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GB430337A - Improvements in and relating to shock-absorbers - Google Patents

Improvements in and relating to shock-absorbers

Info

Publication number
GB430337A
GB430337A GB31634/33A GB3163433A GB430337A GB 430337 A GB430337 A GB 430337A GB 31634/33 A GB31634/33 A GB 31634/33A GB 3163433 A GB3163433 A GB 3163433A GB 430337 A GB430337 A GB 430337A
Authority
GB
United Kingdom
Prior art keywords
piston
chambers
chamber
pressure
air
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
GB31634/33A
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 GB430337A publication Critical patent/GB430337A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F16F9/00Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
    • F16F9/02Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using gas only or vacuum
    • F16F9/0209Telescopic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/58Arrangements or adaptations of shock-absorbers or springs
    • B64C25/60Oleo legs
    • 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
    • F16F9/00Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
    • F16F9/06Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using both gas and liquid
    • F16F9/064Units characterised by the location or shape of the expansion chamber

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Damping Devices (AREA)

Abstract

430,337. Pneumatic shock-absorbers. LANGGUTH, W., 61, Rue Corot, Ville-d'Avray, Seine-et-Oise, France. Nov. 13, 1933, No. 31634. Convention date, Nov. 12, 1932. [Class 108 (iii)] In a pneumatic shockabsorber having a plurality of chambers, at a given value of the pressure in the primary chamber due to movement of a piston therein, the primary chamber is placed in communication with a secondary chamber of equal pressure so that on increase of pressure in the primary chamber the pressure curve of the primary chamber deviates in such a manner that the tangent to the new portion of the curve at the point of deviation is nearer the horizontal than the tangent to the old portion of the curve at the same point. In the operation of the construction shown in Fig. 1, when the piston k reaches the position X the pressure in the primary chamber a, which is substantially equal to that in the secondary chamber b, lifts the spring-pressed valve v so that further movement of the piston compresses the air in both chambers, the rate of increase of pressure being less than that occurring during movement of the piston to position X. On the return movement shock is prevented by a rubber pad g or by a cushion of compressed air formed during the forward stroke of the piston by the passage of air through small piston-perforations h. The valve v may be replaced by a flap-valve controlled by air or spring pressure or by a rod projecting from the piston. In the construction shown in Fig. 2, the rod m of a slide-valve connected to the hollow piston k, is slotted at its lower end and in the position shown its upper end closes two sets of apertures f, q, in secondary chambers b, c. When the piston reaches the position X the pressures of the air in the chambers a, b are substantially equal and when the slots z uncover the apertures f further movement of the piston compresses the air in both chambers. When the piston reaches the position Y the pressure in the chamber c is substantially equal to that in the chambers a, b and after the slots z uncover the apertures q, the piston compresses the air in all three chambers. In a modification, the chamber a is first put into communication with the chamber b and afterwards the chamber b into communication with the chamber c. In another construction the hollow piston k, Fig. 3, has apertures i in its upper and lower surfaces so that when the piston enters the chamber a the air therein is compressed due to the volume taken up by the piston-rod u. When the lower surface of the piston reaches the position O it uncovers apertures f in the secondary chamber b and further movement of the piston compresses the air in both chambers. In a modification of the construction shown in Fig. 1, the secondary chamber b is connected to the primary chamber a by a flexible pipe, and the spring pressing the valve v is replaced by compressed air. A number of such shock-absorbers for use, for example, on an aeroplane, may be connected by flexible pipes to a common secondary chamber, in which case the rate of increase of pressure for a single shock-absorber is less than the rate of the shock absorbers acting together. Each shock-absorber may have its own secondary chamber and these chambers may all be in communication or may communicate in groups. The drawings include a diagram showing the variation in the rate of increase in pressure with movement of the pistons in the constructions described. The Specification as open to inspection under Sect. 91 comprises also other constructions. In Fig. 4 (Cancelled), the secondary chamber b is formed inside the hollow pistonrod u by means of a movable partition u<1>, and the piston k is apertured for the passage of a slide valve rod m fixed to the cylinder. When the piston reaches the position X its lower edge uncovers orifices z in the rod m and the chambers a, b are placed in communication. Fig. 5 (Cancelled), shows a second piston k<1> separating the chambers a, b so that when the pressures in the two chambers are equal further increase in pressure moves the piston kl. In a modification the chambers a, b are formed in telescoping cylinders. This subject-matter does not appear in the Specification as accepted.
GB31634/33A 1932-11-12 1933-11-13 Improvements in and relating to shock-absorbers Expired GB430337A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE430337X 1932-11-12

Publications (1)

Publication Number Publication Date
GB430337A true GB430337A (en) 1935-06-13

Family

ID=6479745

Family Applications (1)

Application Number Title Priority Date Filing Date
GB31634/33A Expired GB430337A (en) 1932-11-12 1933-11-13 Improvements in and relating to shock-absorbers

Country Status (1)

Country Link
GB (1) GB430337A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2445139A (en) * 1941-11-03 1948-07-13 Gret Charles Albert Shock absorbing device for aircraft and other power-driven vehicles
US2756989A (en) * 1952-08-29 1956-07-31 Renault Suspension device for vehicles
US2818142A (en) * 1954-03-18 1957-12-31 Christian Marie Lucien Louis B Shock absorber reservoir valves
FR2467719A1 (en) * 1979-10-17 1981-04-30 Perlini Roberto FLUID SUSPENSION ASSEMBLY, IN PARTICULAR FOR MOTOR VEHICLES
EP1574427A1 (en) * 2004-03-12 2005-09-14 Messier-Dowty S.A. Gas tank type landing gear and its maintenance methods

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2445139A (en) * 1941-11-03 1948-07-13 Gret Charles Albert Shock absorbing device for aircraft and other power-driven vehicles
US2756989A (en) * 1952-08-29 1956-07-31 Renault Suspension device for vehicles
US2818142A (en) * 1954-03-18 1957-12-31 Christian Marie Lucien Louis B Shock absorber reservoir valves
FR2467719A1 (en) * 1979-10-17 1981-04-30 Perlini Roberto FLUID SUSPENSION ASSEMBLY, IN PARTICULAR FOR MOTOR VEHICLES
US4915364A (en) * 1979-10-17 1990-04-10 Roberto Perlini Fluid suspension unit, particularly for heavy motor vehicles
EP1574427A1 (en) * 2004-03-12 2005-09-14 Messier-Dowty S.A. Gas tank type landing gear and its maintenance methods
FR2867451A1 (en) * 2004-03-12 2005-09-16 Messier Dowty Sa GAS RESERVOIR BURNER AND METHODS OF MAINTAINING SUCH A REALIZER
US7204456B2 (en) 2004-03-12 2007-04-17 Messier-Dowty Sa Landing gear having a gas vessel, and methods of maintaining such landing gear

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