GB496222A - Improvements in or relating to resilient or suspension devices - Google Patents

Improvements in or relating to resilient or suspension devices

Info

Publication number
GB496222A
GB496222A GB14280/37A GB1428037A GB496222A GB 496222 A GB496222 A GB 496222A GB 14280/37 A GB14280/37 A GB 14280/37A GB 1428037 A GB1428037 A GB 1428037A GB 496222 A GB496222 A GB 496222A
Authority
GB
United Kingdom
Prior art keywords
rubber
parts
convolutions
resilient
rapidly
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
GB14280/37A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB496222A publication Critical patent/GB496222A/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
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00—Springs
    • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/40—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers consisting of a stack of similar elements separated by non-elastic intermediate layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/04—Aircraft characterised by the type or position of power plants of piston type
    • 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
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F2236/00—Mode of stressing of basic spring or damper elements or devices incorporating such elements
    • F16F2236/12—Mode of stressing of basic spring or damper elements or devices incorporating such elements loaded in combined stresses

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Springs (AREA)

Abstract

496,222. Resilient mountings. GOLDSCHMIDT, M. May 22, 1937, No. 14280. Convention date, May 23, 1936. [Class 108 (iii)] A resilient suspension device comprises metal parts 2, 3 each in the form of a continuous helix, the interspaces between the convolutions of the parts being wholly or partly filled by rubber 5 vulcanized thereto. The parts are connected, for example, to the journal 1 of an aircraft engine and the frame 4 of the aircraft relative axial movements of which are damped by rapidly-increasing resistance of the rubber and relative radial and torsional movements by an initial slight resistance followed by a rapidly-increasing resistance. The convolutions are spaced by coiled metal strips 6, 8 which contain rubber inserts 12, 13 and are clamped in position by sprung-in rings 9 or by screwed flanges. The edges of the convolutions are covered with rubber 10, 11. The Specification as open to inspection under Sect. 91 comprises also constructions in which the helical parts are replaced (a) by conical discs, and (b) by discs having annular curved depressions. This subject-matter does not appear in the Specification as accepted.
GB14280/37A 1936-05-23 1937-05-22 Improvements in or relating to resilient or suspension devices Expired GB496222A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR496222X 1936-05-23

Publications (1)

Publication Number Publication Date
GB496222A true GB496222A (en) 1938-11-22

Family

ID=8904857

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14280/37A Expired GB496222A (en) 1936-05-23 1937-05-22 Improvements in or relating to resilient or suspension devices

Country Status (1)

Country Link
GB (1) GB496222A (en)

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