US3042391A - Compression spring - Google Patents

Compression spring Download PDF

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Publication number
US3042391A
US3042391A US842255A US84225559A US3042391A US 3042391 A US3042391 A US 3042391A US 842255 A US842255 A US 842255A US 84225559 A US84225559 A US 84225559A US 3042391 A US3042391 A US 3042391A
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spring
annular end
compression spring
segments
elements
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US842255A
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Glaser Jerry
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Garrett Corp
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Garrett Corp
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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
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00Springs
    • F16F1/02Springs made of steel or other material having low internal friction; Wound, torsion, leaf, cup, ring or the like springs, the material of the spring not being relevant

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  • This invention relates to a compression spring and has for its object a precision compression spring which will maintain normality of the end thrust with respect to the axis of the spring so as to apply a symmetrical load.
  • Another object of the invention is a compression spring which will avoid twisting or rotational forces incident to its compression or extension.
  • Another object of the invention is a compression spring providing a substantially uniform linear spring rate which may be varied within relatively wide limits.
  • a still further object of the invention is a compression spring in accordance with the preceding objects which will have a low spring rate, Le. a small force will cause a relatively large deflection.
  • FIG. 1 is an isometric view of a compression spring according to the present invention
  • FIG. 2 is a fragmentary view similar to FIG. 1 and showing a modified construction.
  • the spring is given the general reference numeral 1 and is of generally tubular construction with opposite end thrust annuli 2 and 3 having a plurality of thrust lugs or extensions 4 thereon.
  • the body portion of the spring is provided with a plurality of parallel discontinuous circumferential slots 5 and with a plurality of circumferentially spaced axially extending slots 6.
  • the axially extending slots 6 divide the body of the tubular spring into three separated sectors generally designated at 7.
  • the slots 5 divide the material in the sectors 7 into a plurality of parallel circumferential elements 8 and the discontinuities in the slots 5 provide the elements 8 with end ties 9 joining alternate opposite ends of the elements 8 with their adjacent counterparts.
  • the resultant group of parallel elements 8 within each of the sectors 7 are thus, with end ties 9, of substantially zigzag configuration.
  • the extreme elements 8 are connected to their adjacent thrust annuli 2 and 3 by end ties 11 and 12, respectively.
  • the ties 11 and 12 are formed at the same side of each of the groups of elements 8 in each of the sectors 7.
  • the tieing of the groups to the end thrust annuli at opposite sides of the group may be used with the thrust lug position of FIG. 1 and conversely the thrust lug position of FIG. 2 may be used with the end tie arrangement of FIG. 1.
  • the versatility of these arrangements contributes to the wide variation in spring characteristics which may be designed into the spring construction to cover varying service requirements.
  • the spring may be formed from a tube with the slots machined therein or may be stamped from a flat sheet and rolled into its tubular form. Grinding or machining operations may be desirable to insure that the surfaces of the end thrust lugs are normal to the axis of the spring and heat treating of the completed spring for strength may be desirable with a final normalizing grinding operation after heat treatment. Again, these elements of construction and formation are flexible within the desired requirements of spring operation.
  • a compression spring of generally tubular construction comprising: spaced annular end members; a plurality of individual axially extending segments circumferentially spaced apart by axial slots and disposed between said annular end members, each of said segments including a plurality of spaced, parallel, circumferentially extending elements connected at alternate ends in a substantially zigzag formation; and means securing said individual segments to said annular end members.
  • a compression spring of generally tubular construction comprising: spaced annular end members; a plurality of individual axially extending segments circumferentially spaced apart by axial slots and disposed between said annular end members, each of said segments including a plurality of spaced, parallel, circumferentially extending elements connected at alternate ends in a substantially zigzag formation; and means securing said individual segments to said annular end members, said means comprising end ties extending from the element adjacent the respective annular end member to said end member.
  • a compression spring of generally tubular construction comprising: spaced annular end members; a plurality of individual axially extending segments circumferentially spaced apart by axial slots and disposed between said annular end members, each of said segments including a plurality of spaced, parallel, circumferentially extending elements connected at alternate ends in a substantially zigzag formation; and means securing said individual segments to said annular end members, said means comprising end ties extending from the element adjacent the respective annular end member to said end member, said end ties being located at the same side of each of the segments.
  • a compression spring of generally tubular construction comprising: spaced annular end members; a plurality of individual axially extending segments circumferentially spaced apart by axial slots and disposed between said annular end members, each of said segments including a plurality of spaced, parallel, circumferentially extending elements connected at alternate ends in a substantially zigzag formation; and means securing said individual segments to said annular end members, said means comprising end ties extending from the element adjacent the respective annular end member to said end member, said end ties being located at opposite sides of each of the segments.
  • a compression spring of generally tubular construction comprising: spaced annular end members; a plurality of individual axially extending segments circumferentially spaced apart by axial slots and disposed between said annular end members, each of said segments including a plurality of spaced, parallel, circumferentially extending elements connected at alternate ends in a substantially zigzag formation; means securing said individual segments to said annular end members, said means comprising end ties extending from the element adjacent the respective annular end member to said end member; and end thrust lugs extending from said annular end members intermediate said end ties.
  • a compression spring of generally tubular construction comprising: spaced annular end members; a plurality of individual axially extending segments circumferentially spaced apart by axial slots and disposed between said 15 annular end members, each of said segments including a plurality of spaced, parallel, circumferentially extending elements connected at alternate ends in a substantially zigzag formation; means securing said individual segments to said annular end members, said means comprising end ties extending from the element adjacent the respective annular end member to said end member; and end thrust lugs extending from said annular end members adjacent said end ties.

