EP2350556A1 - Système d'absorption de l'énergie des souffles d'explosion - Google Patents

Système d'absorption de l'énergie des souffles d'explosion

Info

Publication number
EP2350556A1
EP2350556A1 EP09812499A EP09812499A EP2350556A1 EP 2350556 A1 EP2350556 A1 EP 2350556A1 EP 09812499 A EP09812499 A EP 09812499A EP 09812499 A EP09812499 A EP 09812499A EP 2350556 A1 EP2350556 A1 EP 2350556A1
Authority
EP
European Patent Office
Prior art keywords
blast
vertical
understructure
longitudinal
energy absorbing
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Withdrawn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
EP09812499A
Other languages
German (de)
English (en)
Inventor
Gregory Lucas Peer
Edward A. Timko
Louis Edgar Forsythe
Miloslav Novak
Deryck H. Serrano
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.)
Howmet Aerospace Inc
Original Assignee
Alcoa Inc
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 Alcoa Inc filed Critical Alcoa Inc
Publication of EP2350556A1 publication Critical patent/EP2350556A1/fr
Withdrawn legal-status Critical Current

Links

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
    • F41H7/00—Armoured or armed vehicles
    • F41H7/02—Land vehicles with enclosing armour, e.g. tanks
    • F41H7/04—Armour construction
    • F41H7/042—Floors or base plates for increased land mine protection

