EP0066734A1 - Dispositif de chasse à air comprimé pour tubes d'éjection et de décharge de bateau sous-marin - Google Patents

Dispositif de chasse à air comprimé pour tubes d'éjection et de décharge de bateau sous-marin Download PDF

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Publication number
EP0066734A1
EP0066734A1 EP82104281A EP82104281A EP0066734A1 EP 0066734 A1 EP0066734 A1 EP 0066734A1 EP 82104281 A EP82104281 A EP 82104281A EP 82104281 A EP82104281 A EP 82104281A EP 0066734 A1 EP0066734 A1 EP 0066734A1
Authority
EP
European Patent Office
Prior art keywords
blow
valve
compressed gas
opening
gas container
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.)
Granted
Application number
EP82104281A
Other languages
German (de)
English (en)
Other versions
EP0066734B1 (fr
Inventor
Richard Woidich
Josef Schmitt
Peter Hartz
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.)
Caterpillar Motoren GmbH and Co KG
Original Assignee
Krupp Mak Maschinenbau 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 Krupp Mak Maschinenbau GmbH filed Critical Krupp Mak Maschinenbau GmbH
Publication of EP0066734A1 publication Critical patent/EP0066734A1/fr
Application granted granted Critical
Publication of EP0066734B1 publication Critical patent/EP0066734B1/fr
Expired legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/08—Rocket or torpedo launchers for marine torpedoes
    • F41F3/10—Rocket or torpedo launchers for marine torpedoes from below the surface of the water

