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US1365719A - Machine-bolt anchor - Google Patents

Machine-bolt anchor Download PDF

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Publication number
US1365719A
US1365719A US318138A US31813819A US1365719A US 1365719 A US1365719 A US 1365719A US 318138 A US318138 A US 318138A US 31813819 A US31813819 A US 31813819A US 1365719 A US1365719 A US 1365719A
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Prior art keywords
machine
bolt
shell
anchorage
bolt anchor
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Expired - Lifetime
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US318138A
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Ogden John Edward
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Priority to US318138A priority Critical patent/US1365719A/en
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    • 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
    • F16B13/00Dowels or other devices fastened in walls or the like by inserting them in holes made therein for that purpose
    • F16B13/04Dowels or other devices fastened in walls or the like by inserting them in holes made therein for that purpose with parts gripping in the hole or behind the reverse side of the wall after inserting from the front
    • F16B13/06Dowels or other devices fastened in walls or the like by inserting them in holes made therein for that purpose with parts gripping in the hole or behind the reverse side of the wall after inserting from the front combined with expanding sleeve
    • F16B13/061Dowels or other devices fastened in walls or the like by inserting them in holes made therein for that purpose with parts gripping in the hole or behind the reverse side of the wall after inserting from the front combined with expanding sleeve of the buckling type

Definitions

  • his invention relates to improvements in machine bolt anchorages and its object is to provide a simple and inexpensive device for this purpose which is easy to operate and which will form an eflg'ective anchorage for machinebolts and the like, which Wlll not effectively engage in the material of which the wall or other structure is constructed .to which the bolt is. to be applied.' More specifically, its object is to provide a device having end members of comparatively rigid construction joined by a shell of collapsible metal which will be distorted when the end members are moved toward each other and will form the desired anchorage.
  • Figure 1 is an elevation of anchorage de vice which is made according to and embodies this invention.
  • Fig. 2 is a longitudinal sectional elevation of the same device.
  • Fig. 3 is a sectional plan view taken on the line 33 of Fig. 2.
  • Fig. 4 is a view similar to Fig. 3 illustrat ing a modified form of construction.
  • - ig. 5 is a sectional elevation of a device like that shown in the preceding figures, placed in a hole in a wall and with a bolt inserted in the device.
  • Fj 6 is a similar view of like parts showing t e positions they assume after expanslon.
  • 10 designates a collar of rigid metal which may be cast, stamped or forged. This has a central clearance hole for a bolt, and roove near one of its ends. 11 is a nut WhlCh is internally threaded to receive the threads of a bolt. This has also a curved annular groove near one of its ends.
  • this part of the-structure may be constructed from a flat blank bent around a longitudinal axis into desired form, in which cases its opposite ends will meet, as shown at 15 in Fig. 3. 1
  • the three parts of the device may be held together by the engagement of the shell with the grooves in the collar and nut.
  • the shell in a plurality of longitudinally divided parts such as 16 and 17 in Fig. 4 in which case it may be desirable to provide some way of holding the parts thereof together, as by means of wiresor springs both of which are well known in this art for this same purpose.
  • the shell 12 will be collapsed as shown in Fig. 6. .
  • the ends of the shell will be forced outwardly into the wall of the hole 21 as shown at 18 and the intermediate portion ⁇ will be buckled inwardly against the shank of the bolt and outwardly against the wall of the hole as shown at 19, this forming the desired anchorage.
  • An anchorage device comprising two rigid end members, and a separate intermediate shell of collapsible material joining said members.
  • An anchorage device comprising two rigid end members provided with annular grooves near their adjacent ends, and an intermediate shell of collapsible material fitted into said grooves and joining said members.
  • An anchorage device comprising two rigid end members in axialalinement, one of which is internally threaded, and a separate intermediate shell of comparatively thin collapsible metal joining said members.
  • An anchorage device comprising two rigid end members in axial alinement provided with annular grooves near their adjacent ends, one of which is internally threaded, and an intermediate shell of comparatively thin collapsible metal fitted into said grooves and joining: said members.
  • An anchorage device comprising two rigid end members in axial alinement provided with annular grooves near their ad jacent ends, one of which is internally threaded, and a plurality of parts forming an intermediate shell of comparatively thin collapsible metal fitted into said grooves and joining, said members.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Dowels (AREA)