Definitions

  • Blast energy absorption system dimensioned to be integrated into the structure of a vehicle, and in particular multiple, removable, interchangeable, and configurable components adaptable to configure the vehicle for varying mission threats are disclosed.
  • a blast energy absorption system comprises: at least first and second floor structures, wherein each floor structure is dimensioned for integration in a longitudinal-horizontal plane of a vehicle; and a housing disposed between the at least first and second floor structures, wherein the housing comprises at least first and second vertical members, wherein a body portion of the first vertical member is connected to a first side of the first floor structure, and wherein a body portion of the second vertical member is connected to a first side of the second floor structure; and wherein each of the floor structures and the housing is configured to absorb blast energy by dampening blast loads along at least one of horizontal-longitudinal plane, longitudinal-vertical plane, and horizontal-vertical plane.
  • the system includes an understructure disposed underneath the at least first and second floor structures and the housing, wherein a first side of the understructure is connected to a second side of the first floor structure, wherein a second side of the understructure is connected to a second side of the second floor structure, wherein a first body portion of the understructure is connected to one end of the first vertical member, and wherein a second body portion of the understructure is connected to one end of the second vertical member; and wherein the first floor structure, the first vertical member, and the understructure are configured to form a first compartment, wherein the second floor structure, the second vertical member, and the understructure are configured to form a second compartment, wherein the housing and the understructure are configured to form a third compartment, and wherein each of the compartments is configured to absorb blast energy by dampening blast loads along a portion of at least one of the at least first and second floor structures, the at least first and second vertical members, the housing, and the understructure.
  • the system includes at least one cross beam member horizontally arranged on top of the understructure, wherein the at least one cross beam member is housed within the third compartment, and wherein the at least one cross beam member is configured to absorb blast energy by dampening blast loads along a horizontal direction.
  • the system includes at least one of longitudinal and vertical blast energy absorbing members housed within the third compartment, wherein the at least one of longitudinal and vertical blast energy absorbing members is configured to absorb blast energy by dampening blast loads along at least one of longitudinal and vertical directions.
  • the system includes at least one adjustable energy absorbing container disposed within each of the first and the second compartments, wherein the at least one adjustable energy absorbing container is configured to absorb blast energy by dampening blast loads along at least one of horizontal, longitudinal, and vertical directions.
  • the system includes at least one of interior and exterior support structures housed within each of the first and second compartments, wherein the at least one of interior and exterior support structures is configured to absorb blast energy by dampening blast loads along at least one of the at least one of interior and exterior support structures.
  • the system includes at least one crush element disposed within the at least one adjustable energy absorbing container, wherein the at least one crush element is configured to absorb blast energy by dampening blast loads along the at least one of horizontal-longitudinal plane, longitudinal-vertical plane, and horizontal-vertical plane.
  • One embodiment of a blast energy absorption system comprises at least first and second floor structures, wherein each floor structure is dimensioned for integration in a longitudinal-horizontal plane of a vehicle; a housing disposed between the at least first and second floor structures, wherein the housing comprises at least first and second vertical members, and wherein a body portion of the first vertical member is connected to a first side of the first floor structure, and wherein a body portion of the second vertical member is connected to a first side of the second floor structure; and an understructure disposed underneath the at least first and second floor structures and the housing, wherein a first side of the understructure is connected to a second side of the first floor structure, wherein a second side of the understructure is connected to a second side of the second floor structure, wherein a first body portion of the understructure is connected to one end of the first vertical member, and wherein a second body portion of the understructure is connected to one end of the second vertical member; and wherein the first floor structure, the first vertical member, and the understructure are configured to
  • the system includes at least one cross beam member horizontally arranged on top of the understructure, wherein the at least one cross beam member is housed within the third compartment, and wherein the at least one cross beam member is configured to absorb blast energy by dampening blast loads along a horizontal direction.
  • the system includes at least one adjustable energy absorbing container disposed within each of the first and the second compartments, wherein the at least one adjustable energy absorbing container is configured to absorb blast energy by dampening blast loads along at least one of horizontal, longitudinal, and vertical directions.
  • the system includes at least one of longitudinal and vertical blast energy absorbing members housed within the third compartment, wherein the at least one of longitudinal and vertical blast energy absorbing members is configured to absorb blast energy by dampening blast loads along the at least one of longitudinal and vertical directions.
  • the system includes at least one adjustable energy absorbing container disposed within each of the first and the second compartments, wherein the at least one adjustable energy absorbing container is configured to absorb blast energy by dampening blast loads along the at least one of horizontal, longitudinal, and vertical directions.
  • the system includes at least one of interior and exterior support structures housed within each of the first and second compartments, wherein the at least one of interior and exterior support structures is configured to absorb blast energy by dampening blast loads along at least one of the at least one of interior and exterior support structures.
  • the system includes at least one crush element disposed within the at least one adjustable energy absorbing container, wherein the at least one crush element is configured to absorb blast energy by dampening blast loads along at least one of horizontal-longitudinal plane, longitudinal-vertical plane, and horizontal-vertical plane.
  • One embodiment of a blast energy absorption system comprises: at least first and second floor structures, wherein each floor structure is dimensioned for integration in a longitudinal-horizontal plane of a vehicle; a housing disposed between the at least first and second floor structures, wherein the housing comprises at least first and second vertical members, and wherein a body portion of the first vertical member is connected to a first side of the first floor structure, and wherein a body portion of the second vertical member is connected to a first side of the second floor structure; an understructure disposed underneath the at least first and second floor structures and the housing, wherein a first side of the understructure is connected to a second side of the first floor structure, wherein a second side of the understructure is connected to a second side of the second floor structure, wherein a first body portion of the understructure is connected to one end of the first vertical member, and wherein a second body portion of the understructure is connected to one end of the second vertical member; and wherein the first floor structure, the first vertical member, and the understructure are configured to
  • the system includes at least one of longitudinal and vertical blast energy absorbing members housed within the third compartment, wherein the at least one of longitudinal and vertical blast energy absorbing members is configured to absorb blast energy by dampening blast loads along at least one of longitudinal and vertical directions.
  • the system includes at least one adjustable energy absorbing container disposed within each of the first and the second compartments, wherein the at least one adjustable energy absorbing container is configured to absorb blast energy by dampening blast loads along at least one of horizontal, longitudinal, and vertical directions.
  • the system includes at least one of interior and exterior support structures housed within each of the first and second compartments, wherein the at least one of interior and exterior support structures is configured to absorb blast energy by dampening blast loads along at least one of the at least one of interior and exterior support structures.
  • the system includes at least one crush element disposed within the at least one adjustable energy absorbing container, wherein the at least one crush element is configured to absorb blast energy by dampening blast loads along at least one of horizontal-longitudinal plane, longitudinal-vertical plane, and horizontal-vertical plane.
  • FIGS. IA and IB are perspective and cross-section views, respectively, of one embodiment of the present disclosure.
  • FIGS. 2A and 2B are perspective top and bottom views, respectively, of the embodiment of FIGS. IA and IB integrated into a vehicle;
  • FIGS. 3A and 3B are perspective top and bottom views, respectively, of an understructure of the embodiment of FIGS. IA and IB;
  • FIGS. 4A-4J are perspective and exploded views of various embodiments of an adjustable energy absorbing container
  • FIGS. 5A and 5B are top and side views, respectively, of various embodiments of alternative crush element retention devices
  • FIGS. 6A and 6B are top views of alternative crush element retention devices sized to retain different sized crush elements
  • FIG. 7 illustrates side views of alternative crush element retention devices integral with different sized crush elements
  • FIGS. 8A-8D are illustrations of an alternative embodiment of an adjustable energy absorbing containers engagement feature
  • FIGS. 9A-9C are perspective views of an alternative embodiment of a horizontal retention device in engaged and disengaged position respectively;
  • FIGS. 1OA and 1OB are perspective views of an alternative embodiment of a horizontal retention device in engaged and disengaged position respectively;
  • FIG. 11 is a perspective view of one embodiment of the crush elements installed into an interior support structure
  • FIG. 12A-C are perspective views of an alternative embodiment of a crush element retention sleeve.
  • FIGS. 13 A and 13B are cross-section views of a crush element installed into an interior support structure using another alternative crush element retention device.
  • FIGS. IA and IB are perspective and cross-section views, respectively, of a blast energy absorption system 2 according to one embodiment of the present disclosure
  • the blast energy absorption system 2 includes a housing 6 coupled to two floor structures 4 on opposing sides of the housing 6.
  • the housing 6 may be disposed between the two floor structures 4.
  • the floor structures 4 and the housing 6 are configured to be integrated in a substantially longitudinal-horizontal (x-y) plane as defined by the axes shown, hi one instance, the blast energy absorption system 2 may be dimensioned for integration in a longitudinal -horizontal (x-y) plane of a vehicle.
  • FIGS. 2A and 2B are perspective top and bottom views, respectively, of an embodiment of a blast energy absorption system 2 being integrated into a floor of a vehicle 100 including the likes of jeeps, sedans, cars, tanks and military vehicles, among others.
  • the floor structures 4 may be dimensioned for integration into the floor of the vehicle 100.
  • the housing 6 may be dimensioned for integration into the floor of the vehicle 100.
  • these and other components may be integrated into the floor of the vehicle 100 and will become more apparent in subsequent figures and discussion.
  • all the components of the blast energy absorption system 2 may be dimensioned for integration into the chassis and/or frame of the vehicle 100.
  • all the components may be integrated directly or indirectly into the vehicle 100.
  • the components may be connected by semi -permanent fastening techniques or re-attachable fastening techniques.
  • the components may be removable either for repair or for varying the level of occupant protection, among others (e.g., weight limitation).
  • the housing 6 has a substantially three-sided (e.g., u-shape) box-like structure with horizontal members 48 connected to vertical members 46 on opposing ends 48A of the horizontal member 48.