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

July 3, 1962 J. GLASER 3,042,391
COMPRESSION SPRING Filed Sept. 25, 1959 INVENTOR. JERRY GLASER,
A rfomey.
ite tates atent 3, 12,391 Fatented July 3, 1962 ffice This invention relates to a compression spring and has for its object a precision compression spring which will maintain normality of the end thrust with respect to the axis of the spring so as to apply a symmetrical load.
Another object of the invention is a compression spring which will avoid twisting or rotational forces incident to its compression or extension.
Another object of the invention is a compression spring providing a substantially uniform linear spring rate which may be varied within relatively wide limits.
A still further object of the invention is a compression spring in accordance with the preceding objects which will have a low spring rate, Le. a small force will cause a relatively large deflection.
Other objects and features of the invention will be readily apparent to those skilled in the art from the specification and appended drawings illustrating certain preferred embodiments in which:
FIG. 1 is an isometric view of a compression spring according to the present invention;
FIG. 2 is a fragmentary view similar to FIG. 1 and showing a modified construction.
In the specific embodiment illustrated in FIG. 1 the spring is given the general reference numeral 1 and is of generally tubular construction with opposite end thrust annuli 2 and 3 having a plurality of thrust lugs or extensions 4 thereon. The body portion of the spring is provided with a plurality of parallel discontinuous circumferential slots 5 and with a plurality of circumferentially spaced axially extending slots 6. The axially extending slots 6 divide the body of the tubular spring into three separated sectors generally designated at 7. The slots 5 divide the material in the sectors 7 into a plurality of parallel circumferential elements 8 and the discontinuities in the slots 5 provide the elements 8 with end ties 9 joining alternate opposite ends of the elements 8 with their adjacent counterparts.
The resultant group of parallel elements 8 within each of the sectors 7 are thus, with end ties 9, of substantially zigzag configuration. The extreme elements 8 are connected to their adjacent thrust annuli 2 and 3 by end ties 11 and 12, respectively. As illustrated in FIG. 1 the ties 11 and 12 are formed at the same side of each of the groups of elements 8 in each of the sectors 7.
In the modification of FIG. 2 the end tie 12 has been moved to the opposite side of the group of elements 8 and is here shown at 13. In this construction the end tie 11 remains in the position shown in FIG. 1 so that in the modification of FIG. 2 the group of parallel elements 8 is connected to the end thrust annuli at opposite sides of the group. FiG. 2 illustrates a further modification in the position of the end thrust lug 4 which has now been moved into the position shown at 14 opposite the end tie 13, whereas in FIG. 1 the thrust lugs 4 are shown centrally of the group of parallel spring elements 8.
The tieing of the groups to the end thrust annuli at opposite sides of the group may be used with the thrust lug position of FIG. 1 and conversely the thrust lug position of FIG. 2 may be used with the end tie arrangement of FIG. 1. The versatility of these arrangements contributes to the wide variation in spring characteristics which may be designed into the spring construction to cover varying service requirements.
The spring may be formed from a tube with the slots machined therein or may be stamped from a flat sheet and rolled into its tubular form. Grinding or machining operations may be desirable to insure that the surfaces of the end thrust lugs are normal to the axis of the spring and heat treating of the completed spring for strength may be desirable with a final normalizing grinding operation after heat treatment. Again, these elements of construction and formation are flexible within the desired requirements of spring operation.
While the specific embodiment of the invention illustrated in the drawing is comprised of three sectors 7,
that is, three groups of the spring elements 8, it is obvious that the number of separations is not limited to three and that two or more than three groups of elements may be utilized in the spring design according to performance requirements.
