the edge of said shell adjacent thereto; positioning said vanes to so fit in said shell; and bending said shell toward said vanes in the zone of said reliefs to substantially simultaneously bring said shell into engagement with all of said vanes, whereby to eliminate said reliefs so that said tabs and the portions of said shell between the respective slots and the adjacent edges of said shell then cooperate to hold said vanes from movement out of said shell.
5 In a method of assembling a vaned element of a power transmitting fluid coupling, the steps comprising: forming a semi-toroidal shell open at one side; providing a plurality of series of slots in said shell with each series including a pair of generally radial slots spaced from each other and with one slot of each pair adjacent to an edge of said shell; forming a plurality of vanes each having a pair of spaced tabs and with the respective vanes substantially semi-circular in shape so that each vane will fit in said shell with the tabs thereof extendin through the slots of one of said pairs of slots, whereby the end of the slots near est the edges of said shell can contact with the adjacent side edge of its associated tab to lock the vane in place, and with a portion of the inner surface of said shell between one of said slots and the adjacent edge or said shell in contact with a peripheral edge portion of said vane, and with the inner surface of said shell and another peripheral edge portion of said vane spaced to provide a relief in a zone between the other slot and the edge of said shell adjacent thereto; positioning said vanes to so fit in said shell; and bending said shell toward said vanes in the zone of said reliefs to bring said shell into engagement with said vanes, whereby to eliminate said reliefs so that said tabs and the portions of said shell between the respective slots and the adjacent edges of said shell then cooperate to hold said vanes from movement out of said shell;
6. In a method of assembling a vaned element of a power transmitting fluid coupling, the steps comprising: forming a semi-toroidal shell open at one side; providing a plurality of series of slots in said shell with each series including a pair of generally radial slots spaced from each other and with one slot of each pair adjacent to an edge of said shell; forming a plurality of vanes each having a pair of spaced tabs one of which tabs is in the form of a hook and with the respective vanes substantially semi-circular in shape so that each vane will fit in said shell with the tabs thereof extending through the slots of one of said pairs of slots, whereby the end of the slots nearest the edges of said shell can contact with the adjacent side edge of its associated tab to lock the vane in place, and with a portion of the inner surface of said shell between one of said slots and the hook-tab and the adjacent side edge of said shell in contact with a peripheral edge portion of said vane, and with the inner surface of said shell and another peripheral edge portion of said vane spaced to provide a relief in a zone between the other slot and its associated tab and the edge of said shell adjacent thereto; positioning each of said vanes to so flt in said shell by inserting the hook-tab through one slot of a pair of slots and then rotating the vane to bring the other tab into alignment with the other slot of said pair; and bending said shell toward said vanes in the zone of said reliefs to substantially simultaneously bring said shell into engagement with all of said vanes, whereby to eliminate said reliefs so that said tabs and the portions of said shell between the respective slots and the adjacent edges of said shell then cooperate to hold said vanes from movement out of said shell.
'7. In a method of assembling a vaned element of a power transmitting fluid coupling, the steps comprising: forming a semi-toroidal shell open at one side; providing a plurality of series of slots in said shell with each series including a pair of generally radial slots spaced from each other and with one slot of each pair adjacent to an edge of said shell; forming a plurality of vanes each having a pair of spaced tabs, one of which tabs is in the form of a hook, and with the respective vanes substantially semi-circular in shape so that each vane will fit in said shell with the tabs thereof extending through one of said pairs of slots, whereby the end of the slots nearest the edges of said shell can contact with the adjacent side edge of its associated tab to lock the vane in place, and with a portion of the inner surface of I said shell between one of said slots and the hooktab and the adjacent side edge of said shell in contact with a peripheral edge portion of said vane, and'with the ixmer surface of said shell and another peripheral edge portion of said vane spaced to provide a relief in a zone between the other slot and its associated tab and the edge of said shell adjacent thereto; positioning each of said vanes to so fit in said shell by inserting the hook-tab through one slot of a pair of slots and then rotating the vane to bring the other tab into alignment with the other slot of said pair; and bending said shell toward said vanes in the zone of said reliefs to bring said shell into engagement with said vanes, whereby to eliminate said reliefs so that said tabs and the portions of said shell between the respective slots and the adjacent edges of said shell then cooperate to hold said vanes from movement out of said shell.
REINHOLD C. ZEIDLER.
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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2599461A (en) * 1948-01-23 1952-06-03 Chrysler Corp Fluid coupling element
US2651830A (en) * 1947-07-17 1953-09-15 Lau Blower Co Apparatus for forming blower wheels
US2692561A (en) * 1948-12-31 1954-10-26 Borg Warner Hydrodynamic coupling
US2692562A (en) * 1948-12-31 1954-10-26 Borg Warner Hydrodynamic coupling
US2712285A (en) * 1952-07-03 1955-07-05 Ford Motor Co Hydraulic torque transmitting device and method of manufacture
US2745354A (en) * 1950-04-22 1956-05-15 Borg Warner Hydrodynamic coupling
US2917001A (en) * 1951-06-16 1959-12-15 Borg Warner Hydrodynamic coupling
US2948226A (en) * 1955-05-27 1960-08-09 Borg Warner Hydrodynamic coupling
US4412718A (en) * 1978-02-17 1983-11-01 Cdm Connectors Development & Mfg. Ag Electric plug contact and method for its manufacture
US5868025A (en) * 1996-07-03 1999-02-09 Exedy Corporation Method for manufacturing a turbine shell
US6023843A (en) * 1997-02-13 2000-02-15 Exedy Corporation Method of forming an annular member of a torque converter

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2651830A (en) * 1947-07-17 1953-09-15 Lau Blower Co Apparatus for forming blower wheels
US2599461A (en) * 1948-01-23 1952-06-03 Chrysler Corp Fluid coupling element
US2692561A (en) * 1948-12-31 1954-10-26 Borg Warner Hydrodynamic coupling
US2692562A (en) * 1948-12-31 1954-10-26 Borg Warner Hydrodynamic coupling
US2745354A (en) * 1950-04-22 1956-05-15 Borg Warner Hydrodynamic coupling
US2917001A (en) * 1951-06-16 1959-12-15 Borg Warner Hydrodynamic coupling
US2712285A (en) * 1952-07-03 1955-07-05 Ford Motor Co Hydraulic torque transmitting device and method of manufacture
US2948226A (en) * 1955-05-27 1960-08-09 Borg Warner Hydrodynamic coupling
US4412718A (en) * 1978-02-17 1983-11-01 Cdm Connectors Development & Mfg. Ag Electric plug contact and method for its manufacture
US5868025A (en) * 1996-07-03 1999-02-09 Exedy Corporation Method for manufacturing a turbine shell
US5946962A (en) * 1996-07-03 1999-09-07 Exedy Corporation Method for manufacturing a turbine shell
US6023843A (en) * 1997-02-13 2000-02-15 Exedy Corporation Method of forming an annular member of a torque converter

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