  • a body portion of the vertical member 46 may be connected to one end of the floor structure 4, while a similar body portion of the vertical member 46 may be connected to one end of the floor structure 4 on an opposite side of the housing 6.
  • the three-sided box-like structure tapers along a longitudinal (x) direction of the housing 6 as best shown in FIG. IA.
  • the three-sided box-like structure may extend throughout the entire length of the housing 6 along the longitudinal (x) direction (not shown).
  • each of the floor structures 4 and the housing 6 is capable of providing load transfer in at least one of longitudinal (x) direction, horizontal (y) direction or vertical (z) direction to dampen blast loads, hi other embodiments, each of the floor structures 4 and the housing 6 is capable of providing load transfer in at least one of horizontal-longitudinal (y-x) plane, longitudinal-vertical (x-z) plane, or horizontal-vertical (y-z) plane for dampening blast loads.
  • blast load and the like means a blast event external to a vehicle.
  • blast load includes any forces external to a vehicle including the likes of bullets, bombs, explosives, grenades, missiles, artillery fires, among others.
  • each of the components of the blast energy absorption system 2 is capable of dissipating blast energy from the blast loads along at least one direction and/or one plane.
  • at least one longitudinal blast energy absorbing member 5OA may be disposed within the housing 6 to supplement the blast energy absorbing capability of the housing 6.
  • the longitudinal blast energy absorbing member 5OA is disposed within the housing 6 along a substantially longitudinal (x) direction.
  • the longitudinal blast energy absorbing member 5OA may dampen blast loads along a portion of at least one of horizontal-longitudinal (y-x) or vertical-longitudinal (z-x) planes. In some instances, the longitudinal blast energy absorbing member 5OA may dampen blast loads along a substantially longitudinal (x) direction.
  • At least one vertical blast energy absorbing member 5OB may be disposed within the housing 6 to supplement the blast energy absorbing capability of the housing 6.
  • the vertical blast energy absorbing member 5OB is disposed within the housing 6 along a substantially vertical (z) direction.
  • the vertical blast energy absorbing member 5OB may dampen blast loads along a portion of at least one of longitudinal-vertical (x-z) or horizontal-vertical (y-z) planes.
  • the vertical blast energy absorbing member 5OB may dampen blast loads along a substantially vertical (z) direction.
  • At least one cross member 8 may be disposed within the housing 6 to supplement the blast energy absorbing capability of the housing 6.
  • the cross member 8 is disposed within the housing 6 along a substantially horizontal (y) direction.
  • the cross member 8 may dampen blast loads along a portion of at least one of longitudinal-horizontal (x-y) or vertical-horizontal (z-y) planes.
  • the cross member 8 may dampen blast loads along a substantially horizontal (y) direction.
  • the blast energy absorption system 2 includes an understructure 10 disposed underneath the floor structures 4 and the housing 6. hi some instances, the understructure 10 may be integrated into an undercarriage of a vehicle 100. In other instances, the understructure 10 may be disposed about an exterior portion of a vehicle 100.
  • FIGS. 3A and 3B are perspective top and bottom views, respectively, of an understructure 10 according to an embodiment of FIGS. IA and IB.
  • the understructure 10 of an armored vehicle includes a bottom plate 12 and two cover plates 14 of armor.
  • the number of and general shapes of the bottom plate 12 and the cover plates 14 may vary depending on the vehicle and type of mission. As such, the illustrations herein are for illustration purposes only and are not intended to limit the claimed disclosure.
  • the bottom plate 12 may be connected to two cover plates 14 on opposing sides of the bottom plate 12.
  • one end of a cover plate 14 may be connected to an end of the floor structure 4 via through holes 68 sized to receive threaded bolts 70 for engaging with through holes 72 of the floor structure 4 (best shown in FIG. IB).
  • an opposite end of the cover plate 14 may be coupled to an end of the bottom plate 12 via an overlapping arrangement (best shown in FIG. IB and corresponding inset).
  • the bottom plate 12 and the cover plate 14 may be arranged in an overlapping relationship 20 along a mating edge 22 that substantially eliminates any gaps between the mating parts 12, 14 and improves the blast integrity by reducing any blast air infiltration leak paths into the vehicle.
  • an end of the bottom plate 12 may include a lip 24 having a cutout 26 with a depth D being approximately the thickness T of the cover plate 14.
  • the cutout 26 may have a length L sufficient such that gap G is less than length L during operational mission conditions.
  • the cover plate 14 may be completely received within the cutout 26 without any gap G and with the depth D being approximately the thickness T.
  • additional fasteners may be utilized (e.g., nuts, bolts) to ensure that the bottom plate 12 and the cover plate 14 are securely fastened to each other.
  • cover plate 14 may be secured to the bottom plate 12 via fasteners (e.g., nuts, bolts) or the plates 14, 12 may be an integrated unit (e.g., welding, single aluminum sheet formed by bending).
  • fasteners e.g., nuts, bolts
  • the plates 14, 12 may be an integrated unit (e.g., welding, single aluminum sheet formed by bending).
  • the bottom plate 12 of the blast energy absorption system 2 can be a sandwiched structure having outer skins 16A, 16B and a core 18 (best shown in FIGS. IB and 3A).
  • the outer skins 16A and 16B can be made of a metallic material (e.g. steel, aluminum) or a composite structure (e.g., plastic, thermoplastic, polymer).
  • the core 18 can be made of a metallic material (e.g. steel, aluminum), composite structure (e.g., plastic, thermoplastic, polymer), or foam (e.g. metal, plastic).
  • the cover plates 14 may also include through holes 68 sized to receive threaded bolts 70 for engaging with through holes 72 of the floor structures 4 and with through holes 74 disposed about the exterior support structures 28 (best shown in FIG. IB). In one instance, the two cover plates 14 may be first attached followed by the bottom plate 12 to complete installation of the blast energy absorption system 2.
  • the portion of the bottom plate 12, while coupled to a portion of the cover plate 14, may also be connected to a portion of the vertical member 46 via through holes 64 sized to receive a threaded bolt 62 for engaging with through holes 66 of the housing 6.
  • the floor structure 4, the vertical member 46, and the understructure 10 are capable of forming a side compartment 91.
  • the housing 6 and the understructure 10 are capable of forming a central compartment 93.
  • the compartments 91, 93 are capable of absorbing blast energy by dampening blast loads along a portion of at least one of the floor structures 4, the vertical members 46, the housing 6 and the understructure 10.
  • at least one longitudinal blast energy absorbing member 5OA, 5OB may be housed within the central compartment 93, along with at least one cross member 8.
  • At least one of the floor structures 4, the housing 6, the understructure 10, the longitudinal blast energy absorbing members 5OA, the vertical blast energy absorbing members 5OB, and the cross members 8 is capable of providing load transfer in at least one of longitudinal (x) direction, horizontal (y) direction or vertical (z) direction to dampen blast loads.
  • at least one of the floor structures 4, the housing 6, the understructure 10, the longitudinal blast energy absorbing members 5OA, the vertical blast energy absorbing members 5OB, and the cross members 8 is capable of providing load transfer in at least one of horizontal-longitudinal (y-x) plane, longitudinal- vertical (x-z) plane, or horizontal-vertical (y-z) plane for dampening blast loads.
  • At least one of the compartments 91, 93 is capable of providing load transfer in at least one of longitudinal (x) direction, horizontal (y) direction or vertical (z) direction to dampen blast loads. In other embodiments, at least one of the compartments 91, 93 is capable of providing load transfer in at least one of horizontal- longitudinal (y-x) plane, longitudinal-vertical (x-z) plane, or horizontal-vertical (y-z) plane for dampening blast loads.
  • the understructure 10 has been described as having multiple members (e.g., bottom plate 12 and two cover plates 14), in one embodiment, the understructure 10 may be provided as an integrated, singular member (e.g., welding separate components, bending an aluminum sheet or plate).
  • At least one cross beam member 8 may be horizontally arranged on top of the understructure 10 and housed within the central compartment 93.
  • a bottom portion of the cross beam member 8 may include an aperture 66 while an adjacent end of the bottom plate 12 of the understructure 10 may include a corresponding aperture 64.
  • the apertures 66, 64 may be similarly sized and threaded. Accordingly, the apertures 66, 64 may be capable of receiving a bolt 62 for securely attaching the cross beam member 8 to a portion of the understructure 10.
  • the cross beam member 8 is configured to absorb blast energy by dampening blast loads at least along a horizontal direction, among others.
  • the cross beam member 8 may be coupled to the housing 6 via a cross beam member attachment member 52.
  • one end 54 of the cross beam member attachment member 52 may include through holes 56 while an adjacent end of the cross beam member 8 may include corresponding through holes 58.
  • the through holes 56, 58 may be similarly sized and threaded. Accordingly, each of the through holes 56, 58 may be capable of receiving a bolt 60 for securely attaching the cross beam member 8 to a portion of the housing 6.
  • An opposite end of the cross beam member attachment member 52 may be fastened to the vertical member 46 in a similar fashion. In other embodiments, the opposite end of the cross beam member attachment member 52 may be permanently fastened to a portion of the vertical member 46 via welding, among other bonding techniques.
  • the number of cross beam members 8 attached to the housing 6 at any given time may depend on the mission threat.
  • one embodiment of the blast energy absorption system 2 includes at least two floor structures 4 and a central housing 6 for a minimal or no mission threat, hi addition, the two floor structures 4 and the central housing 6 may function as integral components of a vehicle 100 (see FIGS. 2A and 2B).
  • the housing 6 may act as a center hub interconnecting a plurality of independent reactant systems (e.g., cross beam members 8, adjustable energy absorbing containers 9, understructure 10) on one side of the vehicle 100 to corresponding independent reactant systems 8, 9, 10 on the other side of the vehicle 100.
  • the housing 6 is capable of interconnecting a plurality of independent reactant systems to the vehicle 100.
  • FIGS. 4A-4J are perspective and exploded views of various embodiments of an adjustable energy absorbing container 9 for a blast energy absorption system 2.
  • the adjustable energy absorbing containers 9 includes an exterior support structure 28 (e.g., angle brackets), an interior support structure 30, and one or more crush elements 32, which will be discussed in more details below.
  • each component may be an independent reactant system. The integral relationship between the above mentioned components may form a system that is capable of absorbing and distributing blast energy to minimize energy transfer to occupants of a vehicle.
  • the blast energy absorption system 2 is capable of many configurations depending on the threat level of a mission.
  • a blast energy absorption system 2 includes at least two floor structures 4, the housing 6 and the understructure 10 for high mission threats levels.
  • a blast energy absorption system 2 includes at least two floor structures 4, the housing 6, the understructure 10 and at least one cross beam members 8 for higher mission threats.
  • a blast energy absorption system 2 includes at least two floor structures 4, the housing 6, the understructure 10, exterior support structure 28 and interior support structure 30 for higher mission threats. Additional details about the exterior support structure 28 and the interior support structure 30 will become more apparent in subsequent figures and discussion.
  • a blast energy absorption system 2 includes at least two floor structures 4, the housing 6, the understructure 10, at least one cross beam members 8, exterior support structure 28 and interior support structure 30 for higher mission threats.
  • a blast energy absorption system 2 includes at least two floor structures 4, the housing 6, the understructure 10, at least one cross beam members 8, exterior support structure 28, interior support structure 30 and one or more crush elements 32 for yet a higher mission threats. Additional details about the one or more crush elements 32 will become more apparent in subsequent figures and discussion.