While certain preferred embodiments of the invention have been specifically disclosed, it is understood that the invention is not limited thereto, as many variations will be readily apparent to those skilled in the art and the invention is to be given its broadest possible interpretation consistent with the prior art.
What is claimed is:
1. A compression spring of generally tubular construction comprising: spaced annular end members; a plurality of individual axially extending segments circumferentially spaced apart by axial slots and disposed between said annular end members, each of said segments including a plurality of spaced, parallel, circumferentially extending elements connected at alternate ends in a substantially zigzag formation; and means securing said individual segments to said annular end members.
2. A compression spring of generally tubular construction comprising: spaced annular end members; a plurality of individual axially extending segments circumferentially spaced apart by axial slots and disposed between said annular end members, each of said segments including a plurality of spaced, parallel, circumferentially extending elements connected at alternate ends in a substantially zigzag formation; and means securing said individual segments to said annular end members, said means comprising end ties extending from the element adjacent the respective annular end member to said end member.
3. A compression spring of generally tubular construction comprising: spaced annular end members; a plurality of individual axially extending segments circumferentially spaced apart by axial slots and disposed between said annular end members, each of said segments including a plurality of spaced, parallel, circumferentially extending elements connected at alternate ends in a substantially zigzag formation; and means securing said individual segments to said annular end members, said means comprising end ties extending from the element adjacent the respective annular end member to said end member, said end ties being located at the same side of each of the segments.
4. A compression spring of generally tubular construction comprising: spaced annular end members; a plurality of individual axially extending segments circumferentially spaced apart by axial slots and disposed between said annular end members, each of said segments including a plurality of spaced, parallel, circumferentially extending elements connected at alternate ends in a substantially zigzag formation; and means securing said individual segments to said annular end members, said means comprising end ties extending from the element adjacent the respective annular end member to said end member, said end ties being located at opposite sides of each of the segments.
5. A compression spring of generally tubular construction comprising: spaced annular end members; a plurality of individual axially extending segments circumferentially spaced apart by axial slots and disposed between said annular end members, each of said segments including a plurality of spaced, parallel, circumferentially extending elements connected at alternate ends in a substantially zigzag formation; means securing said individual segments to said annular end members, said means comprising end ties extending from the element adjacent the respective annular end member to said end member; and end thrust lugs extending from said annular end members intermediate said end ties.
6. A compression spring of generally tubular construction comprising: spaced annular end members; a plurality of individual axially extending segments circumferentially spaced apart by axial slots and disposed between said 15 annular end members, each of said segments including a plurality of spaced, parallel, circumferentially extending elements connected at alternate ends in a substantially zigzag formation; means securing said individual segments to said annular end members, said means comprising end ties extending from the element adjacent the respective annular end member to said end member; and end thrust lugs extending from said annular end members adjacent said end ties.
References Cited in the file of this patent UNITED STATES PATENTS 993,208 Watson et al. May 23, 1911 1,541,124 Dunham June 9, 1925 FOREIGN PATENTS 1,090,004 France Oct. 13, 1954
US842255A 1959-09-25 1959-09-25 Compression spring Expired - Lifetime US3042391A (en)

