| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 41 | Quick detachable gun supporting tripod | US67284657 | 1957-07-18 | US2906176A | 1959-09-29 | WALTON MUSSER C |
| 42 | Armored vehicle | US46570454 | 1954-10-29 | US2788713A | 1957-04-16 | GEORGES EVEN |
| 43 | Self-propelled rocket launcher | US61479845 | 1945-09-06 | US2566390A | 1951-09-04 | WEBER JR MATT J |
| 44 | Mobile missile launch system and method thereof | US13260731 | 2010-01-11 | US08800418B2 | 2014-08-12 | Siddalingappa Guruprasad; Shreedhar Aravind Katti; Alasani Prasad Goud; Vikas Narayan Waghmare; Sanjay Kumar; Atul Gupta; Ravindra Sudhakar Khire; Tushar Kant Santosh; Bimal Gautam; Paras Ram |
| The present invention relates to launching system, more particularly relates to mobile launching system for missiles. The mobile missile launch system comprising a vehicle (14) having a chassis structure adapted to carry the launch system; a mounting frame (16) comprising predetermined truss framework mounted onto the chassis structure; plurality of sliding mechanisms mounted at rear end of the mounting frame (16); plurality of canisters (43) mounted onto said beam (22) and plurality of missiles (11) ensconced within the canisters (43); plurality of containers (42) enclosing said canisters (43) and are connected to the saddles (32, 34) for linear movement; plurality of resting units (27) abutting to rear end of the canisters (43) and are adapted to move linearly to transfer reaction forces from said missiles (11) to ground. | ||||||
| 45 | Deformable Modular Armored Combat System | US13293271 | 2011-11-10 | US20120181100A1 | 2012-07-19 | Donald R. Halliday |
| A modular, wheeled military vehicle includes a driver module, an engine module, which form a central chassis module (CCM) that is adapted to receive the multipurpose pods on both sides and the rear of the CCM. The CCM and pods are generally V-shaped with slanted, upward extending sides to create multiple blast venting paths to deflect blast energy away from the vehicle occupants. These blast paths could consist of one or more chimneys through the vehicle further reducing occupant exposure to blast energy. For example, the engine module, and front and rear tractive units, can be manufactured with an open framework, allowing significant under vehicle blast venting between the modules and pods, through the engine module, and forward, rearward and to the sides of the vehicle; thereby increasing survivability of the crew. The pods can be designed to rotate and/or be frangible to increase the blast-venting path through the vehicle. | ||||||
| 46 | Launch tube deployable surveillance and reconnaissance system | US12799297 | 2010-04-21 | US20110168838A1 | 2011-07-14 | William Hornback; Michael Holly |
| An unmanned aerial surveillance and reconnaissance system are disclosed wherein an unmanned aerial vehicle is launchable from a launch tube, for instance, the bore of an existing weapons system mounted on a mobile vehicle, such as a weapon barrel of a tank or armored combat vehicle and which the launch may be remotely initiated from the protected armored compartment of the mobile vehicle. | ||||||
| 47 | MOBILE CARRIER FOR A PROJECTILE LAUNCHER | US11475380 | 2006-06-27 | US20100095831A1 | 2010-04-22 | Ehud Dekel |
| A mobile projectile launcher is disclosed having a tiltable launching platform for supporting a plurality of canisters in each of which projectiles to be launched are stored and fired, a support plate pivotally connected to a horizontal cargo bed, and at least one linear actuator by which the support plate is swingable from a closed position substantially perpendicular to the cargo bed to an open position substantially parallel to the cargo bed. The support plate is made of a material that is resistant to the projectile plume following launching and is sufficiently sturdy to support a technician during the loading of projectiles when set in an open position, yet is adapted to protect and hide the loaded canisters when set in a closed position. | ||||||
| 48 | Multiple tube pneumatic launcher | US10503625 | 2004-03-29 | US07089843B2 | 2006-08-15 | Stephen W. Miller; Steven J. Fox; David M. Feild; Richard A. Bauernschub; Justin A. Mettee |
| A launcher includes a plurality of launch tubes for stowing and launching a plurality of air vehicles. A central air manifold is operatively connected to an air storage tank; a first launch tube air manifold is operatively connected to a first group of the launch tubes and operatively connected to the central air manifold. The first launch tube air manifold has a separate port corresponding to each launch tube of the first group of launch tubes. A release valve mechanism is removably mounted in one of the ports of the first launch tube air manifold, the release valve mechanism controlling the passage of launch air between the first launch tube air manifold and the launch tube corresponding to the port in which the release valve mechanism is mounted. A plug is removably mounted in each of the ports not occupied by the release valve mechanism. | ||||||