  • the adjustable energy absorbing container 9 can include an exterior support structure 28 (e.g., angle brackets), interior support structure 30, and crush elements 32.
  • the exterior support structure 28, the interior support structure 30, and the crush elements 32 are capable of forming a triangular box-like structure.
  • the interior support structure 30 can be an extrusion or forging having an outer frame 38 and energy absorbing members 40 interiorly connected to the outer frame 38 to form collapsible cavities 42.
  • the outer frame 38 may be substantially planar extending along at least a portion of the horizontal-longitudinal (y-x) and/or longitudinal-vertical (x-z) planes.
  • the outer frame 38 may be substantially adjacent the understructure 10 and runs along the length of the outer cover plates 14.
  • a side 44 of the outer frame 38 adjacent the cover plate 14 may include at least one aperture 34 for forming at least one cavity 36, wherein the aperture 34 and the cavity 36 are both sized to receive and retain crush elements 32.
  • the crush elements may be retained in the apertures 34 and cavities 36 by semi-permanent and/or re- attachable fastening techniques. These and other embodiments of the crush elements 32 will be described in more detail below.
  • the adjustable energy absorbing container 9 may be connected to a portion of the floor structure 4 via one or more bolts 74.
  • an upper portion of the exterior support structure 28 of the adjustable energy absorbing container 9 may include through holes 78 while an adjacent portion of the floor structure 4 may include corresponding through holes 76.
  • the through holes 78, 76 may be similarly sized and threaded.
  • the through holes 76 may be counter-sunk and the through holes 78 may be threaded to correspond.
  • each of the through holes 78, 76 may be capable of receiving a bolt 74 for securely attaching the adjustable energy absorbing container 9 to a portion of the floor structure 4.
  • the adjustable energy absorbing containers 9, having three- dimensional box-like structures may be disposed within each of the side compartments 91.
  • the adjustable energy absorbing containers 9 are capable of providing load transfer in at least one of longitudinal (x) direction, horizontal (y) direction or vertical (z) direction to dampen blast loads.
  • the adjustable energy absorbing containers 9 are capable of providing load transfer in at least one of horizontal-longitudinal (y-x) plane, longitudinal-vertical (x-z) plane, or horizontal-vertical (y-z) plane for dampening blast loads.
  • any combination of cross beam members 8, adjustable crush containers 9 e.g., exterior support structure 28, interior support structure 30, and crush elements 32
  • each component is designed to plastically deform (e.g., buckle, bend) to absorb energy from a bomb or mine blast and not to fragment into small pieces that become projectiles.
  • the energy that is not dissipated by these components may be dissipated by the floor structures 4 and/or the housing 6 with minimal or reduced plastic deformation.
  • the adjustable energy absorbing container 9 may be slidably attached to the bottom surface of the floor structure 4 as best shown in FIG. 4A.
  • the adjustable energy absorbing container 9 includes a casing 80 that encases the exterior support structure 28, the interior support structure 30, and the crush elements 32.
  • the enclosure of the casing 80 may facilitate the installation of the adjustable energy absorbing container 9 from an exterior portion of the vehicle 100 without having to gain entry into the vehicle 100 to remove attachment features including the likes of nuts and bolts, among others.
  • the ability to change external armament configuration may allow for a change in armor while solders are on-board a vehicle 100 waiting or are otherwise readying the vehicle 100 (e.g., replenishing ammunition, ordnances, supplies) for the next mission without interference by the ground crew changing the armor (e.g., adjustable energy absorbing containers 9).
  • the casing 80 may include a series of handles 82, 84 to facilitate the handling and installation of the casing 80 onto a vehicle 100 (best shown in FIGS. 4C-4D and 4G-4I). Handles 82, 84 may be located on an edge 86 or a side 88 of the casing 80. Depending on the size of the adjustable energy absorbing containers 9A, 9B, smaller adjustable energy absorbing container 9B may be picked up and carried by one installer while larger adjustable energy absorbing container 9A may need to be picked up and carried by two or more installers either because of weight or length. In some instances, multiple small adjustable energy absorbing containers 9 may be installed simultaneously as best shown in FIGS. 4H and 41.
  • the casing 80 includes a top surface 96 that opens for the installation and removal of the crush elements 32 as best illustrated in FIG. 4A.
  • the top surface 96 allows for access to exterior support structures 28 and interior support structures 30 for routine maintenance and/or repairs.
  • ground crew members need not change the entire adjustable energy absorbing container 9 but instead may change out crush elements 32, exterior support structures 28, or interior support structures 30, among others as necessary.
  • any components within the casing 80 of the adjustable energy absorbing container 9 may be module- like and may be maintained and/or repaired using external access without interior access to the vehicle 100.
  • the top surface 96 may be movably attached or connected to a back surface 158 along a back edge 162 or at least one side 88 along a side edge 164 as best illustrated in FIGS. 4A and 4C.
  • the attachment between the top surface 96 and the back surface 158 or the sides 88 can be a solid connection or joint where the top surface 96 and the back surface 158 or the sides 88 are a monolithic or single piece of material that is bent approximately 90 degrees to form the substantially 90 degree orientation of the top surface 96 to the back surface 158 or the sides 88.
  • there can be sufficient spring-back in the solid joint making it capable of opening and closing several times without fatiguing the joint and without a device such as a conventional hinge.
  • the top surface 96 may be attached to the back surface 158 and the sides 88 via hinges (not shown).
  • the top surface 96 can include a rotatable latch 160 having an extension 166 that contacts an inner leading edge 89 of a lower surface 168 for temporarily securing the top surface 96 to the lower surface 168.
  • the rotatable latch 160 is capable of securing the top surface 96 to the leading edge 86 and the inner leading edge 89.
  • the leading edge 86 of the lower surface 168 may be integrated with a bottom side 152 of the adjustable energy absorbing container 9.
  • a clockwise rotation of the latch 160 would release the top surface 96 from the lower surface 168.
  • a counter-clockwise rotation would secure the top surface 96 to the lower surface 168.
  • different angles of rotation and/or amount of rotation may be made to secure and/or release the top surface 96 from the lower surface 168.
  • recessed hand grips 90 may be located on a bottom side 152 of the adjustable energy absorbing container 9 as best illustrated in FIGS. 4D-4F.
  • the recessed hand grips 90 may be covered by spring-loaded flappers 154 that may substantially cover and seal the interior of the recessed hand grips 90 from environmental dirt and debris, hi another example, the spring-loaded flappers 154 may streamline the bottom surface 152 to remove discontinuities on the bottom surface 152 for improved aerodynamic performance. In these instances, the spring-loaded flappers 154 may be actuated to allow handling of the adjustable energy absorbing containers 9 using the recessed hand grips 90 as best illustrated in FIGS. 4E-4F.
  • the casing 80 may be coupled to the floor structure 4 via engaging members 92 and cooperating engagement features 94 as best illustrated in FIG. 4A.
  • the engagement may be that of a dovetail or dovetail joint.
  • the engaging member 92 may be a dovetail joint received within the cooperating engagement feature 94 such as a dovetail slot, hi this instance, the engagement members 92 are disposed about a top surface 96 of the adjustable energy absorbing container 9 while the cooperating engagement features 94 are disposed about a bottom surface 98 of the floor structure 4.
  • the dovetail joint 92 and the dovetail slot 94 may be slidably engaged.
  • the geometries of the dovetail joints 92 may be slightly smaller in size than the dovetail slots 94 to facilitate ease of installation and removal.
  • the engagement may be sufficient as to prevent the adjustable energy absorbing container 9 from significant vertical, horizontal and/or longitudinal movements under operational mission conditions.
  • the coefficient of friction between engaging member mating surface 95A and the cooperating engagement feature mating surface 95B may be low enough to facilitate ease of sliding the dovetail joint 92 in and out of the dovetail slot 94.
  • the reduced coefficient of friction may minimize or mitigate binding of the adjustable energy absorbing container 9 to the floor structure 4 during removal and/or installation.
  • the engagement features are capable of enabling installation of the adjustable energy absorbing containers 9 from the exterior of the vehicle 100 without the need to enter the occupant compartment.
  • an adjustable energy absorbing container 9 can be lifted for installation onto a vehicle by a single person.
  • the person places fingers onto spring loaded flappers 154 and slightly pushes inward displacing the spring loaded flappers 154 into the recesses 90 in order to hold and balance the adjustable energy absorbing container 9.
  • the person can use his or her forearms to steady and distribute the load of the adjustable energy absorbing container 9 while picking up, as well as transportation.
  • the person transports the adjustable energy absorbing container 9 (shown only as blast energy absorption system 2 for convenience) to the vehicle 100 and positions the adjustable energy absorbing container 9 for horizontal installation (y-direction relative to vehicle orientation) onto the vehicle 100.
  • retention devices may be actuated.
  • Retention devices can be any suitable mechanical, electrical, electromechanical, or magnetic devices capable of holding the adjustable energy absorbing container 9 in place when longitudinal, horizontal or vertical loads are induced onto the vehicle 100 due to events such as hard cornering or serpentine maneuvers to avoid enemy assault.
  • Retention devices may also be helpful during the installation process to hold the adjustable energy absorbing container 9 in place during the installation of other components of the blast energy absorption system 2 (e.g., cover plates 14).
  • the cover plates 14 may further strengthen and secure the adjustable energy absorbing container 9.
  • retention devices may also facilitate the installation process by holding the adjustable energy absorbing container 9 steady on un-level surfaces or while the vehicle 100 is in motion.
  • the casing 80 of the adjustable energy absorbing container 9 can include vertically-oriented retention devices 102 situated about portions of the top surface 96.
  • the retention devices 102 may be received by corresponding engagement recesses 104 disposed about an edge of the floor structure 4 for inhibiting movement of the casing 80 in at least one of horizontal, longitudinal or vertical direction when the vehicle 100 is in operation or when the vehicle 100 is parked on an uneven surface.
  • the retention device 102 can be a pivotal pin operably attached to the handles 82, whereby the retention device 102 may be rotated 90 degrees by rotating the handle 82 by 90 degrees.
  • the casing 80 can include horizontally-oriented cooperating retention devices 106 extending through horizontal retention devices 108 of the housing 6 as best illustrated in FIGS. 4B and 9A-9C.
  • the cooperating retention devices 106 and the horizontal retention devices 108 may be installed in the casing 80 as shown, hi other embodiments, the horizontal retention devices 108 may be installed on the longitudinal or vertical blast energy absorbing members 5OA, 5OB within the housing 6.
  • FIGS. 9A-9C illustrate the cooperating retention device 106 engaging and disengaging the horizontal retention devices 108.
  • FIGS. 9A and 9C shows the devices 106, 108 in an engaged or locked position while FIG.
  • the horizontally-oriented cooperating retention device 106 may include a pin 110 at one end 112 of a longitudinal member 114, while an opposite end 116 of the longitudinal member 114 may be operably connected to a handle 82.
  • the horizontal retention device 108 can be a slot having width and length being slightly larger than the width and length of the pin 110.
  • the pin 110 may be aligned with the slot 108 and inserted therethrough as best illustrated in FIG. 9B. Once the pin 110 has cleared the slot 108, the handle 82 may be rotated 90 degrees to rotate the pin 110 such that the pin 110 makes contact with an interior housing wall 170.
  • the cooperating retention device 106 may be situated at a first horizontal position (9 o'clock position) or a second horizontal position (3 o'clock position) relative to the slot 108 as best illustrated in FIGS. 9A and 9C, respectively.