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Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1260882B (en) * 1963-12-26 1968-02-08 Drafto Corp Feather from a folded ribbon
JPS49123463U (en) * 1973-02-20 1974-10-23
US4270610A (en) * 1980-01-15 1981-06-02 Halliburton Company Annulus pressure operated closure valve with improved power mandrel
US4542708A (en) * 1984-01-06 1985-09-24 Raytheon Company Composite cable fairing
US4973221A (en) * 1989-04-17 1990-11-27 General Electric Company Gas turbine engine motor assembly
US5069413A (en) * 1988-04-11 1991-12-03 E. I. Du Pont De Nemours And Company Centrifuge motor mount having two slotted members
US5558393A (en) * 1995-01-24 1996-09-24 Proteus Engineering, Inc. Composite multi-wave compression spring
DE19812527A1 (en) * 1998-03-21 1999-09-30 Zahnradwerk Pritzwalk Gmbh Differential coupling
US6068250A (en) * 1996-09-23 2000-05-30 Proteus Engineering Inc. Composite multi-wave compression spring
US20050049051A1 (en) * 2001-06-28 2005-03-03 Pinard Adam I. Lead screw coupling
DE10338080A1 (en) * 2003-08-19 2005-03-10 Bosch Gmbh Robert Bourdon tube for actuator
US20090321668A1 (en) * 2008-06-27 2009-12-31 Caterpillar Inc. Distributed stiffness biasing spring for actuator system and fuel injector using same
US20150033918A1 (en) * 2013-07-30 2015-02-05 Schuster Maschinenbau Gmbh Spindle Unit for a Machining Device with a Spindle Lock
US20150060433A1 (en) * 2013-08-29 2015-03-05 Varian Semiconductor Equipment Associates, Inc. High temperature platen power contact
US10000102B2 (en) * 2015-06-19 2018-06-19 GM Global Technology Operations LLC Tunable compact spring aid
US10933525B2 (en) * 2018-07-04 2021-03-02 Fanuc Corporation Horizontal articulated robot
WO2024003861A1 (en) * 2022-07-01 2024-01-04 3Dific Societa' A Responsabilita' Limitata Flexible joint

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US993208A (en) * 1911-01-09 1911-05-23 Cecil Watson Spring.
US1541124A (en) * 1920-06-17 1925-06-09 Dunham Orson Winfield Stuffing box for bearings
FR1090004A (en) * 1953-07-22 1955-03-25 Spring

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US993208A (en) * 1911-01-09 1911-05-23 Cecil Watson Spring.
US1541124A (en) * 1920-06-17 1925-06-09 Dunham Orson Winfield Stuffing box for bearings
FR1090004A (en) * 1953-07-22 1955-03-25 Spring

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1260882B (en) * 1963-12-26 1968-02-08 Drafto Corp Feather from a folded ribbon
JPS49123463U (en) * 1973-02-20 1974-10-23
JPS5427470Y2 (en) * 1973-02-20 1979-09-06
US4270610A (en) * 1980-01-15 1981-06-02 Halliburton Company Annulus pressure operated closure valve with improved power mandrel
US4542708A (en) * 1984-01-06 1985-09-24 Raytheon Company Composite cable fairing
US5069413A (en) * 1988-04-11 1991-12-03 E. I. Du Pont De Nemours And Company Centrifuge motor mount having two slotted members
US4973221A (en) * 1989-04-17 1990-11-27 General Electric Company Gas turbine engine motor assembly
US5558393A (en) * 1995-01-24 1996-09-24 Proteus Engineering, Inc. Composite multi-wave compression spring
US6068250A (en) * 1996-09-23 2000-05-30 Proteus Engineering Inc. Composite multi-wave compression spring
DE19812527C2 (en) * 1998-03-21 2000-04-27 Zahnradwerk Pritzwalk Gmbh Differential coupling
DE19812527A1 (en) * 1998-03-21 1999-09-30 Zahnradwerk Pritzwalk Gmbh Differential coupling
US20050049051A1 (en) * 2001-06-28 2005-03-03 Pinard Adam I. Lead screw coupling
DE10338080A1 (en) * 2003-08-19 2005-03-10 Bosch Gmbh Robert Bourdon tube for actuator
US20090321668A1 (en) * 2008-06-27 2009-12-31 Caterpillar Inc. Distributed stiffness biasing spring for actuator system and fuel injector using same
US7950596B2 (en) 2008-06-27 2011-05-31 Caterpillar Inc. Distributed stiffness biasing spring for actuator system and fuel injector using same
US20150033918A1 (en) * 2013-07-30 2015-02-05 Schuster Maschinenbau Gmbh Spindle Unit for a Machining Device with a Spindle Lock
US9700980B2 (en) * 2013-07-30 2017-07-11 Schuster Maschinenbau Gmbh Spindle unit for a machining device with a spindle lock
US20150060433A1 (en) * 2013-08-29 2015-03-05 Varian Semiconductor Equipment Associates, Inc. High temperature platen power contact
US10000102B2 (en) * 2015-06-19 2018-06-19 GM Global Technology Operations LLC Tunable compact spring aid
US10933525B2 (en) * 2018-07-04 2021-03-02 Fanuc Corporation Horizontal articulated robot
WO2024003861A1 (en) * 2022-07-01 2024-01-04 3Dific Societa' A Responsabilita' Limitata Flexible joint

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