EP0309646A2 - Equilibreur - Google Patents

Equilibreur Download PDF

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Publication number
EP0309646A2
EP0309646A2 EP88107280A EP88107280A EP0309646A2 EP 0309646 A2 EP0309646 A2 EP 0309646A2 EP 88107280 A EP88107280 A EP 88107280A EP 88107280 A EP88107280 A EP 88107280A EP 0309646 A2 EP0309646 A2 EP 0309646A2
Authority
EP
European Patent Office
Prior art keywords
gas
temperature
pressure
pressure regulator
cylinder chamber
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.)
Withdrawn
Application number
EP88107280A
Other languages
German (de)
English (en)
Other versions
EP0309646A3 (fr
Inventor
Georg Sauer
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.)
Rheinmetall Industrie AG
Original Assignee
Rheinmetall GmbH
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 Rheinmetall GmbH filed Critical Rheinmetall GmbH
Publication of EP0309646A2 publication Critical patent/EP0309646A2/fr
Publication of EP0309646A3 publication Critical patent/EP0309646A3/fr
Withdrawn legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A27/00Gun mountings permitting traversing or elevating movement, e.g. gun carriages
    • F41A27/30Stabilisation or compensation systems, e.g. compensating for barrel weight or wind force on the barrel

Definitions

  • the invention relates to a pneumatic balancer for guns with a balancer cylinder, the cylinder space takes out an extendable control rod and is filled with a gas.
  • Such compensators for example known from the "Weapons-technical paperback" Rheinmetall, 6th edition 1983 page 356, picture 890, are used in guns to cancel the front load of the height adjustment part as possible, so that the focus of the height adjustment part lies in the height adjustment axis, the shield pin axis.
  • the balancer is placed between the top mount and the cradle of the gun.
  • the front load creates a torque equal to the weight multiplied by its distance from the gun's trunnion axis. This is countered by a compensating torque equal to the compensating force multiplied by its distance from the shield pin axis of the same size, so that easy and uniform straightening is possible.
  • Pneumatic compensators have the disadvantage that they are sensitive to temperature. In order to achieve a better temperature adjustment, it is known to change the equalizer volume. This is done by moving the rear suspension point of the compensating cylinder. This displacement is carried out by a spindle which moves the rear articulation point along a straight line inclined at a small angle to the vertical. However, this temperature adjustment is not satisfactory. In particular at low temperatures there is a considerable deterioration in the moment compensation, while an improvement is only evident at temperatures above approximately + 20 ° C.
  • the object of the invention is therefore to provide a compensator of the type mentioned which is practically independent of temperature.
  • This object is achieved in that the cylinder space is connected to a device which compensates for the temperature-related pressure change of the gas in the cylinder space.
  • the temperature-related change in pressure is compensated according to the invention, ie gas is added or removed in accordance with the change in temperature, so that the compensator behaves in the same way as it does for p o and T o (normal temperature). In this way you get a moment compensation over the entire temperature range.
  • the compensator shown has a compensating cylinder 1 which has a cylinder space 2 filled with a gas, in particular nitrogen, which has a constriction 3 in the central region.
  • a regulating rod 4 projects into the compensating cylinder 1 to the area of the constriction 3 while leaving a narrow gap 5.
  • the control rod 4 has a gas space 6 that is open to the cylinder space 2.
  • a bellows 7 is used to protect the part of the control rod 4 that protrudes from the cylinder 1 is provided, which is used to fill the compensator with gas.
  • a pressure regulator 9 which is connected to a gas source 10 and has a gas return line 11 returning to the gas source 10, is also connected to the gas supply connection 8.
  • the pressure regulator 9 supplies gas from the gas source 10 to the pressure compensation due to the pressure drop determined by the pressure regulator 9 of the cylinder chamber pressure present thereon, while it ensures that the gas to be discharged for pressure compensation is removed when the temperature rises above T o .
  • the gas to be discharged is fed back to the gas source 10 without loss via a feed pump 12 connected to the gas return line 11.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Fluid Pressure (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Actuator (AREA)
  • Fluid-Damping Devices (AREA)
EP19880107280 1987-09-29 1988-05-06 Equilibreur Withdrawn EP0309646A3 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19873732745 DE3732745A1 (de) 1987-09-29 1987-09-29 Ausgleicher
DE3732745 1987-09-29

Publications (2)

Publication Number Publication Date
EP0309646A2 true EP0309646A2 (fr) 1989-04-05
EP0309646A3 EP0309646A3 (fr) 1990-09-12

Family

ID=6337105

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19880107280 Withdrawn EP0309646A3 (fr) 1987-09-29 1988-05-06 Equilibreur

Country Status (2)

Country Link
EP (1) EP0309646A3 (fr)
DE (1) DE3732745A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0687887A1 (fr) * 1994-06-16 1995-12-20 Giat Industries Dispositif d'équilibrage d'un canon
EP0702202A1 (fr) 1994-09-19 1996-03-20 Giat Industries Dispositif de réglage en fonction de la température extérieure d'un système d'équilibrage d'une pièce d'artillerie
CN116818791A (zh) * 2023-06-20 2023-09-29 成都飞机工业(集团)有限责任公司 一种飞机配电转换组件缺陷检测装置

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4100102A1 (de) * 1991-01-04 1992-07-09 Wegmann & Co Unbalance-ausgleichsvorrichtung fuer eine waffe, insbesondere eine grosskalibrige waffe mit langem rohr

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3033085A (en) * 1959-01-28 1962-05-08 Donald E Witkin Temperature compensating system for hydropneumatic equilibrator
US3017170A (en) * 1959-03-27 1962-01-16 Cleveland Pneumatic Ind Inc Temperature compensated liquid spring

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0687887A1 (fr) * 1994-06-16 1995-12-20 Giat Industries Dispositif d'équilibrage d'un canon
FR2721393A1 (fr) * 1994-06-16 1995-12-22 Giat Ind Sa Dispositif d'équilibrage d'un canon.
US5614690A (en) * 1994-06-16 1997-03-25 Giat Industries Equilibrating device for a gun
EP0702202A1 (fr) 1994-09-19 1996-03-20 Giat Industries Dispositif de réglage en fonction de la température extérieure d'un système d'équilibrage d'une pièce d'artillerie
FR2724715A1 (fr) * 1994-09-19 1996-03-22 Giat Ind Sa Dispositif de reglage en fonction de la temperature exterieure d'un systeme d'equilibrage d'une piece d'artillerie
US5663521A (en) * 1994-09-19 1997-09-02 Giat Industries Method and apparatus for controlling an equilibrating system subject to varying temperatures and laying angles
CN116818791A (zh) * 2023-06-20 2023-09-29 成都飞机工业(集团)有限责任公司 一种飞机配电转换组件缺陷检测装置

Also Published As

Publication number Publication date
DE3732745A1 (de) 1989-04-06
EP0309646A3 (fr) 1990-09-12

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