  • the cooperating retention device 106 may be rotated to a vertical position (12 o'clock position) as best illustrated in FIG. 9B. In some embodiments, the rotation of the cooperating retention device 106 may be carried out with or without the use of handle 82.
  • a retractable pin mechanism 190 may be used for horizontally retaining the adjustable energy absorbing container 9 as best illustrated in FIGS. 1OA (engaged position) and 1OB (disengaged position), hi this embodiment, the retractable pin mechanism 190 includes a pin 192 operably connected to a handle 82, which may be pivotally coupled to a leading edge 86 of the adjustable energy absorbing container 9. The pin 192 may be received into and through a hole 194 disposed adjacent the leading edge 86. In the engaged position (FIG. 10A), the pin 192 extends beyond an upper surface 196 of the leading edge 86 and may be received into a hole or recess similar to the corresponding engagement recess 104 of the floor structure 4 as shown in FIG. 4A.
  • the spring 198 may be disposed between a washer unit 200 and a stopper unit 202.
  • the washer unit 200 may be pressed into the hole 194 and flush with an upper surface 196 while the stopper unit 202 may be fixedly connected to the pin 192.
  • the spring 198 may also be connected at each of its ends to the washer 200 and the stopper unit 202 such that as the handle 82 is rotated downward (FIG. 10A), the spring 198 stretches in response to the movement of the handle 82.
  • Another engagement feature according to the present disclosure includes vertical retention devices such as a hook latch 172 and a locking block 174 as best illustrated in FIGS. 8A and 8B.
  • the hook latch 172 may be rotatably connected to the side 88 of the casing 80 by a stationary pin 176.
  • a spring 178 may be attached to a pin 179, which is connected to the hook latch 172, and can bias the rotating hook latch 172 relative to the stationary pin 176 such that as a head 180 of the hook latch 172 contacts a side surface 181 of a locking block 174 connected to the floor structure 4, the hook latch 172 deflects or rotates counter-clockwise (or clockwise) until the head 180 vertically clears a top surface 182 of the locking block 174. Once the head 180 clears the top surface 182, spring 178 urges the hook latch 172 clockwise (or counter-clockwise) to receive a portion 184 of the locking block 174 into a hook recess 186.
  • the hook latch 172 can also include a release arm 188 to release the hook latch 172 from the locking block 174.
  • a release arm 188 By asserting a spring counter force Fl, F2 onto the release arm 188, the hook latch 172 rotates counter-clockwise (or clockwise) until the head 180 horizontally clears the top surface 182 of the locking block 174, thereby removing the vertical restraint allowing the adjustable energy absorbing container 9 to freely move downward.
  • Actuation of the release arm 188 can be manual by applying a downward force Fl or a horizontal Force F2.
  • the manual actuation can be carried out by a linkage mechanism (not shown) or a person's thumb (not shown).
  • the adjustable energy absorbing containers 9 may be horizontally installed (y-direction) onto a vehicle 100 as discussed above (FIGS. 4E-4J). In some embodiments, the adjustable energy absorbing containers 9 may be vertically installed (z- direction) onto a vehicle 100 as shown in FIGS. 8C and 8D. In this instance, a user (not shown) may position the adjustable energy absorbing container 9C below the floor structure 4, followed by bringing the adjustable energy absorbing container 9C vertically in the direction of arrows V for engaging the hook latch 172 with the locking block 174.
  • the spring force of the spring 178 may be sufficient not to require the horizontal retention devices 106, 108 as discussed above.
  • the horizontal retention devices 106, 108 as described herein may be necessary for installing the adjustable energy absorbing containers 9A, 9B, 9C to the floor structures 4.
  • FIG. 11 illustrates a perspective view of an interior support structure 30 containing at least one crush element 32.
  • the crush element 32 can take on other polygonal shapes and sizes, hi one embodiment, the crush element 32 may be loosely housed within a hole 34 of the interior support structure 30. In another embodiment, the crush element 32 may be semi-permanently fastened to the interior support structure 30. In one embodiment, the crush element 32 may be coupled to the interior support structure 30 via re-attachable fastening techniques. Regarding the re-attachable fastening techniques, minimal interference fit or press fit may be required for purposes of maintaining the crush element 32 in place. In these instances, the larger the interference fit, the higher the force is required to insert and remove the crush element 32.
  • each of the exterior support structure 28, the interior support structure 30, and the crush element 32 may be disposed within each of the side compartments 91.
  • at least one crush element 32 may be housed or disposed within the adjustable energy absorbing container 9, which can be housed within the side compartment 91.
  • at least one crush element 32 may be housed or disposed within the interior support structure 30.
  • each of the exterior support structure 28, the interior support structure 30, and the crush element 32 is capable of providing load transfer in at least one of longitudinal (x) direction, horizontal (y) direction or vertical (z) direction to dampen blast loads.
  • each of the exterior support structure 28, the interior support structure 30, and the crush element 32 is capable of providing load transfer in at least one of horizontal-longitudinal (y-x) plane, longitudinal-vertical (x-z) plane, or horizontal- vertical (y-z) plane for dampening blast loads.
  • the exterior support structure 28 is configured to absorb blast load or blast energy by dampening blast loads along the exterior support structure 28.
  • the interior support structure 30 is configured to absorb blast load or blast energy by dampening blast loads along the interior support structure 30.
  • the crush element 32 is configured to absorb blast load or blast energy by dampening blast loads along the crush element 32.
  • each of the exterior support structure 28, the interior support structure 30, and the crush element 32 is capable of collapsing on itself to absorb or resist the blast energy from the blast loads thereby minimizing physical harm to the occupants within the vehicle.
  • the crush element 32 may be circular in shape with an outer diameter greater than the diameter of the hole 34.
  • the contact surface area of the crush element in relation to the hole 34 may be determined by the perimeter of the hole 34.
  • Other possible shapes are oval, oblong, elliptical, or any other shapes with two or more contact points.
  • the use of a polygon-shaped crush element 32 reduces the contact surface area to two or more contact points with less contact surface area than the perimeter of a hole 34.
  • the sides of a polygon may determine the number of contact points between the crush element 32 and the hole 34.
  • FIGS. 5A and 5B are top and side views, respectively, of various embodiments of alternative crush element retention devices 31 for retaining the crush element 32 within a hole 34 of the exterior support structure 28.
  • the crush element retention device 31 may also be used for retaining the crush element 32 within a hole 34 of the interior support structure 30.
  • the crush element retention device 31 can be an insert 118 made of resilient material (e.g., silicone, rubber, polymer) having a plurality of fingers 120.
  • the fingers 120 are capable of deflecting outward and contacting an outer surface 122 of the crush elements 32 (see FIG. IB) to create frictional loads that may center and retain the crush element 32 within the hole 34 of the interior support structure 30.
  • Position A is the shape of the crush element retention device 31 before the crush element 32 is inserted within the insert 118.
  • Position B is the shape of the crush element retention device 31 after the crush element 32 is inserted within the insert 118. In this instance, the crush element 32 will lead to a deformation of the crush element retention device 31.
  • FIGS. 6A and 6B illustrate examples of inserts 118 for use with the hole 34 of the interior support structure 30 having a diameter 124 (see FIG. 5B).
  • each of the inserts 126, 128, 130 may have the same outer diameter OD relative to the diameter 124 of the hole 34.
  • the inserts 126, 128, 130 may have different inner diameters ID sized for the outer diameters OD of different crush elements 32 (see FIG. IB).
  • the outer diameter OD of the inserts 118 of the crush element retention device 31 may match the diameter 124 of the hole 34, but the inner diameter ID of the inserts 118 of the crush element retention device 31 may be adjusted as needed for housing different shapes and sizes of crush elements 32.
  • FIG. 6B illustrates another set of inserts 132, 134, 136 that can be configured with resilient, deformable material (e.g., rubber, polymer, silicone) having inner diameters ID being smaller than the diameter of the holes 34.
  • the inner diameters ID are also smaller than the outer diameter OD of the crush element 32 in forming an interference fit.
  • the interference fit can be sufficient for centering and retaining the crush element 32 within the hole 34.
  • the interference fit may also ease the removal of the crush element retention device 31 from the crush element 32.
  • FIG. 7 illustrates side views of alternative crush element retention devices 31 integrated with different sized crush elements 32.
  • each insert within the set of inserts 138, 140, 142 includes a resilient sleeve 144 capable of being integrated, respectively, with crush elements 146, 148, 150 in forming a single, integral member.
  • each crush member retention device 31 may be received within the diameter of the hole 34, and may be integrate with crush elements 146, 148, 150 having different sizes, hi other embodiments, the crush member retention device 31 may be customized to fit different shapes and sizes for accommodating the size of the hole 34 and the crush element 32. Furthermore, the crush member retention device 31 may also be integrated with a sleeve 144. [0091] FIG.
  • FIGS. 12A-12C are perspective views of an alternative embodiment of a crush element retention system having a retention sleeve 206 with a tapered inner diameter ID.
  • the opening inner diameter 208 of the crush element 32 may be greater than the outer diameter 210 of the crush element 32.
  • the inner diameter 212 at a bottom end 214 of the retention sleeve 206 may be less than the outer diameter 210 of the crush element 32.
  • the crush element 32 is capable of being received by the inner diameter ID of the retention sleeve 206 until the outer diameter 210 of the crush element 32 exceeds that of the inner diameter ID of the retention sleeve 206.
  • the crush element 32 can no longer travel down the interior 215 of the retention sleeve 206.
  • the tapering can be designed to retain crush elements 32 having different outer diameter OD 210 without being required to have matched retainers for each crush element 32.
  • FIGS. 13A and 13B are cross-section views of a crush retention system having a crush element 32 installed into an interior support structure 30 using another alternative crush element retention device 31.
  • the crush retention system includes a spring clamp 216 that deflects outward when a crush element 32 with an outer diameter OD 210 is greater than the relaxed diameter 218 (solid lines in FIG. 13A) of the spring clamp 216 that is insert therein.
  • the spring clamp 216 may have a maximum deflection diameter 220 (dotted lines in FIG. 13A) that may not be exceeded to assure the spring clamp 216 substantial returns to its relaxed position.
  • the blast energy absorption system 2 may deform to absorb the blast energy.
  • the understructure 10 and cross beam members 8 may bend and buckle inward.
  • the interior support structure 30 may buckle.
  • the crush elements 32 may be crushed.
  • the exterior support structure 28 may bend and buckle inward, hi some embodiments, longitudinal energy absorbing members 50 (if any) may buckle.
  • the floor structure 4 and the housing 6 may dampen the remaining energy with little or no plastic deformation.
  • all the components described above may be integrated into the chassis and/or frame of the vehicle 100 as shown in FIGS. 2A and 2B either directly (e.g., floor structures 4, housing 6) or indirectly (e.g., cross beam members 8, adjustable energy absorbing containers 9, understructure 10), and may either be connected by semi-permanent fastening techniques (e.g., welding or adhesive) or by re-attachable fastening techniques (e.g., screws, nuts/bolts), whereby the components are all contemplated as being capable of being removable either for repair or for varying the level of occupant protection.
  • dovetails/dovetail slots and hooks/latches are illustrated, any acceptable devices are contemplated with the scope of the disclosure and not intended to limit the disclosure to any one configuration.

