US2722625A - Tab fastening device - Google Patents

Tab fastening device Download PDF

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Publication number
US2722625A
US2722625A US228320A US22832051A US2722625A US 2722625 A US2722625 A US 2722625A US 228320 A US228320 A US 228320A US 22832051 A US22832051 A US 22832051A US 2722625 A US2722625 A US 2722625A
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US
United States
Prior art keywords
tab
sheet
wings
anode
spacer
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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
US228320A
Inventor
Wilbur H Bingeman
Francis T Quigley
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.)
GTE Sylvania Inc
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Sylvania Electric Products Inc
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.)
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Publication date
Application filed by Sylvania Electric Products Inc filed Critical Sylvania Electric Products Inc
Priority to US228320A priority Critical patent/US2722625A/en
Application granted granted Critical
Publication of US2722625A publication Critical patent/US2722625A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J19/00—Details of vacuum tubes of the types covered by group H01J21/00
    • H01J19/42—Mounting, supporting, spacing, or insulating of electrodes or of electrode assemblies
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
    • F16B2200/20—Connections with hook-like parts gripping behind a blind side of an element to be connected
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J2893/00—Discharge tubes and lamps
    • H01J2893/0001—Electrodes and electrode systems suitable for discharge tubes or lamps
    • H01J2893/0002—Construction arrangements of electrode systems
    • H01J2893/0005—Fixing of electrodes
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49908—Joining by deforming
    • Y10T29/49915—Overedge assembling of seated part
    • Y10T29/49922—Overedge assembling of seated part by bending over projecting prongs

Definitions

  • This invention relates to articles made of sheet metal, and more particularly to a new and improved construction for joining portions of such material. More specically, the invention relates to an improved tab fastening device for use in quickly joining the end of one sheet of material to a second sheet of material.
  • An object of the invention is to provide a joint structure having a positive clamping action, yet one which may be made quickly and easily with simple tools.
  • Another object of the invention is to provide a quickly assembled joint structure which will retain the joined parts in position indefinitely.
  • a further object of the invention is the reduction of strain and tearing of the tab or the slot forming the joint.
  • Still another object is the utilization of the natural resilience of the sheet materials forming the joint to aid the clamping action.
  • Fig. 1 is a perspective view, partly in section of a partially assembled tab joint of the invention.
  • Fig. 2 is a modified view similar to Figure l, illustrating completion of the locking process.
  • FIGs. 3 and 4 illustrate modifications in construction of the invention shown in Fig. 1.
  • Fig. 5 is a view of a vacuum tube showing an electrode structure utilizing the present invention.
  • twist tab 1 projects from a first sheet of material 2 through aperture 3 in a second sheet of material 4.
  • a narrow neck 6 formed between punchouts 7 joins tab 1 to sheet 2.
  • Wings 8 are formed at each lower corner of tab 1 by the upward slant of cut-outs 7. For ease of manufacture and to reduce concentrated local strains the sides 7' of slots 7 are rounded.
  • tab 1 is shown after it has been twisted to lock sheet 4 in place between wings 8 and upper surfaces 9 of sheet 2.
  • the twisting of tab 1 has caused a bending up of wings 8 and a deformation of the material forming neck 6 in the area immediately between the inner ends of slots 7.
  • the deformation of neck 6 has caused a foreshortening which tends to draw tab 1 in towards sheet 2.
  • the bending of wings 8 has resulted in the development of a certain amount of tension in the wings, in that they tend to press down on sheet 4.
  • the effect of the forej 2,722,625 vPatented Nov. l, 1955 ICC shortening of neck 6 and the bending of wings 8 is to produce concurrently acting forces which are transmitted to sheet 4 through wings 8 and serve to bind the material of sheet 4 between wings 8 and upper surfaces 9 of sheet 2.
  • slots 7 it is preferable for the upper end of slots 7 to extend a short distance above the top surface of sheet ⁇ 4 so that wings 8 will yield readily when a twisting force is applied to tab 1 for locking. However, increasing the length of slot 7 excessively beyond the plane of the outer surface of sheet 4 would produce a reduction in eiciency and strength of the locking device. It should also be understood that it is preferable to employ a slot having widened ends in order to facilitate passage of the ends of wings 8 as tab 1 is twisted.
  • aperture 3 is panduriform in outline, that is obovate, with a concavity in each side. If aperture 3 is made rectangular, some deformation of the material of sheet 4 around sheet 2 may occur.
  • Figures 3 and 4 illustrate modifications which may be made in the tab structure illustrated in Figures l and 2. Where the old structure has not been modified the same reference figures are used. In Figure 3 the curved side 7 of Figure l has been eliminated, leaving a narrow slot and permitting the use of a simpler cutting tool.
  • tab 1 and sheet 2 many materials can be used in sheet 4, in tab 1 and sheet 2.
  • tab 1 of sheet 2 may be of metal, plastic, or any ductile resilient material.
  • sheet 4 may be of metal or of an insulating material, provided that the surface of it is relatively hard. It is not essential that tab 1 be integral with sheet 2 as it should be clear to the skilled mechanic that there are many situations where a separate tab would be more convenient.
  • wing 8 has been shown as triangular, and this is the preferred form, it will be apparent to those skilled in the art that other forms may be found useful as well.
  • square or rectangular wings may be used, preferably with a suitable modification of slot 3 to facilitate operation of the twist lock.
  • a mica separator used for supporting the electrodes is held in place on the electrode structure by twist tabs of the sort described above.
  • Mica 12 having serrations 13 on at least part of its periphery for making contact with envelope 14, has apertures for receiving cathode 15 and grid side rods 16.
  • Slots 17 are provided for passing twist tabs 18 extending from anode 19. The tabs are twisted to lock mica 12 and anode 19 together.
  • a joint between sheet materials comprising a first member having an elongated aperture therethrough, a second member bearing against a first surface of the first member and having a tab extending through said aperture, said tab lying in a surface displaced with respect to the surface of the second member, and said tab having wings extending away from the surface of the tab and bearing against a surface of said rst member opposite to said rst surface, whereby said members are locked together.
  • a vacuum tube having a mount structure therein, said mount structure including an anode and an insulating spacer at an end of said anode, said spacer having an elongated aperture therein, said anode having Va tab extending through the aperture with an edge of the anode bearing against a surface of the spacer and with the tab extending perpendicular to the spacer but at an angle to the adjacent anode wall, and wings extending laterally from the tab bearing on the surface of the spacer opposite to said rst surface, whereby said anode and spacer are locked together.