Definitions

  • the invention relates to a blow-out device for ejection and drain pipes of submarines for ejecting weapons by means of compressed gas which can be supplied from the associated compressed gas containers and controlled via a circuit arrangement.
  • blow-out devices consist of voluminous pressure bottles which are arranged outside the torpedo tube and are provided with corresponding connecting lines. It is also known to press water into the torpedo tube in large quantities and at high pressure. These arrangements are too complex for many areas of application and, above all, have the defect that it is difficult to retrofit them in existing systems.
  • the object of the invention is to provide a device of the generic type, which also ensures retrofitting in existing systems and enables in a simple manner to reduce the initial pressure surge and prevents water from entering the blow-out device after the blow-out process has ended.
  • the pressurized gas container is arranged in the bottom region of the discharge and drain pipe and one with a rear on the side assigned to the weapon has impact valve provided outlet opening which is connected to a buffer tube penetrating the compressed gas container, which has passage openings leading to the interior of the compressed gas container at the end region opposite the check valve and an outlet opening is formed which can be controlled via an outlet valve.
  • Flawless operation is advantageously achieved in that the closing force of the check valve corresponds to a pressure difference of at least 0.5 bar.
  • a favorable arrangement is achieved in that the compressed gas container forms a unit with the control arrangement.
  • the opening stroke of the blow-off valve be designed to be adjustable via a linkage.
  • the blow-out valve be coupled to a control piston arrangement which can be acted upon on both sides and that the cylinder spaces formed are connected to one another via a throttle device with an adjustable cross section.
  • the firing valve be connected to the buffer tube by a control line to maintain the firing position. This effectively locks the fire position achieved.
  • blow-off valve with its shut-off cone protrude into the blow-out opening in such a way that a minimal part of the opening cross-section of the blow-out opening is released in the first part of the opening path.
  • the torpedo tube 1 shown is provided with a bottom cover 2 and receives a blow-out device 3.
  • the blow-out device 3 is formed by a compressed gas container 3.0 and an instrument part 3.1 for the control arrangement, which are introduced as a unit in the torpedo tube 1.
  • the pressure gas container 3.0 is provided on the side facing the weapon with an outlet opening 3.16 and is controlled by a check valve 3.4 with a pressure spring 3.5.
  • the opening 3.16 is connected to a buffer tube 3.3 which is guided through the compressed gas container 3.0.
  • through-openings 5.2 to the interior of the compressed gas container 3.0 are arranged and the actual blow-out opening 3.17 to the buffer tube 3.3 is controlled by a blow-out valve 3.2.
  • the check valve 3.4 is acted upon by the pressure spring 3.5 in the closing direction, so that at least a pressure difference of 0.5 bar is formed.
  • the two sides of the piston of the control piston arrangement 3.7 are connected to one another by a cylinder 3.10 via lines 3.11, the flow cross-section and thus the opening speed being changeable in dependence on the depth by means of an adjustable throttle device 3.12.
  • This adjustment device is adjustable from the inside of the boat via an operating spindle 3.13 through the closed bottom cover 2.
  • this side is a low pressure accumulator. 3.14 assigned.
  • the adjustment can also be controlled automatically by the depth of the water pressure.
  • the actual blow-out process to eject the weapon is triggered by a firing valve 4, which in this case is controlled electrically.
  • This firing valve 4 is locked in the firing position after initiation of the firing process by the pressure in the buffer tube 3.3 being applied to the control side 4.2 of the firing valve 4 via a connecting line 4.1.
  • the blow-off valve 3.2 is enclosed, for example, by an annular gate valve 5 and is normally positioned so that its radial bores 5.1 are aligned with the associated bores 5.2 of the valve housing.
  • a switching valve 5.4 is actuated via a line 5.3, which switches the gate valve 5 on one side via the vent line 5.5 relieved, so that it is moved into a blocking position in which the passage through the bores 5.2 to the blow-off valve 3.2 is blocked.
  • the switching valve 5.4 is locked in the venting position or the gate valve remains in the blocking position until the pressure in the buffer tube 3.3 has dropped. It is of course also possible to lock the gate valve 5 in the closed position.
  • the instrument part 3.1 forms a structural and functional unit with the compressed gas container 3.0, with the connecting lines to the inside of the boat, namely a ventilation line 6 and an electrical one Supply line 7 and adjustment devices 3.9 and 3.13 are easily detachable in the bottom cover 2 of the torpedo tube.
  • the device becomes particularly easy to handle and failsafe if the operating and supply elements are not guided through the bottom cover 2 but through the wall of the torpedo tube 1, as shown in FIG. 2.
  • the depth-dependent stroke limitation of the blow-out valve 3.2 via the piston rod 3.6 is represented by an eccentric disk 3.15, the position of which can be changed using the actuating spindle 3.9.
  • vent and blow-out bores arranged on the encapsulated control arrangement 3.1 on the firing valve 4, the switching valve 5.4 for the gate valve 5 and the switching valve 8 of the compressed gas container 3.0 are combined to form a common vent line 6.1, which leads into the connecting line 6 to the inside of the boat.
  • This measure prevents that inevitable moisture, which can escape from the valves mentioned, collects in the control arrangement 3.1 and there leads to malfunctions in the electrical components.
  • the line 6.1 also reduces any excess pressure that may have arisen in the encapsulated control arrangement 3.1.
  • an additional line is connected via a check valve 6.2, the check valve 6.2 being installed in such a way that only the direction of flow from the instrument part into line 6.1 is released.
  • a locking device for the blow-out valve 3.2 is shown, which prevents unintentional actuation of the filled blow-out device during transport or in the torpedo tube 1.
  • the piston rod 3.6 is given a cylindrical extension 21, the end 22 of which is offset in half over a length corresponding to the valve stroke.
  • a corresponding spindle 23 can be rotated in the control arrangement 3.1, but is axially immovable. Both parts 21, 23 are aligned so that the stepped ends 22 and 24 face each other in the blocking position with a minimal distance, but after the spindle 23 has rotated through 180 ° in the release position, an unimpeded opening of the blow-off valve 3.2 is allowed.
  • the lock can be operated through the bottom cover 2 with the help of an extension spindle 26 even when the torpedo tube 1 is flooded.