Abstract

La présente invention concerne un système d'absorption (2) de l'énergie des souffles d'explosion pouvant s'intégrer à la structure d'un véhicule, et comportant des composants amovibles, interchangeables et configurables pouvant s'adapter de façon à configurer le véhicule en fonction des divers niveaux de menace des missions. Ce système d'absorption (2) de l'énergie des souffles d'explosion est constitué de plusieurs systèmes d'absorption d'énergie indépendants dans lesquels se combinent l'un ou plusieurs des éléments que sont la structure de plancher (4), un logement (6), des poutres transversales (8), des boîtes à absorption d'énergie réglables (9), et le cadre-plancher (10). Chaque composant peut être un système réagissant indépendant. L'intégration du jeu de relations entre les composants mentionnés donne un système qui absorbe et répartit l'énergie du souffle d'explosion de façon à réduire le plus possible le transfert d'énergie vers les occupants du véhicule. Ce système d'absorption (2) de l'énergie des souffles d'explosion permet l'adoption de nombreuses configurations adaptées au niveau de menace de la mission.
EP09812499A 2008-10-24 2009-10-26 Système d'absorption de l'énergie des souffles d'explosion Withdrawn EP2350556A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10816708P 2008-10-24 2008-10-24
PCT/US2009/062025 WO2010090661A1 (fr) 2008-10-24 2009-10-26 Système d'absorption de l'énergie des souffles d'explosion

Publications (1)

Publication Number Publication Date
EP2350556A1 true EP2350556A1 (fr) 2011-08-03

Family

ID=42167487

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09812499A Withdrawn EP2350556A1 (fr) 2008-10-24 2009-10-26 Système d'absorption de l'énergie des souffles d'explosion

Country Status (4)