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  • Clamps And Clips (AREA)

Description

Nov. 1, 1955 W. H. BINGEMAN ET AL 2,722,625
TAB FASTENING DEVICE Filed May 25, 1951 l INVENTORS WILB R H. BNGEMAN BFYRAbgCIS T. QUIGLEY l# /ZM ATTRN/vf United States Patent() TAB FASTENIN G DEVICE Wilbur H. Bingeman and Francis T. Quigley, Emporium,
Pa., assignors to Sylvania Electric Products Inc., a corporation of Massachusetts Application May 25, 1951, Serial No. 228,320
3 Claims. (Cl. 313-260) This invention relates to articles made of sheet metal, and more particularly to a new and improved construction for joining portions of such material. More specically, the invention relates to an improved tab fastening device for use in quickly joining the end of one sheet of material to a second sheet of material.
An object of the invention is to provide a joint structure having a positive clamping action, yet one which may be made quickly and easily with simple tools.
Another object of the invention is to provide a quickly assembled joint structure which will retain the joined parts in position indefinitely.
A further object of the invention is the reduction of strain and tearing of the tab or the slot forming the joint.
Still another object is the utilization of the natural resilience of the sheet materials forming the joint to aid the clamping action.
In accordance with this invention, these objects and others which may appear from the following detailed description are attained in a new and improved tab fastening device, in which a metal twist tab attached to one object being fastened is inserted through an aperture in a second object being fastened, and the protruding end of the tab is then twisted, forcing the surfaces of the deformed metal against the outer edges of the slot, thereby binding the two objects together, special cuts in the tab providing downward extending flaps which fold as the tab is twisted and provide the principal surface contact area in the joint.
For better understanding of my invention, reference is made in the following detailed description to the appended drawings, in which:
Fig. 1 is a perspective view, partly in section of a partially assembled tab joint of the invention.
Fig. 2 is a modified view similar to Figure l, illustrating completion of the locking process.
Figs. 3 and 4 illustrate modifications in construction of the invention shown in Fig. 1.
Fig. 5 is a view of a vacuum tube showing an electrode structure utilizing the present invention.
In Fig. l, twist tab 1 projects from a first sheet of material 2 through aperture 3 in a second sheet of material 4. A narrow neck 6 formed between punchouts 7 joins tab 1 to sheet 2. Wings 8 are formed at each lower corner of tab 1 by the upward slant of cut-outs 7. For ease of manufacture and to reduce concentrated local strains the sides 7' of slots 7 are rounded.
In Fig. 2, tab 1 is shown after it has been twisted to lock sheet 4 in place between wings 8 and upper surfaces 9 of sheet 2. The twisting of tab 1 has caused a bending up of wings 8 and a deformation of the material forming neck 6 in the area immediately between the inner ends of slots 7. The deformation of neck 6 has caused a foreshortening which tends to draw tab 1 in towards sheet 2. The bending of wings 8 has resulted in the development of a certain amount of tension in the wings, in that they tend to press down on sheet 4. The effect of the forej 2,722,625 vPatented Nov. l, 1955 ICC shortening of neck 6 and the bending of wings 8 is to produce concurrently acting forces which are transmitted to sheet 4 through wings 8 and serve to bind the material of sheet 4 between wings 8 and upper surfaces 9 of sheet 2.
It should be noted that it is preferable for the upper end of slots 7 to extend a short distance above the top surface of sheet` 4 so that wings 8 will yield readily when a twisting force is applied to tab 1 for locking. However, increasing the length of slot 7 excessively beyond the plane of the outer surface of sheet 4 would produce a reduction in eiciency and strength of the locking device. It should also be understood that it is preferable to employ a slot having widened ends in order to facilitate passage of the ends of wings 8 as tab 1 is twisted. In the drawing, aperture 3 is panduriform in outline, that is obovate, with a concavity in each side. If aperture 3 is made rectangular, some deformation of the material of sheet 4 around sheet 2 may occur.
