EP2265885B1 - Dispositif de stabilisation - Google Patents
Dispositif de stabilisation Download PDFInfo
- Publication number
- EP2265885B1 EP2265885B1 EP09731196A EP09731196A EP2265885B1 EP 2265885 B1 EP2265885 B1 EP 2265885B1 EP 09731196 A EP09731196 A EP 09731196A EP 09731196 A EP09731196 A EP 09731196A EP 2265885 B1 EP2265885 B1 EP 2265885B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- damper
- piece
- pressure
- stabilizing device
- damping system
- 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.)
- Not-in-force
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A25/00—Gun mountings permitting recoil or return to battery, e.g. gun cradles; Barrel buffers or brakes
- F41A25/10—Spring-operated systems
- F41A25/12—Spring-operated systems using coil springs
Definitions
- the invention relates to a device for stabilizing a thrower, in particular during the firing of camouflage and decoys, or other systems that can rock and in particular a launcher who can fulfill their task in terms of accuracy and accuracy only limited.
- a radar device for the object protection with a launching container is known.
- Such launchers or launchers are subject to the problem of rocking at least during use.
- the stabilization of launchers during the service load taking into account the shock performance is a technical problem.
- Many launchers and associated control cabinets are damped with metal cable dampers or the like.
- these measures are often not sufficient to prevent a build-up, for example, by shooting sequences.
- dampers are offered, for example, by Socitec et al. Under the product lines Polycal, Half-Helical or Helical ( http://www.socitec.fr/ )
- a further stabilization device for a particular launcher is known, which is characterized in that in addition to a known damper system, for example, to a metal cable damper, etc., a stabilization is provided which is held together at least with a shear pin. After shock, the bolt shears off and the damper system can absorb the shock.
- the stabilization or the associated construction is capable of doing so in all Directions to be freely movable, so that despite shear pin, no parts flying around, the structure remains intact in their function and only the bolt is retrofitted.
- the solution allows in a particular embodiment, a fixation of the launcher at operating load (launch, movement), the provision of the damping path in the event of shock to avoid overloading the system and a restoration of the stiff state after shock with simple means.
- the invention takes on the task to show a further simple constructive way that counteracts a rocking of the working load.
- the invention is based on the idea to provide a re-adjustable stabilization, with which the release force can be customized.
- the device or the system, which can be mounted on the stabilization are automatically returned to their original position after a mine shock or the like, a message or replacement of parts can be omitted.
- Starting construction is a built-in between two strips or the like damper, for example, a metal cable damper, with incorporated at the starting points ball joints, preferably two, which ensure a free angular mobility of the construction in a known manner.
- ball joints preferably two, which ensure a free angular mobility of the construction in a known manner.
- two preferably telescoping tubes are integrated at these ball joints in a simple embodiment. These tubes are in principle adjustable. In the preferred embodiment, two telescoping pairs of tubes are used.
- this stabilization device here in the pipe pairs.
- This system consists primarily of a cam, a plate spring package or other biased device with which a pressure on the piece and a kind of pawl piece a pressure on the cam can be exercised. With an axial force, this can act in both directions, the force is introduced via the cam bevel on the pawl piece and the pressure piece in the plate spring package.
- the system itself only moves when the preload of the damper springs is exceeded.
- the pawl moves perpendicular to the axial force and releases the cam. This allows an equipped so equipped wire rope damper to move freely after triggering and to be able to record, for example, 45mm in all directions.
- the system goes into a state of vibration and the pawl piece goes through the curve in the cam several times. As long as the kinetic energy is sufficiently large, the system will continue to oscillate. If the kinetic energy falls below a limit, the pawl piece finally engages again and fixes the system in the original position.
- the mobility of the system itself in all directions is ensured by the ball joints.
- Another major advantage of this simple solution is that it can be retrofitted on existing systems or projector systems.
- the overall design can also be applied to cabinets or other devices that have damping systems of this type in a similar manner and can be upgraded or retrofitted with the stabilization.
- Fig. 1 is a metal cable damper 1 shown as an example, which is used for example for vibration damping of a projector not shown here.
- This damper or damping system 1 consists in this embodiment of two interconnected metal springs 2 struts or strips 3. Between the strips 3 and the metal springs 2 is integrated a stabilization device 4, which in the starting points for connection to the damper 1 two ball joints 5.1 , 5.2, 6.1, 6.2, over which a free angular mobility of the device 4 is ensured.
- At these ball joints 5.1, 5.2 and 6.1, 6.2 are preferably two mutually running or adjustable tubes 7.1, 7.2, and 8.1, 8.2 fixed ( Fig. 2, 2a ).
