EP2438388A1 - Systeme de protection deployable - Google Patents
Systeme de protection deployableInfo
- Publication number
- EP2438388A1 EP2438388A1 EP10724739A EP10724739A EP2438388A1 EP 2438388 A1 EP2438388 A1 EP 2438388A1 EP 10724739 A EP10724739 A EP 10724739A EP 10724739 A EP10724739 A EP 10724739A EP 2438388 A1 EP2438388 A1 EP 2438388A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- rigid
- rigid tubes
- tube
- protection system
- tubes
- 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
Links
- 239000004744 fabric Substances 0.000 claims description 29
- 238000010304 firing Methods 0.000 claims description 3
- 238000007789 sealing Methods 0.000 claims 1
- 230000001681 protective effect Effects 0.000 description 10
- 239000007789 gas Substances 0.000 description 7
- 239000002775 capsule Substances 0.000 description 3
- 238000006073 displacement reaction Methods 0.000 description 2
- 230000036961 partial effect Effects 0.000 description 2
- 229920000271 Kevlar® Polymers 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 239000004761 kevlar Substances 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H13/00—Means of attack or defence not otherwise provided for
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H13/00—Means of attack or defence not otherwise provided for
- F41H13/0006—Ballistically deployed systems for restraining persons or animals, e.g. ballistically deployed nets
Definitions
- the present invention relates to a deployable protection system that can be used in particular in a framework for the protection of warships.
- the invention proposes a protection system characterized in that it comprises a frame that can be disassembled around a central tube of the armature, with a pin longitudinal XX ', having two ends, a covering fabric of the frame, the frame comprising:
- a semi-rigid tube per pair of rigid tubes in said axial plane of the pair, comprising at each of its ends a piston, each piston of a semi-rigid tube being able to slide in a sealed manner in the one and in the other rigid tubes of the pair to form a pressurizing chamber in each of the rigid tubes, the protection system further comprising a device for pressurizing the chambers of the rigid tubes to move the pistons in the rigid tubes and move the system from a folded position to a deployed position.
- the rigid tubes have a degree of freedom in rotation about an axis of articulation YY 'with its respective articulation clevis perpendicular to its respective axial plane passing through the axis XX' of the central tube.
- the articulated ends of the rigid tubes are closed to form, with the piston of the semi-rigid tube, the pressurizing chamber in each of the rigid tubes.
- the rigid tube comprises, on the side of its free end, an abutment integral with the rigid tube in the form of an O-ring surrounding the semi-rigid tube.
- each of the rigid tubes comprises an intermediate guide for guiding a portion of the end of the semi-rigid tube as it moves in the rigid tube.
- the central tube has thrust stops disposed on its periphery so that, the system being in the folded position, the free ends of the rigid tubes bear on these bearing stops to form an angle incidence ⁇ with the central tube.
- the fabric is configured to take an ovoid shape when the system is in the deployed position, the fabric comprising at one and the other ends of the central tube an opening for the passage of the rigid tubes and in that that the edges of the openings of the fabric are secured to the rigid tubes to hold the fabric in place on the frame.
- the system further comprises cables of predetermined lengths attached to both ends of the central tube to give a predetermined shape to the deployed web.
- the main objectives of the invention is to provide a deployable protection system that is simple to implement, reliable and economical.
- FIG. 1 shows a longitudinal sectional view of the deployable protection system according to the invention in a folded position in a protective envelope
- FIGS. 2a and 2b show two partial views in one direction and in the opposite direction along a longitudinal axis of the system of Figure 1 in the deployed position;
- FIG. 3a shows a schematic axial sectional view showing the system according to the invention in the folded position and
- FIG. 3b shows a schematic axial sectional view showing the system according to the invention in the deployed position.
- Figure 1 shows a longitudinal sectional view of the deployable protection system according to the invention in a folded position in a protective envelope.
- Figures 2a and 2b show two partial views in one direction and in the opposite direction along a longitudinal axis of the system of Figure 1 in the deployed position.
- the protection system essentially comprises a frame 2 and a cover fabric 4 configured to give the deployed system the desired shape around a central tube 10 of the frame, of longitudinal axis XX '.
- the system is contained in an outer protection envelope 6 having its own opening device prior to deployment of the protection system.
- the protective envelope 6 is of tubular shape along the axis XX '.
- FIG. 2a shows a view transverse to the axis XX 'according to UU' and FIG. 2b a transverse view to the same axis XX 'according to VV (see FIG. 1).