Figures 3 and 4 illustrate modifications which may be made in the tab structure illustrated in Figures l and 2. Where the old structure has not been modified the same reference figures are used. In Figure 3 the curved side 7 of Figure l has been eliminated, leaving a narrow slot and permitting the use of a simpler cutting tool.
In Figure 4, a further modification is shown in which recesses or cut out areas 12 are provided at the base of neck 6 in order to remove areas of strain due to twisting of the neck from the region of the slot 3 in the cornpleted joint.
It should be noted that many materials can be used in sheet 4, in tab 1 and sheet 2. For example, tab 1 of sheet 2 may be of metal, plastic, or any ductile resilient material. Similarly, sheet 4 may be of metal or of an insulating material, provided that the surface of it is relatively hard. It is not essential that tab 1 be integral with sheet 2 as it should be clear to the skilled mechanic that there are many situations where a separate tab would be more convenient.
While in the drawings and the description above the shape of wing 8 has been shown as triangular, and this is the preferred form, it will be apparent to those skilled in the art that other forms may be found useful as well. For example, square or rectangular wings may be used, preferably with a suitable modification of slot 3 to facilitate operation of the twist lock.
In Fig. 5, a View is shown of a typical use of this twist lock in the structure of a vacuum tube. In this illustrative embodiment, a mica separator used for supporting the electrodes is held in place on the electrode structure by twist tabs of the sort described above. Mica 12 having serrations 13 on at least part of its periphery for making contact with envelope 14, has apertures for receiving cathode 15 and grid side rods 16. Slots 17 are provided for passing twist tabs 18 extending from anode 19. The tabs are twisted to lock mica 12 and anode 19 together. This use of the invention has proved its worth by demonstrating its superior locking ability and the elimination of damage to the mica separator caused by older forms of twist lock.
Although several embodiments of the invention have been shown and described, it should be understood that there is no intention to limit the invention to such embodiments, but rather that the following claims be interpreted to cover all modifications and alternatives within the spirit and scope of the invention.
What We claim is:
1. A joint between sheet materials comprising a first member having an elongated aperture therethrough, a second member bearing against a first surface of the first member and having a tab extending through said aperture, said tab lying in a surface displaced with respect to the surface of the second member, and said tab having wings extending away from the surface of the tab and bearing against a surface of said rst member opposite to said rst surface, whereby said members are locked together.
2. A vacuum tube having a mount structure therein, said mount structure including an anode and an insulating spacer at an end of said anode, said spacer having an elongated aperture therein, said anode having Va tab extending through the aperture with an edge of the anode bearing against a surface of the spacer and with the tab extending perpendicular to the spacer but at an angle to the adjacent anode wall, and wings extending laterally from the tab bearing on the surface of the spacer opposite to said rst surface, whereby said anode and spacer are locked together.
3. The process of assembling an anode having a tab Vin which there are diagonal slits extending from lateral edges thereof toward the free end of the tab with an insulating spacer having an elongated opening with central con` stricted portion and widened end portions, said process comprising inserting the tab through the opening in the spacer bringing the anode close to a surface of the spacer and twisting the tab to cause portions of the tab adjacent the slits to engage edges of the opening at thc wider portions thereof and to bend them out of the openings to bring them against the adjacent opposite surface of the spacer to lock the anode and spacer together.
References Cited in the le of this patent UNITED STATES PATENTS 2,002,358 Smith May 21, 1935 2,458,534 Schwerin Jan. 11, 1949 2,572,032 Jacobus Jr. et al. Oct. 23, 1951 2,625,665 Batzle Jan. 13, 1953
US228320A 1951-05-25 1951-05-25 Tab fastening device Expired - Lifetime US2722625A (en)