Landscapes

  • Engineering & Computer Science (AREA)
  • Ocean & Marine Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)
EP82104281A 1981-06-06 1982-05-15 Dispositif de chasse à air comprimé pour tubes d'éjection et de décharge de bateau sous-marin Expired EP0066734B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19813122631 DE3122631A1 (de) 1981-06-06 1981-06-06 "ausblas-einrichtung fuer ausstoss- und ablaufrohre von u-booten"
DE3122631 1981-06-06

Publications (2)

Publication Number Publication Date
EP0066734A1 true EP0066734A1 (fr) 1982-12-15
EP0066734B1 EP0066734B1 (fr) 1984-10-03

Family

ID=6134148

Family Applications (1)

Application Number Title Priority Date Filing Date
EP82104281A Expired EP0066734B1 (fr) 1981-06-06 1982-05-15 Dispositif de chasse à air comprimé pour tubes d'éjection et de décharge de bateau sous-marin

Country Status (3)

Country Link
US (1) US5123370A (fr)
EP (1) EP0066734B1 (fr)
DE (2) DE3122631A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0360370A2 (fr) * 1988-09-21 1990-03-28 Howaldtswerke-Deutsche Werft Ag Mécanisme à vanne de lancement, contrôlé par la profondeur d'immersion

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3322020C2 (de) * 1983-06-18 1986-05-28 Krupp Mak Maschinenbau Gmbh, 2300 Kiel Ausblaseinrichtung für Ausstoß- und Ablaufrohre von U-Booten
DE10305778A1 (de) * 2003-02-12 2004-08-26 Howaldtswerke-Deutsche Werft Ag Unterseeboot
US6796260B1 (en) 2003-09-08 2004-09-28 The United States Of America As Represented By The Secretary Of The Navy Elastomeric ejection system with acoustically improved check valve
KR100923381B1 (ko) 2007-08-28 2009-10-23 대우조선해양 주식회사 잠수함의 구조물 일체형 조종블록 장치
DE102014217747A1 (de) 2014-09-04 2016-03-10 Thyssenkrupp Marine Systems Gmbh Unterseeboot

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2099249A5 (fr) * 1970-06-18 1972-03-10 Faun Werke Kommunalfahrz
US4185538A (en) * 1960-08-30 1980-01-29 The United States Of America As Represented By The Secretary Of The Navy Simplified air system for underwater rocket launching

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US430101A (en) * 1890-06-10 Method of regulating firing-fluid delivery to pneumatic guns
US2043203A (en) * 1929-07-31 1936-06-02 Crane Co Full area safety valve
US2514747A (en) * 1945-01-15 1950-07-11 Daniels Oscar Fluid pressure operated apparatus
DE1147866B (de) * 1961-01-18 1963-04-25 Pintsch Bamag Ag Ausstossrohr fuer Torpedos, Minen u. dgl.
US3087386A (en) * 1961-03-23 1963-04-30 Robert D Rung Adapter for missile launcher
US3971405A (en) * 1974-07-15 1976-07-27 Parker-Hannifin Corporation Pressure controlled hydrant valve coupler

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4185538A (en) * 1960-08-30 1980-01-29 The United States Of America As Represented By The Secretary Of The Navy Simplified air system for underwater rocket launching
FR2099249A5 (fr) * 1970-06-18 1972-03-10 Faun Werke Kommunalfahrz

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0360370A2 (fr) * 1988-09-21 1990-03-28 Howaldtswerke-Deutsche Werft Ag Mécanisme à vanne de lancement, contrôlé par la profondeur d'immersion
EP0360370A3 (fr) * 1988-09-21 1992-10-07 Howaldtswerke-Deutsche Werft Ag Mécanisme à vanne de lancement, contrôlé par la profondeur d'immersion

Also Published As

Publication number Publication date
DE3122631A1 (de) 1982-12-23
DE3260878D1 (en) 1984-11-08
US5123370A (en) 1992-06-23
EP0066734B1 (fr) 1984-10-03

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