- the armature of the protection system of FIGS. 1, 2a and 2b according to the invention comprises five pairs P1, P2, P3, P4, P5 of rigid tubes angularly distributed around the central tube 10 (see FIGS. 2a and 2b).
- Each of the rigid tubes of a pair is articulated by one of its ends eA, along an axis YY 'perpendicular to the axis XX', on a clevis secured to one or the other end of the central tube according to the tube rigid considered, clevises 40, 44, 48, 52, 56 of articulation of the rigid tubes 20, 24, 28, 32, 34, 36 on the left end side of the central tube and the yokes 42, 46, 50, 54, 58 of articulation of the rigid tubes 22, 26, 30, 34, 38 of the right end side of the central tube 10.
- the rigid tubes have a degree of freedom in rotation around the hinge axis YY 'on the yoke in the respective axial plane fold, pl2, pl3, pl4, pl5 passing through the axis XX' of the central tube.
- the other free ends of the rigid tubes can therefore move in the respective axial plane fold, pl2, pl3, pl4, pl5 of the pair considered.
- a semi-rigid tube 70, 71, 72, 73, 74 associated with a pair P1, P2, P3, P4, P5 of rigid tubes comprises at each of its ends a piston 75.
- the two pistons 75 of a semi-rigid tube sealingly close the side of the free ends, the rigid tubes facing a pair of rigid tubes at one and the other end of the central tube 10 and in the same axial plane passing through the axis XX '.
- the articulated ends eA rigid tubes, the side of the yokes, are closed to form with the piston 75 in each of the rigid tubes, a sealed chamber 80 to be pressurized.
- the piston 75 is intended to be moved longitudinally in the rigid tube by a pressure in the chamber 80 of the rigid tube.
- the free end of the rigid tube comprises a stop 90 integral with the rigid tube and closing it at this end.
- this stop is in the form of an O-ring surrounding the semi-rigid tube 70, 71, 72, 73, 74.
- Each of the rigid tubes further comprises an intermediate guide.
- the intermediate guide 92 is immobilized in a predetermined position pt in a central part of the rigid tube between the piston 75 and the stopper 90.
- the intermediate guide 92 can be driven in translation in the rigid tube when a force exceeding a certain threshold is exerted by the piston 75 on the intermediate guide 92 along the longitudinal axis of the rigid tube during the deployment of the protection system.
- the central tube 10 has abutment stops 94 on the periphery of the central tube 10 and arranged on the central tube so that the free ends of the rigid tubes bear on these bearing abutments to form said angle of incidence ⁇ .
- the system comprises a device for pressurizing the chambers 80 of the rigid tubes (not shown in the figures) to effect the deployment of its armature 2.
- the rigid tubes are closed, on their articulated ends eA side, by flanges, a right flange 84 on the side of one end of the central tube 10, (the right end in Figure 1) and a flange left 86 side of the other end (the left end in Figure 1) of the central tube.
- the chambers 80 of the rigid tubes are pressurized by pressurizing the flanges 84, 86.
- the device for pressurizing the chambers of the rigid tubes comprises a pyrotechnic gas generator in each of the flanges 84, 86 of the armature.
- each rigid tube is closed independently of the side of its articulated end eA.
- the pressurization of the chambers 80 of the rigid tubes is done independently for each of the rigid tubes.
- the device for pressurizing the chambers of the rigid tubes comprises a pyrotechnic gas generator in each of the chambers 80 of the rigid tubes.
- the system comprises, for example, an electric device for firing the pyrotechnic gas generators.
- the electrical device can be controlled by a computer for detecting the threat and triggering the deployment of the protection system.
- the fabric 4 of the system is configured to take an ovoid shape when the system is deployed (expanded canvas shown in dotted lines in Figures 2a, 2b, 3b).
- the fabric 4 has at each end, on one side and on the other side of the central tube 10, an opening 100, 102 for the passage of the rigid tubes.
- the fabric 4 is integral with the rigid and semi-rigid tubes to hold the fabric in place on the frame 2.
- the edges 104, 106 of the openings 100, 102 of the fabric may be integral with the rigid tubes.
- the fabric 4 In position of the folded system, the fabric 4 forms folds 1 to enter the protective envelope 6 as shown in FIG.
- the fabric 4 of the system In the deployed position (see FIGS. 2a and 2b), the fabric 4 of the system has facets formed by the pairs of rigid tubes and their associated semi-rigid tubes, a facet f8 formed by the consecutive pairs P5 and P1 of rigid tubes and their tubes. associated semi-rigid, another facet f7 formed by the consecutive pairs P4 and P5 of rigid tubes and their associated semi-rigid tube.