Country Link
US (2) US20120186428A1 (fr)
EP (1) EP2350556A1 (fr)
AU (1) AU2009339276A1 (fr)
WO (1) WO2010090661A1 (fr)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090217811A1 (en) 2006-01-17 2009-09-03 David William Leeming Textile armour
WO2011018797A1 (fr) * 2009-08-11 2011-02-17 Sujoy Kumar Guha Véhicule apte à disperser la force et l’énergie d’une explosion
DE102010016605A1 (de) * 2010-04-23 2011-10-27 Krauss-Maffei Wegmann Gmbh & Co. Kg Bodenwanne eines Fahrzeugs, insbesondere eines gepanzerten militärischen Fahrzeugs, und Zusatzpanzerung für eine Bodenwanne
US8413567B2 (en) * 2010-06-23 2013-04-09 International Truck Intellectual Property Company, Llc Vehicle armor
IL207241A0 (en) 2010-07-26 2011-01-31 Plasan Sasa Ltd Belly armor
AU2011205221A1 (en) * 2010-08-09 2012-02-23 Plasan Sasa Ltd. Reinforcement system for a vehicle
US8616617B2 (en) * 2010-10-25 2013-12-31 BAE Systems Tactical Vehicle Systems L.P. Lightweight blast resistant armored cab for vehicles
US8640594B2 (en) * 2011-02-01 2014-02-04 Corvid Technologies, Inc. Blast deflecting shield for ground vehicles and shielded ground vehicles and methods including same
US9027458B2 (en) 2011-09-07 2015-05-12 Bae Systems Land & Armaments, L.P. Floating floor assembly for armored vehicles
US9045014B1 (en) 2012-03-26 2015-06-02 Oshkosh Defense, Llc Military vehicle
USD966958S1 (en) 2011-09-27 2022-10-18 Oshkosh Corporation Grille element
US9163910B2 (en) 2011-11-22 2015-10-20 Bae Systems Tactical Vehicle Systems Lp Armored cab for light tactical vehicles
US9038523B2 (en) * 2012-08-24 2015-05-26 International Truck Intellectual Property Company, Llc Vehicle floor
US8746741B2 (en) * 2012-11-14 2014-06-10 The United States Of America As Represented By The Secretary Of The Army Truncated V underbody protection enhancement
US8905164B1 (en) * 2013-03-20 2014-12-09 Us Government As Represented By The Secretary Of The Army Vehicle with sacrificial underbody structure
FR3005626B1 (fr) 2013-05-15 2016-11-11 Nexter Systems Caisse de vehicule blinde et structure de plancher pour une caisse de vehicule blinde
USD776003S1 (en) 2014-11-07 2017-01-10 The United States Of America As Represented By The Secretary Of The Army Light tactical vehicle hull
US9989333B2 (en) * 2014-11-20 2018-06-05 Mitsubishi Heavy Industries, Ltd. Armor and vehicle
US20180058820A1 (en) * 2016-08-24 2018-03-01 Pratt & Miller Engineering and Fabrication, Inc. Multiple layer hull
US10495419B1 (en) * 2017-04-27 2019-12-03 Oshkosh Defense, Llc Vehicle armor systems and methods
US20190310055A1 (en) * 2018-04-09 2019-10-10 Pratt & Miller Engineering and Fabrication, Inc. Blast deflector
FR3103548B1 (fr) * 2019-11-27 2023-04-14 Univ Toulouse 3 Paul Sabatier Dispositif de protection de structures statiques ou mobiles, terrestres, nautiques ou aériennes contre le souffle d’une explosion ou détonation et les projections de matière associées
CN112339676A (zh) * 2020-11-17 2021-02-09 重庆长安工业(集团)有限责任公司 车辆底部防爆炸冲击压溃吸能梁
US11313652B1 (en) 2021-02-25 2022-04-26 Government Of The United States, As Represented By The Secretary Of The Army Underbody kit
US11801904B2 (en) * 2021-11-16 2023-10-31 Textron Systems Corporation Techniques involving a modular vehicle belly armor kit
CN114577071A (zh) * 2022-03-31 2022-06-03 重庆望江工业有限公司 一种阈值熔断式车辆底部防地雷结构
EP4345409A1 (fr) 2022-09-30 2024-04-03 John Cockerill Defense SA Tourelle télé operée ayant un système de protection balistique dans la structure du toit et dans le sol