Description

J. E. OGDEN.
MACHINE BOLT ANCHOR.
APPLICATION FILED AUG.18. 1919.
1 ,365,719. Patented Jan. 18, 1921.
I acitizen of the United States of America,
" an annular curved JOHN EDWARD OGDEN, OF CORNWALL, NEW YORK.
MACHINE-BOLT ANCHOR.
Specification of Letters Patent.
Patented Jan. 18,1921.
Application filed August 18, 1918. Serial No. 818,138
To all whom it may concern:
' Be it known that I, J OHN EDWARD OGDEN,-
and a resident of Mountainville; town of Cornwall, Orange county, and State of New York, have invented certain new and useful Improvements in Machine-Bolt Anchorages, of which the following is a specification, reference being had to the accompanying drawin s, forming a part thereof.
his invention relates to improvements in machine bolt anchorages and its object is to provide a simple and inexpensive device for this purpose which is easy to operate and which will form an eflg'ective anchorage for machinebolts and the like, which Wlll not effectively engage in the material of which the wall or other structure is constructed .to which the bolt is. to be applied.' More specifically, its object is to provide a device having end members of comparatively rigid construction joined by a shell of collapsible metal which will be distorted when the end members are moved toward each other and will form the desired anchorage.
These and other objects of the invention will ap ear in the following specification in which Fwill describe the invention, the novel features of which will be set forth in appended claims.
Referring to the drawings:
Figure 1 is an elevation of anchorage de vice which is made according to and embodies this invention.
Fig. 2 is a longitudinal sectional elevation of the same device.
Fig. 3 is a sectional plan view taken on the line 33 of Fig. 2.
Fig. 4: is a view similar to Fig. 3 illustrat ing a modified form of construction.
- ig. 5 is a sectional elevation of a device like that shown in the preceding figures, placed in a hole in a wall and with a bolt inserted in the device.
Fj 6 is a similar view of like parts showing t e positions they assume after expanslon.
Like characters of reference designate corresponding parts in all the figures.
10 designates a collar of rigid metal which may be cast, stamped or forged. This has a central clearance hole for a bolt, and roove near one of its ends. 11 is a nut WhlCh is internally threaded to receive the threads of a bolt. This has also a curved annular groove near one of its ends.
12 is a tubular shell of comparatively thin metal which may have its end portions rolled into the annular grooves of the collar and nut, as at 13 and 14, and may have its intermediate part rolled down to have an outside diameter equal to that of the collar and nut. Or if desired, this part of the-structure may be constructed from a flat blank bent around a longitudinal axis into desired form, in which cases its opposite ends will meet, as shown at 15 in Fig. 3. 1
In either of these cases the three parts of the device may be held together by the engagement of the shell with the grooves in the collar and nut.
It is also within the scope of this invention to make the shell in a plurality of longitudinally divided parts such as 16 and 17 in Fig. 4 in which case it may be desirable to provide some way of holding the parts thereof together, as by means of wiresor springs both of which are well known in this art for this same purpose.
The manner in which this device isused is illustrated in Figs. 5 and 6 in which 20 designates a part of a wall in which a hole pull the nut toward the collar and in doing.
this the shell 12 will be collapsed as shown in Fig. 6. .The ends of the shell will be forced outwardly into the wall of the hole 21 as shown at 18 and the intermediate portion \will be buckled inwardly against the shank of the bolt and outwardly against the wall of the hole as shown at 19, this forming the desired anchorage.
I have described What I consider preferred forms of construction, but intend no limitations other than those imposed by the appended claims.
What I claim is:
1. An anchorage device comprising two rigid end members, and a separate intermediate shell of collapsible material joining said members.
2. An anchorage device comprising two rigid end members provided with annular grooves near their adjacent ends, and an intermediate shell of collapsible material fitted into said grooves and joining said members.
3. An anchorage device comprising two rigid end members in axialalinement, one of which is internally threaded, and a separate intermediate shell of comparatively thin collapsible metal joining said members.
4. An anchorage device comprising two rigid end members in axial alinement provided with annular grooves near their adjacent ends, one of which is internally threaded, and an intermediate shell of comparatively thin collapsible metal fitted into said grooves and joining: said members.
5. An anchorage device comprising two rigid end members in axial alinement provided with annular grooves near their ad jacent ends, one of which is internally threaded, and a plurality of parts forming an intermediate shell of comparatively thin collapsible metal fitted into said grooves and joining, said members.
In Witness whereof I hereunto set my hand this 12th day of August 1919.
JOHN EDWARD OGDEN.
\Vitness:
I.- B. MOORE.
US318138A 1919-08-18 1919-08-18 Machine-bolt anchor Expired - Lifetime US1365719A (en)

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US318138A US1365719A (en) 1919-08-18 1919-08-18 Machine-bolt anchor