- the system further comprises cables of predetermined lengths attached to one and the other end of the central tube 10, to give a predetermined shape to the deployed web.
- the system comprises three cables CL1, CL, CL3 fixed on one side and the other of the central tube 10, each of the cables being fixed between two angularly consecutive yokes around the XX 'axis to form additional facets on the deployed canvas and thus obtain different incidences of the facets of the fabric.
- the fabric 4 can be made from several sections of canvas assembled to obtain the ovoid shape when it is deployed.
- the fabric can be made from flexible and very resistant materials such as poly-para-phenylene terephthalamide sold under the trade name Kevlar.
- the protection system further comprises a device for pressurizing the chambers 80 of the rigid tubes to move the pistons 75 in the rigid tubes and deploy the armature.
- the yokes may include a stop in angular rotation of the rigid tubes after deployment of the frame.
- the yokes may also include another abutment for obtaining the angle of incidence ⁇ of the rigid tubes in the position of the folded reinforcement, the bearing abutments 94 on the central tube are then no longer necessary.
- Figure 3a shows a schematic axial sectional view showing the system according to the invention in the folded position.
- Figure 3b shows a schematic axial sectional view showing the system according to the invention in the deployed position.
- the protection system is enclosed in the protective envelope 6 of restricted section having at each end the closure flange 84, 86.
- the protective envelope 6 When actuating the protection system, the protective envelope 6 is open to allow the deployment of the frame and the protective fabric as described above.
- the pyrotechnic gas capsules are activated pressurizing the chambers 80 of the rigid tubes.
- the piston 75 of the semi-rigid tubes 70, 71, 72, 73, 74 are then pushed towards the free ends of the rigid tubes which undergo, by said pistons, forces transverse to the axis XX 'in the respective planes pli, pl2, pl3, pl4, pl5 pairs P1, P2, P3, P4, P5 of rigid tubes, pivoting the articulated ends of the rigid tubes away from the central tube 10.
- Each of the semi-rigid tubes 70, 71, 72, 73 , 74 also moving away from the central tube pushed by its pistons take then a form of arc which is modulated by the presence of the canvas 4 which they involve in their displacement.
- the pressure increase control of the chambers 80 is not necessarily simultaneous. A time shift is acceptable.
- FIG. 2b shows a schematic simplified sectional view in position of the deployed system showing the pairs P1 and P4 of rigid tubes and their semi-rigid tube 70, 73 associated in the respective axial planes pli, pl4.
- the pistons 75 of the semi-rigid tubes pushed by the gases under pressure in chambers 80 of the rigid tubes move in the rigid tubes causing in their displacement the intermediate guides 92 to the stops 90, which limits the deployment of the frame 2 .
- the length of the arc formed by two rigid tubes of a pair and its respective associated semi-rigid tube increases at the time of the deployment of the system resulting in the deployment of the canvas which then takes its form ovoid.
- the armature 2 with the cables CL1, CL2, CL3 modulate the outer shape of the fabric 4 forming the facets f1 to f8 in a generally ovoid shape.
- the armature may comprise a greater or lesser number of pairs of rigid and semi-rigid tubes associated (for example between 4 and 6 pairs and a variable number of intermediate cables to obtain a desired shape of the unfolded fabric.
- the protection system according to the invention has the advantage of a simplified implementation, more reliable, less expensive and easier to maintain than the systems of the state of the art with inflation of a protective cloth waterproof.