Family Cites Families (72)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4326445A (en) * 1980-03-19 1982-04-27 Cadillac Gage Company Armored underbody for road vehicle
US4398446A (en) * 1980-07-14 1983-08-16 The United States Of America As Represented By The Secretary Of The Army Adjustable combat vehicle armor
IL70914A (en) * 1984-02-09 1988-08-31 Israel State Elements for an add-on reactive armour for land vehicles
DE3931895A1 (de) * 1989-09-25 1994-12-15 Wegmann & Co Gmbh Einrichtung zur Anordnung von adaptierbaren Panzerungselementen an gegen Waffeneinwirkung zu schützenden Objekten, insbesondere an Kampffahrzeugen
DE69305944T2 (de) * 1992-09-16 1997-05-28 Fmc Corp Panzerung in Baukasten-Form
US5421238A (en) * 1993-07-26 1995-06-06 The United States Of America As Represented By The Secretary Of The Army Modular armor mounting system
AU6731294A (en) * 1993-07-28 1995-02-16 Foster-Miller Inc. Survivability enhancement
US5499568A (en) * 1994-05-18 1996-03-19 Fmc Corporation Modular protection system
US5533781A (en) * 1994-06-20 1996-07-09 O'gara-Hess & Eisenhardt Armoring Co., Inc. Armoring assembly
US5670734A (en) * 1994-10-05 1997-09-23 United Defense, L.P. Modular armor mounting system
IL113041A (en) * 1995-03-20 1997-11-20 Israel State Add-on armor securing means
US5705765A (en) * 1996-05-30 1998-01-06 United Defense, L.P. Passive roof armor
US5663520A (en) * 1996-06-04 1997-09-02 O'gara-Hess & Eisenhardt Armoring Co. Vehicle mine protection structure
US5747721A (en) * 1997-02-20 1998-05-05 Creative Aeronautical Accessories, Inc. Ballistic shield
DE19913845C2 (de) * 1999-03-26 2002-06-13 Henschel Wehrtechnik Gmbh Einrichtung zur Sicherung der Verfügbarkeit von militärischen Fahrzeugen
US6418832B1 (en) * 2000-04-26 2002-07-16 Pyramid Technologies International, Inc. Body armor
DE10117575A1 (de) * 2001-04-07 2002-10-10 Krauss Maffei Wegmann Gmbh & C Einrichtung zum Schutz der Besatzung eines militärischen Fahrzeugs bei Minenexplosion
DE10134394B4 (de) * 2001-07-14 2004-02-12 Rheinmetall Landsysteme Gmbh Minenschutzboden für ein Panzerfahrzeug
DE10250132B4 (de) * 2002-10-28 2007-10-31 Geke Technologie Gmbh Schutzmodul für gepanzerte Fahrzeuge
IL158045A (en) * 2003-09-22 2010-04-15 Cohen Michael Modular armored vehicle system including a combat vehicle chassis with openings and armored plates for covering the same
DE102004006819B4 (de) * 2004-02-11 2007-01-04 Rheinmetall Landsysteme Gmbh Fahrzeug mit Schutz gegen die Wirkung einer Landmine
AT413445B (de) * 2004-02-18 2006-02-15 Steyr Daimler Puch Ag Minengeschützte fahrzeugwannenbodenstruktur
US7695053B1 (en) * 2004-04-16 2010-04-13 Bae Systems Survivability Systems, Llc Lethal threat protection system for a vehicle and method
CA2595837A1 (fr) * 2004-12-08 2006-08-10 Armordynamics, Inc. Techniques et appareil de protection balistique
US8857311B2 (en) * 2004-12-08 2014-10-14 Armordynamics, Inc. Apparatus for providing protection from ballistic rounds, projectiles, fragments and explosives
US7401540B1 (en) * 2006-08-21 2008-07-22 Robert William Kocher Highly survivable urban utility vehicle (HSUUV)
EP1754949A1 (fr) * 2005-08-18 2007-02-21 Mowag GmbH Véhicule blindé
US7500422B2 (en) * 2005-12-16 2009-03-10 Robert Mazur Modular functional star-disc system
FR2897677B1 (fr) * 2006-02-17 2010-05-28 Giat Ind Sa Dispositif de protection d'un plancher de vehicule
US7631589B2 (en) * 2006-03-09 2009-12-15 Lockheed Martin Corporation Apparatus for inhibiting effects of an explosive blast
US7458306B2 (en) * 2006-04-10 2008-12-02 Bae Systems Land & Armaments L.P. External modular armor assembly
US7357062B2 (en) * 2006-04-11 2008-04-15 Force Protection Industries, Inc. Mine resistant armored vehicle
US20080173167A1 (en) * 2006-09-15 2008-07-24 Armor Holdings Vehicular based mine blast energy mitigation structure
US8047117B1 (en) * 2007-04-13 2011-11-01 Wright Materials Research Company Composite blast wave attenuators for boots
US7908959B2 (en) * 2007-07-05 2011-03-22 Pavon John J System and method for protecting vehicle occupants
US7997182B1 (en) * 2007-08-16 2011-08-16 Timothy J. Cox Protective hull for vehicles
IL186152A (en) * 2007-09-20 2014-04-30 Rafael Advanced Defense Sys Shielding module
WO2009102364A2 (fr) * 2007-11-16 2009-08-20 Bae Systems Tactical Vehicle Systems Lp Cabine blindée pour des véhicules
GB2469428B (en) * 2008-02-05 2012-11-07 Guy Leath Gettle Blast effect mitigating assembly using aerogels
IL196837A (en) * 2008-05-29 2014-12-31 Plasan Sasa Ltd An armored car passenger compartment
IL198881A (en) * 2008-05-29 2013-06-27 Plasan Sasa Ltd Ventral car system
FR2932556B1 (fr) * 2008-06-12 2014-09-12 Nexter Systems Dispositif de protection de plancher pour une cabine de vehicule
US7905540B2 (en) * 2008-07-24 2011-03-15 Alcoa Inc. Modular architecture for combat tactical vehicle
US8430196B2 (en) * 2008-12-29 2013-04-30 Hal-Tech Limited Deformable armored land vehicle
IL196456A0 (en) * 2009-01-12 2009-12-24 Shlomo Birger Uderbelly of armord vehicle
DE112010000809T5 (de) * 2009-01-21 2013-06-20 Rafael Advanced Defense Systems Ltd. Dämpfungsaufhängung mit der Möglichkeit zum Heben für ein Zusatz-Bewehrungssystem
US8418594B1 (en) * 2009-03-30 2013-04-16 The Boeing Company Blast load attenuation system for a vehicle
IL198017A (en) * 2009-04-05 2015-02-26 Rafael Advanced Defense Sys Means and method of protecting a fighter cell in a wheeled vehicle against explosives
US8033208B2 (en) * 2009-04-10 2011-10-11 Force Protection Technologies, Inc. Mine resistant armored vehicle
US8146478B2 (en) * 2009-04-10 2012-04-03 Force Protection Technologies, Inc. Mine resistant armored vehicle
US7987762B2 (en) * 2009-04-22 2011-08-02 Force Protection Technologies, Inc. Apparatus for defeating high energy projectiles
US8667880B1 (en) * 2009-05-12 2014-03-11 Granite Tactical Vehicles Inc. Cabin for a Humvee vehicle
IL199559A0 (en) * 2009-06-25 2011-08-01 Plasan Sasa Ltd Belly armor
IL202275A0 (en) * 2009-11-23 2010-11-30 Plasan Sasa Ltd A system for providing protection against an explosive threat
US8499677B2 (en) * 2009-11-30 2013-08-06 General Dynamics Land Systems—Canada Corporation W-shaped hull
FR2953586A1 (fr) * 2009-12-04 2011-06-10 Nexter Munitions Element de blindage pour une structure telle qu'un vehicule
US8146477B2 (en) * 2010-05-14 2012-04-03 Force Protection Technologies, Inc. System for protecting a vehicle from a mine
US20110307327A1 (en) * 2010-06-14 2011-12-15 Fair Isaac Corporation Optimization of consumer offerings using predictive analytics
US8413567B2 (en) * 2010-06-23 2013-04-09 International Truck Intellectual Property Company, Llc Vehicle armor
IL207241A0 (en) * 2010-07-26 2011-01-31 Plasan Sasa Ltd Belly armor
US8616617B2 (en) * 2010-10-25 2013-12-31 BAE Systems Tactical Vehicle Systems L.P. Lightweight blast resistant armored cab for vehicles
US8707848B2 (en) * 2010-12-01 2014-04-29 Ceradyne, Inc. V-shaped blast shield for protection against IEDs
US8424443B2 (en) * 2011-01-31 2013-04-23 The United States Of America As Represented By The Secretary Of The Army Vented armor V structure
US8943946B1 (en) * 2011-09-27 2015-02-03 Oshkosh Corporation Energy dissipation system for an armored vehicle having shear fingers and crushable sections
US20130111734A1 (en) * 2011-11-08 2013-05-09 Ceradyne, Inc. Method of attaching a blast shield to a space frame vehicle
CA2809605C (fr) * 2012-03-26 2018-12-04 Navistar Defense Engineering, Llc Dispositif de transfert de charge
US9097493B2 (en) * 2012-05-31 2015-08-04 Foster-Miller, Inc. Blast/impact mitigation shield
US9097494B2 (en) * 2012-05-31 2015-08-04 Foster-Miller, Inc. Blast/impact mitigation shield
US8770086B2 (en) * 2012-08-31 2014-07-08 International Truck Intellectual Property Company, Llc Blast protection attachment
US8746741B2 (en) * 2012-11-14 2014-06-10 The United States Of America As Represented By The Secretary Of The Army Truncated V underbody protection enhancement
US8826796B1 (en) * 2013-01-31 2014-09-09 The United States Of America As Represented By The Secretary Of The Army Tapered V underbody protection enhancement
IL224575A (en) * 2013-02-05 2014-01-30 Plasan Sasa Ltd Vehicle ventral system

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2010090661A1 *

Also Published As

Publication number Publication date
WO2010090661A1 (fr) 2010-08-12
US20120186428A1 (en) 2012-07-26
AU2009339276A1 (en) 2010-08-12
US20140318360A1 (en) 2014-10-30

Similar Documents

Publication Publication Date Title
US20140318360A1 (en) Blast energy absorption system
US6161462A (en) Bulletproof blanket for use with law enforcement vehicles such as police cars
US7533600B2 (en) Armor assembly for a truck
CA1326970C (fr) Magasin
US8356541B2 (en) Vehicle protective structure
US20110113952A1 (en) Apparatus and method for the protection of a vehicle from rocket-propelled grenades
US7270045B1 (en) System and method for induced acceleration mitigation for seat occupant
US5845831A (en) Detachable carrier for automobiles
US20140150633A1 (en) Removable blast protection
WO2006135704A1 (fr) Ensemble boucle a libération unique pour connecteurs de ceinture multiples
US7987788B2 (en) Dispenser arrangement for discharging countermeasure means
US20140060303A1 (en) Blast protection attachment
US8276795B1 (en) Modular ammunition restraint system for ambush protected vehicles
EP2332779B1 (fr) Caisse d'armes pour la fixation dans un véhicule automobile
US9423069B2 (en) Portable equipment system mount
US9347249B2 (en) Armored vehicle door release system
US20100043195A1 (en) Laminate armor system for police vehicle
US20090241318A1 (en) Laminate armor system for police vehicle
GB2107440A (en) Ejectable cluster ammunition
US7255059B1 (en) Adjustable adapter assembly
US9283882B1 (en) Convertible fighting vehicle
US20170350672A1 (en) Vehicle mounted firearm retention device
GB2479785A (en) Vehicle
CN210592442U (zh) 一种投弹装置
CN220750954U (zh) 物体固定装置及车辆

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20110523

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR

DAX Request for extension of the european patent (deleted)
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20130503