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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2630039A (en) * 1946-09-03 1953-03-03 William F Klemm Expansion arbor
US4422813A (en) * 1981-03-05 1983-12-27 Sheldon Greenbaum Wall expansion device with anchoring socket
US4889457A (en) * 1988-04-11 1989-12-26 Premier Industrial Corporation Load indicator
US5401131A (en) * 1992-07-10 1995-03-28 Yoshino Seiki Inc. Expansion anchor
US6088902A (en) * 1994-07-22 2000-07-18 Summers; Dennis Arthur Method of fixing a tubular metal member in an aperture and tool therefor
US20050158138A1 (en) * 2004-01-21 2005-07-21 Stefan Schneider Blind rivet nut
US20050180837A1 (en) * 2004-02-16 2005-08-18 Newfrey Llc Blind rivet
US20050201844A1 (en) * 2004-01-21 2005-09-15 Davies John D. Blind rivet nut
US20070147971A1 (en) * 2000-12-21 2007-06-28 Gary Jennings Blind rivet
US20110058916A1 (en) * 2009-09-09 2011-03-10 Toosky Rahmatollah F Self-interlocking sleeve-core shear pin fastener
US20140130910A1 (en) * 2012-11-14 2014-05-15 The Boeing Company Bushing assemblies, bushing assembly kits, apparatuses including bushing assemblies, and associated methods
WO2015002592A1 (en) * 2013-07-05 2015-01-08 Scania Cv Ab Deformable sliding bushing
US8987612B2 (en) 2012-11-26 2015-03-24 The Boeing Company Bushings, apparatuses including bushings, and associated methods
US9404521B2 (en) 2012-12-12 2016-08-02 Polaris Fastening Consulting, Llc Self integrating structural insert sleeve
US10220435B2 (en) 2015-08-26 2019-03-05 Polaris Fastener Testing And Tooling, Llc Installation tooling system for buckle and swage type fastener

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2630039A (en) * 1946-09-03 1953-03-03 William F Klemm Expansion arbor
US4422813A (en) * 1981-03-05 1983-12-27 Sheldon Greenbaum Wall expansion device with anchoring socket
US4889457A (en) * 1988-04-11 1989-12-26 Premier Industrial Corporation Load indicator
US5401131A (en) * 1992-07-10 1995-03-28 Yoshino Seiki Inc. Expansion anchor
US6088902A (en) * 1994-07-22 2000-07-18 Summers; Dennis Arthur Method of fixing a tubular metal member in an aperture and tool therefor
US20070147971A1 (en) * 2000-12-21 2007-06-28 Gary Jennings Blind rivet
US7396287B2 (en) 2000-12-21 2008-07-08 Newfrey Llc Blind rivet
US20050158138A1 (en) * 2004-01-21 2005-07-21 Stefan Schneider Blind rivet nut
US20050201844A1 (en) * 2004-01-21 2005-09-15 Davies John D. Blind rivet nut
US7223056B2 (en) * 2004-01-21 2007-05-29 Newfrey Llc Blind rivet nut
US20050180837A1 (en) * 2004-02-16 2005-08-18 Newfrey Llc Blind rivet
US20110058916A1 (en) * 2009-09-09 2011-03-10 Toosky Rahmatollah F Self-interlocking sleeve-core shear pin fastener
US8434984B2 (en) * 2009-09-09 2013-05-07 Polaris Fastening Consulting, Llc Self-interlocking sleeve-core shear pin fastener
US20140130910A1 (en) * 2012-11-14 2014-05-15 The Boeing Company Bushing assemblies, bushing assembly kits, apparatuses including bushing assemblies, and associated methods
US9016992B2 (en) * 2012-11-14 2015-04-28 The Boeing Company Bushing assemblies, bushing assembly kits, apparatuses including bushing assemblies, and associated methods
US8987612B2 (en) 2012-11-26 2015-03-24 The Boeing Company Bushings, apparatuses including bushings, and associated methods
US9404521B2 (en) 2012-12-12 2016-08-02 Polaris Fastening Consulting, Llc Self integrating structural insert sleeve
WO2015002592A1 (en) * 2013-07-05 2015-01-08 Scania Cv Ab Deformable sliding bushing
CN105283679A (en) * 2013-07-05 2016-01-27 斯堪尼亚商用车有限公司 Deformable sliding bushing
RU2633217C2 (en) * 2013-07-05 2017-10-11 Сканиа Св Аб Deformable sliding bushing
US10220435B2 (en) 2015-08-26 2019-03-05 Polaris Fastener Testing And Tooling, Llc Installation tooling system for buckle and swage type fastener

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