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tents Or Canopies (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0902732A FR2946422B1 (fr) | 2009-06-05 | 2009-06-05 | Systeme de protection deployable |
| PCT/EP2010/057756 WO2010139750A1 (fr) | 2009-06-05 | 2010-06-03 | Systeme de protection deployable |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2438388A1 true EP2438388A1 (fr) | 2012-04-11 |
| EP2438388B1 EP2438388B1 (fr) | 2013-07-24 |
Family
ID=41459805
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP10724739.7A Not-in-force EP2438388B1 (fr) | 2009-06-05 | 2010-06-03 | Systeme de protection deployable |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US8516942B2 (fr) |
| EP (1) | EP2438388B1 (fr) |
| ES (1) | ES2433571T3 (fr) |
| FR (1) | FR2946422B1 (fr) |
| IL (1) | IL216732A0 (fr) |
| WO (1) | WO2010139750A1 (fr) |
| ZA (1) | ZA201108875B (fr) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| LU92101B1 (fr) * | 2012-11-20 | 2014-05-21 | Raphael Vercruysse | Dispositif de protection de personnes ou d'objets |
Family Cites Families (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1324904A (en) * | 1919-12-16 | Tobpedo-gtjabd fob ships | ||
| US1463431A (en) * | 1923-07-31 | Protective curtain | ||
| US1263003A (en) * | 1917-07-11 | 1918-04-16 | Fred A Thomas | Torpedo-protector for vessels. |
| US1405294A (en) * | 1921-06-24 | 1922-01-31 | Corsini Atilio | Torpedo guard |
| US2337165A (en) * | 1943-03-08 | 1943-12-21 | Joseph M Olaszy | Protecting device for ships and other structures subject to enemy attack |
| US2385985A (en) * | 1944-04-13 | 1945-10-02 | George R Harrison | Ship |
| US2475239A (en) * | 1945-07-27 | 1949-07-05 | Fielding A Hambrick | Ship protector |
| US2490793A (en) * | 1945-10-25 | 1949-12-13 | Floyd L Fleming | Gunnery target |
| US3568191A (en) * | 1960-12-15 | 1971-03-02 | James C Hiester | Method for defending an aircraft against a frontal attack |
| US4021974A (en) * | 1976-03-05 | 1977-05-10 | Varo, Inc. | Camouflage disrupter frame |
| US4262595A (en) * | 1978-10-12 | 1981-04-21 | The Singer Company | Anti torpedo device |
| SE459885B (sv) * | 1985-02-22 | 1989-08-14 | Affarsverket Ffv | Fordonsburet system foer maskering med skum |
| US5249527A (en) * | 1992-07-01 | 1993-10-05 | Westinghouse Electric Corp. | High speed, inflating bag infrared countermeasure |
| FR2727506B1 (fr) * | 1994-11-30 | 1997-01-24 | Giat Ind Sa | Dispositif de protection d'un vehicule ou d'une structure |
| US5576508A (en) * | 1995-09-26 | 1996-11-19 | The United States Of America As Represented By The Secretary Of The Army | Extendable armor |
| US6647855B1 (en) * | 2002-09-30 | 2003-11-18 | The United States Of America As Represented By The United States National Aeronautics And Space Administration | Apparatus and method for deploying a hypervelocity shield |
| DE102005038071A1 (de) * | 2005-08-10 | 2007-02-15 | Rheinmetall Waffe Munition Gmbh | Vorrichtung sowie Verfahren zum Schutz von Fahrzeugen vor Munition, insbesondere vor Hohlladungsgeschossen |
| DE102005060882B3 (de) * | 2005-12-20 | 2007-05-24 | Bundesrepublik Deutschland, vertreten durch das Bundesministerium der Verteidigung, vertreten durch das Bundesamt für Wehrtechnik und Beschaffung | Nichtletales Impulsgeschoss |
| US7866250B2 (en) * | 2006-02-09 | 2011-01-11 | Foster-Miller, Inc. | Vehicle protection system |
-
2009
- 2009-06-05 FR FR0902732A patent/FR2946422B1/fr not_active Expired - Fee Related
-
2010
- 2010-06-03 WO PCT/EP2010/057756 patent/WO2010139750A1/fr not_active Ceased
- 2010-06-03 EP EP10724739.7A patent/EP2438388B1/fr not_active Not-in-force
- 2010-06-03 ES ES10724739T patent/ES2433571T3/es active Active
- 2010-06-03 US US13/376,028 patent/US8516942B2/en not_active Expired - Fee Related
-
2011
- 2011-12-01 IL IL216732A patent/IL216732A0/en unknown
- 2011-12-02 ZA ZA2011/08875A patent/ZA201108875B/en unknown
Non-Patent Citations (1)
| Title |
|---|
| See references of WO2010139750A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2010139750A1 (fr) | 2010-12-09 |
| FR2946422B1 (fr) | 2011-07-15 |
| FR2946422A1 (fr) | 2010-12-10 |
| ES2433571T3 (es) | 2013-12-11 |
| US20120125188A1 (en) | 2012-05-24 |
| ZA201108875B (en) | 2013-01-30 |
| IL216732A0 (en) | 2012-02-29 |
| EP2438388B1 (fr) | 2013-07-24 |
| US8516942B2 (en) | 2013-08-27 |
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