- a re-adjustable adjustable device or a re-adjustable adjustable system 10 is involved.
- This system 10 consists primarily of a cam 11, a plate spring package 12 or other biased device with which a pressure on the piece 13 and a kind of pawl piece 14 a pressure on the cam bar 11 can be exercised ( Fig. 3 ).
- the bias of the device can be made by an adjustment screw 16.
- the system 10 itself moves only from exceeding the bias of the springs of the damper 1.
- the pawl 14 moves perpendicular to the axial force and releases the cam bar 11.
- the system 10 goes into a state of vibration and the pawl 14 passes several times through the curve 15 in the cam bar 11. If the kinetic energy falls below a limit, the pawl 14 finally locks again and fixes the system (not shown) in the original position.
Landscapes
- General Engineering & Computer Science (AREA)
- Engineering & Computer Science (AREA)
- Vibration Dampers (AREA)
- Vibration Prevention Devices (AREA)
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
- Paper (AREA)
- Polarising Elements (AREA)
- Disintegrating Or Milling (AREA)
- Joints Allowing Movement (AREA)
- Power-Operated Mechanisms For Wings (AREA)
- Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)
- Catching Or Destruction (AREA)
- Lift-Guide Devices, And Elevator Ropes And Cables (AREA)
- Surgical Instruments (AREA)
- Vehicle Body Suspensions (AREA)
Claims (4)
- Dispositif de stabilisation (4) pour un lanceur ou d'autres installations, qui sont soumises à des chocs et sont pourvues d'un système d'amortissement (1), le dispositif de stabilisation (4) présentant en au moins deux points d'application sur le système d'amortissement (1) une articulation sphérique respective (5.1, 5.2 ; 6.1, 6.2), entre lesquelles sont intégrés au moins deux tubes glissant l'un dans l'autre (7.1, 7.2 ; 8.1, 8.2), caractérisé en ce que dans les tubes (7.1, 7.2 ; 8.1, 8.2) est placé un système (10) ramenant dans sa position d'origine le lanceur ou les autres installations, le système étant constitué d'une barre courbe (11), d'un dispositif précontraint (12), d'une pièce de pression (13) et d'une pièce de cliquet (14), une pression pouvant être exercée sur la barre courbe (11) au moyen du dispositif précontraint (12), par le biais de la pièce de pression (13) et par le biais de la pièce de cliquet (14).
- Dispositif de stabilisation selon la revendication 1, caractérisé en ce que le système d'amortissement (1) se compose de deux lattes (3) qui sont connectées fonctionnellement l'une à l'autre par le biais de ressorts métalliques (2).
- Dispositif de stabilisation selon la revendication 2, caractérisé en ce qu'il se déplace de lui-même à partir du dépassement de la précontrainte des ressorts métalliques (2) du système d'amortissement (1).
- Dispositif de stabilisation selon l'une quelconque des revendications 1 à 3, caractérisé en ce que la précontrainte peut être exercée au moyen d'une vis d'ajustage (16).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102008017926A DE102008017926B3 (de) | 2008-04-08 | 2008-04-08 | Stabilisierungsvorrichtung |
PCT/EP2009/001976 WO2009124641A1 (fr) | 2008-04-08 | 2009-03-18 | Dispositif de stabilisation |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2265885A1 EP2265885A1 (fr) | 2010-12-29 |
EP2265885B1 true EP2265885B1 (fr) | 2012-02-22 |
Family
ID=40530855
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP09731196A Not-in-force EP2265885B1 (fr) | 2008-04-08 | 2009-03-18 | Dispositif de stabilisation |
Country Status (12)
Country | Link |
---|---|
US (1) | US8864118B2 (fr) |
EP (1) | EP2265885B1 (fr) |
KR (1) | KR101582702B1 (fr) |
AT (1) | ATE546707T1 (fr) |
AU (1) | AU2009235789B2 (fr) |
BR (1) | BRPI0911237A2 (fr) |
CA (1) | CA2719233C (fr) |
