GB759943A - Improvements relating to split spring retaining rings - Google Patents

Improvements relating to split spring retaining rings

Info

Publication number
GB759943A
GB759943A GB600354A GB600354A GB759943A GB 759943 A GB759943 A GB 759943A GB 600354 A GB600354 A GB 600354A GB 600354 A GB600354 A GB 600354A GB 759943 A GB759943 A GB 759943A
Authority
GB
United Kingdom
Prior art keywords
centre
retaining rings
improvements relating
spring retaining
split
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB600354A
Inventor
Philip Gordon Binns
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB600354A priority Critical patent/GB759943A/en
Publication of GB759943A publication Critical patent/GB759943A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F16B21/00—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings
    • F16B21/10—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts
    • F16B21/16—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts with grooves or notches in the pin or shaft
    • F16B21/18—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts with grooves or notches in the pin or shaft with circlips or like resilient retaining devices, i.e. resilient in the plane of the ring or the like; Details
    • F16B21/183—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts with grooves or notches in the pin or shaft with circlips or like resilient retaining devices, i.e. resilient in the plane of the ring or the like; Details internal, i.e. with spreading action

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)

Abstract

759,943. Circlips. ROLLS-ROYCE, Ltd. March 1, 1955 [March ], 1954], No. 6003/54. Class 89 (2). A circlip is defined by inner and outer circles struck from centres Y, X, respectively, the distance therebetween being such that the centre of gravity of the circlip lies at the centre X. The clip is to be seated in a groove in a bore of a shaft so that centre X is coincident with the axis of rotation of the shaft. The clip is split at P and tool-engaging holes Q are provided adjacent the ends. The outer periphery may be chamfered on a radius struck from centre Z, the three centres being located on a diameter which bisects the split P.
GB600354A 1954-03-01 1954-03-01 Improvements relating to split spring retaining rings Expired GB759943A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB600354A GB759943A (en) 1954-03-01 1954-03-01 Improvements relating to split spring retaining rings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB600354A GB759943A (en) 1954-03-01 1954-03-01 Improvements relating to split spring retaining rings

Publications (1)

Publication Number Publication Date
GB759943A true GB759943A (en) 1956-10-24

Family

ID=9806639

Family Applications (1)

Application Number Title Priority Date Filing Date
GB600354A Expired GB759943A (en) 1954-03-01 1954-03-01 Improvements relating to split spring retaining rings

Country Status (1)

Country Link
GB (1) GB759943A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2888877A1 (en) * 2005-07-21 2007-01-26 Snecma Vibration dampening device for aircraft, has dampening rod formed by split ring and self balanced in rotation using reduction of rod`s section in zone that is diametrically opposite to ends with respect to rotational axis
WO2015117994A1 (en) * 2014-02-06 2015-08-13 Hugo Benzing Gmbh & Co. Kg Securing ring
US20160047270A1 (en) * 2014-05-29 2016-02-18 United Technologies Corporation Split ring spring dampers for gas turbine rotor assemblies

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2888877A1 (en) * 2005-07-21 2007-01-26 Snecma Vibration dampening device for aircraft, has dampening rod formed by split ring and self balanced in rotation using reduction of rod`s section in zone that is diametrically opposite to ends with respect to rotational axis
WO2015117994A1 (en) * 2014-02-06 2015-08-13 Hugo Benzing Gmbh & Co. Kg Securing ring
US20160047270A1 (en) * 2014-05-29 2016-02-18 United Technologies Corporation Split ring spring dampers for gas turbine rotor assemblies
US10309224B2 (en) * 2014-05-29 2019-06-04 United Technologies Corporation Split ring spring dampers for gas turbine rotor assemblies

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