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Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2805907A (en) * 1955-09-30 1957-09-10 American Seating Co Table to construction and methods
US2862135A (en) * 1956-12-14 1958-11-25 Westinghouse Electric Corp Ear plate
US2901817A (en) * 1957-06-17 1959-09-01 Waldes Kohinoor Inc Tools for assembling external retaining rings
US2910609A (en) * 1956-06-07 1959-10-27 Gen Electric Low microphonics tube structures
US2932888A (en) * 1955-05-27 1960-04-19 Smiths America Corp Methods of joining parts
US2938133A (en) * 1958-12-16 1960-05-24 Stewart Engineering Company Electron gun assembly
US2963127A (en) * 1957-12-24 1960-12-06 Manville George Dewey Variable length brace
US2995806A (en) * 1957-10-08 1961-08-15 Gen Electric Co Ltd Methods of manufacturing waveguides
US3062261A (en) * 1954-01-28 1962-11-06 Sears Roebuck & Co Tool for assembling plates in flatwise engagement and method of assembling plates
US3068555A (en) * 1958-12-15 1962-12-18 Sylvania Electric Prod Method of staking and forming tabs
US3153294A (en) * 1962-04-23 1964-10-20 Car Go Inc Display stand construction
US3199179A (en) * 1960-02-15 1965-08-10 Laing Vortex Inc Method of making bladed rotors for flow machines
US3218767A (en) * 1960-05-19 1965-11-23 Owens Illinois Glass Co Poured double-walled structures
US3231791A (en) * 1963-06-06 1966-01-25 Square D Co Locking means for electromagnetic relays
US4076165A (en) * 1976-06-03 1978-02-28 Motorola, Inc. Mounting arrangement for chassis and printed circuit board with method of assembly
US5301465A (en) * 1992-06-18 1994-04-12 Dennis Caferro Planter, and processes for construction thereof and planting therein
US5770320A (en) * 1996-09-26 1998-06-23 Northern Telecom Limited Assembling sheet metal members
US5886322A (en) * 1996-01-16 1999-03-23 Black & Decker Inc. Assembly of an electrical contact terminal in an electrical appliance
US6131286A (en) * 1996-09-20 2000-10-17 Caterpillar Inc. Method for securing a first fabrication element to a second fabrication element during a welding operation
US6548184B1 (en) * 1998-07-18 2003-04-15 Rolls-Royce Plc Joint for sheet material and a method of joining sheet material
US20080184691A1 (en) * 2007-02-01 2008-08-07 Horchler Fred M Bale forming roller