DE (1) | DE102008017926B3 (fr) |
IL (1) | IL208501A (fr) |
RU (3) | RU2010145137A (fr) |
WO (1) | WO2009124641A1 (fr) |
ZA (1) | ZA201006735B (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012217189A1 (de) * | 2012-09-24 | 2014-03-27 | Siemens Aktiengesellschaft | Dämpfungsanordnung einer schwingfähig gelagerten Elektroenergieübertragungseinrichtung |
EP2889877B1 (fr) * | 2013-12-06 | 2021-03-10 | ITT Manufacturing Enterprises LLC | Ensemble d'isolation sismique |
DE102014014065B4 (de) | 2014-09-29 | 2016-08-04 | Rheinmetall Air Defence Ag | Schocklagerungsanordnung für potentiell Schockeinwirkung ausgesetzten Geräten in militärischen Anwendungen |
DE102018128954A1 (de) | 2018-11-19 | 2020-05-20 | Rheinmetall Waffe Munition Gmbh | Stabilisierungsvorrichtung, Fahrzeug und Verfahren zum Betrieb einer Stabilisierungseinrichtung |
DE102018128956A1 (de) | 2018-11-19 | 2020-05-20 | Rheinmetall Waffe Munition Gmbh | Aufnahmevorrichtung, Fahrzeug und Verfahren zum Betrieb einer Aufnahmevorrichtung |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2989968A (en) * | 1957-12-06 | 1961-06-27 | Kortenbach & Rauh Kg | Umbrella stick |
US4385849A (en) * | 1981-02-02 | 1983-05-31 | Crain Enterprises, Inc. | Extensible and retractable rod |
US5386897A (en) * | 1993-05-27 | 1995-02-07 | Yang; Tai-Her | Delay restoring type limit-torque coupling mechanism |
US6325188B1 (en) * | 1999-08-24 | 2001-12-04 | Chin-Long Wu | Linear motion damping device |
DE10024320C2 (de) * | 2000-05-17 | 2002-09-05 | Diehl Munitionssysteme Gmbh | Radareinrichtung für den Objekt-Selbstschutz |
US6854916B2 (en) * | 2002-05-17 | 2005-02-15 | David Hsieh | Retractable rod assembly |
DE202005011008U1 (de) * | 2005-07-13 | 2005-11-24 | Rheinmetall Waffe Munition Gmbh | Stabilisierungsvorrichtung |
DE102006009371A1 (de) * | 2006-03-01 | 2007-09-06 | Hoppe Ag | Rastmittel und Verwendung bei Betätigungshandhaben |
-
2008
- 2008-04-08 DE DE102008017926A patent/DE102008017926B3/de not_active Expired - Fee Related
-
2009
- 2009-03-18 EP EP09731196A patent/EP2265885B1/fr not_active Not-in-force
- 2009-03-18 AU AU2009235789A patent/AU2009235789B2/en not_active Ceased
- 2009-03-18 KR KR1020107022058A patent/KR101582702B1/ko not_active IP Right Cessation
- 2009-03-18 RU RU2010145137/11A patent/RU2010145137A/ru unknown
- 2009-03-18 WO PCT/EP2009/001976 patent/WO2009124641A1/fr active Application Filing
- 2009-03-18 CA CA2719233A patent/CA2719233C/fr not_active Expired - Fee Related
- 2009-03-18 RU RU2014133416/11U patent/RU150996U1/ru not_active IP Right Cessation
- 2009-03-18 AT AT09731196T patent/ATE546707T1/de active
- 2009-03-18 US US12/936,847 patent/US8864118B2/en not_active Expired - Fee Related
- 2009-03-18 BR BRPI0911237A patent/BRPI0911237A2/pt not_active IP Right Cessation
-
2010
- 2010-09-20 ZA ZA2010/06735A patent/ZA201006735B/en unknown
- 2010-10-05 IL IL208501A patent/IL208501A/en not_active IP Right Cessation
-
2014
- 2014-08-13 RU RU2014133424A patent/RU2014133424A/ru not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
IL208501A (en) | 2014-07-31 |
ATE546707T1 (de) | 2012-03-15 |
CA2719233C (fr) | 2016-05-31 |
IL208501A0 (en) | 2010-12-30 |
AU2009235789B2 (en) | 2014-05-22 |
US20110094488A1 (en) | 2011-04-28 |
DE102008017926B3 (de) | 2009-05-14 |
KR20110000651A (ko) | 2011-01-04 |
RU2010145137A (ru) | 2012-05-20 |
EP2265885A1 (fr) | 2010-12-29 |
BRPI0911237A2 (pt) | 2018-01-09 |
US8864118B2 (en) | 2014-10-21 |
WO2009124641A1 (fr) | 2009-10-15 |
ZA201006735B (en) | 2011-05-25 |
CA2719233A1 (fr) | 2009-10-15 |
RU150996U1 (ru) | 2015-03-10 |
RU2014133424A (ru) | 2016-03-10 |
AU2009235789A1 (en) | 2009-10-15 |
KR101582702B1 (ko) | 2016-01-05 |
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