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2002358A (en) * 1933-08-18 1935-05-21 Girard Model Works Inc Electrically lighted toy
US2458534A (en) * 1946-06-29 1949-01-11 Sonotone Corp Vibration suppressing suspension for tensioned filaments of electron space charge devices
US2572032A (en) * 1949-01-26 1951-10-23 Sonotone Corp Electrode and envelope assembly for multielectrode space discharge devices
US2625665A (en) * 1950-03-31 1953-01-13 Rca Corp Electron tube mount and method of assembly

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2002358A (en) * 1933-08-18 1935-05-21 Girard Model Works Inc Electrically lighted toy
US2458534A (en) * 1946-06-29 1949-01-11 Sonotone Corp Vibration suppressing suspension for tensioned filaments of electron space charge devices
US2572032A (en) * 1949-01-26 1951-10-23 Sonotone Corp Electrode and envelope assembly for multielectrode space discharge devices
US2625665A (en) * 1950-03-31 1953-01-13 Rca Corp Electron tube mount and method of assembly

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3062261A (en) * 1954-01-28 1962-11-06 Sears Roebuck & Co Tool for assembling plates in flatwise engagement and method of assembling plates
US2932888A (en) * 1955-05-27 1960-04-19 Smiths America Corp Methods of joining parts
US2805907A (en) * 1955-09-30 1957-09-10 American Seating Co Table to construction and methods
US2910609A (en) * 1956-06-07 1959-10-27 Gen Electric Low microphonics tube structures
US2862135A (en) * 1956-12-14 1958-11-25 Westinghouse Electric Corp Ear plate
US2901817A (en) * 1957-06-17 1959-09-01 Waldes Kohinoor Inc Tools for assembling external retaining rings
US2995806A (en) * 1957-10-08 1961-08-15 Gen Electric Co Ltd Methods of manufacturing waveguides
US2963127A (en) * 1957-12-24 1960-12-06 Manville George Dewey Variable length brace
US3068555A (en) * 1958-12-15 1962-12-18 Sylvania Electric Prod Method of staking and forming tabs
US2938133A (en) * 1958-12-16 1960-05-24 Stewart Engineering Company Electron gun assembly
US3199179A (en) * 1960-02-15 1965-08-10 Laing Vortex Inc Method of making bladed rotors for flow machines
US3218767A (en) * 1960-05-19 1965-11-23 Owens Illinois Glass Co Poured double-walled structures
US3153294A (en) * 1962-04-23 1964-10-20 Car Go Inc Display stand construction
US3231791A (en) * 1963-06-06 1966-01-25 Square D Co Locking means for electromagnetic relays
US4076165A (en) * 1976-06-03 1978-02-28 Motorola, Inc. Mounting arrangement for chassis and printed circuit board with method of assembly
US5301465A (en) * 1992-06-18 1994-04-12 Dennis Caferro Planter, and processes for construction thereof and planting therein
US5886322A (en) * 1996-01-16 1999-03-23 Black & Decker Inc. Assembly of an electrical contact terminal in an electrical appliance
US6131286A (en) * 1996-09-20 2000-10-17 Caterpillar Inc. Method for securing a first fabrication element to a second fabrication element during a welding operation
US6135666A (en) * 1996-09-20 2000-10-24 Caterpillar Inc. Apparatus and method for securing a first fabrication element to a second fabrication element during a welding operation
US5770320A (en) * 1996-09-26 1998-06-23 Northern Telecom Limited Assembling sheet metal members
US6548184B1 (en) * 1998-07-18 2003-04-15 Rolls-Royce Plc Joint for sheet material and a method of joining sheet material
US20080184691A1 (en) * 2007-02-01 2008-08-07 Horchler Fred M Bale forming roller

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