| 49 | Multi-purpose missile launcher system for a military land vehicle | US10316476 | 2002-12-11 | US20030089220A1 | 2003-05-15 | David R. Boudreau; Stan Bovee; Philip Matterson; Bruce Gaedke; Dennis Borgwarth |
| A multi-purpose missile launcher system for a military land vehicle that has the capability for direct targeting both short and medium range land targets, as well launching missiles against longer-range land targets or air targets using indirect targeting. The multi-purpose missile launcher system is deployed as part of a modular weapon system that mates with a modular bed of the military land vehicle. | ||||||
| 50 | Elevating system | US66526 | 1993-05-24 | US5465808A | 1995-11-14 | Robert G. Musgrove |
| An elevating system elevates a payload platform between a first position and a second position, such elevating system having a stowed position, an operational position, and a fully-deployed position. The elevating system includes an extendable actuator rod pivotably mounted on a frame and a link pivotably mounted to the extendable actuator rod and pivotably mounted to the payload platform. The extendable actuator rod and the link are moved from the stowed position to the operational position by increasing the length of the extendable actuator rod from a first length to a second length. The extendable actuator rod and the link are moved from the operational position to the fully-deployed position by increasing the length of the extendable actuator rod from the second length to a third length. The extendable actuator rod and the link elevate the payload platform from the first position to the second position as the extendable actuator rod and link are moved from the operational position to the fully deployed position. | ||||||
| 51 | Missile trans porter-launcher | US595190 | 1975-07-11 | US3981224A | 1976-09-21 | Chester W. Byars; Edgar L. Van Cott; Clifton F. Orchard |
| A launcher carried on the flatbed of a mobile vehicle to provide the dual le of missile transporter and pre-launch positioning of its multi-missile payload. The launcher is not trainable in azimuth or elevation. When emplaced the launcher carriage erects the missiles to substantially a 75.degree. launch angle and a missile is fired from a combination launch tube shipping container by a small propellant charge and uses its own control to put it on the proper trajectory. Missile motor ignition is delayed for a predetermined time after launch. | ||||||
| 52 | Mobile anti-aircraft device | US418615 | 1973-11-23 | US3946640A | 1976-03-30 | Emil Baumann |
| A mobile anti-aircraft weapon incorporating a housing rotatable about a substantially vertical axis with respect to the chassis of a support vehicle. The housing is equipped with side doors which can be pivoted about hinges and a respective rocket launcher accommodating a plurality of rockets mounted at the outside of each side door and serving as weapons. | ||||||
| 53 | Rocket launcher mount | US41861673 | 1973-11-23 | US3895557A | 1975-07-22 | BAUMANN EMIL |
| A mobile rocket launcher mount equipped for travel and firing operations wherein two rocket launchers, each accommodating a plurality of rockets, and driven to be pivotable about a respective horizontal pivot axis are mounted at the outside of a respective side door of a substantially box-like housing, and which side doors are pivotable about substantially vertical axis hinges. The housing, in which there are accommodated one or more seats and actuation devices for the operating personnel and equipped with observation- and target tracking devices, is mounted as a unit so as to be rotatable about a vertical axis of rotation at the mount chassis.
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| 54 | Vehicle mounted projector for jetpropelled guided missiles with adjustable angle of elevation | US3446112D | 1967-08-02 | US3446112A | 1969-05-27 | PLANITZER ERICH; MAUS EICKE; MULTERER ALBERT; SCHOBER ERWIN; SCHINDLER WERNER |
| 55 | Rocket launching | US52109566 | 1966-01-17 | US3379097A | 1968-04-23 | THOBY FISHER WILLIAM |
| 56 | Launching device | US43354765 | 1965-02-16 | US3319522A | 1967-05-16 | GOULD BERT B; BIEHL ARTHUR T |
| 57 | Missile transporter-launcher | US7201560 | 1960-11-28 | US3106864A | 1963-10-15 | SEEDLOCK WALTER F; GURSKIS JR JOSEPH; COOMBS LESLIE C; BUCKMAN THOMAS P |
| 58 | Wheeled gun carriage | US80121359 | 1959-03-23 | US3023674A | 1962-03-06 | EMANUEL SUNDSTROM JOHN NILS |
| 59 | Carriage for a mobile missile mount | US42505654 | 1954-04-22 | US2977857A | 1961-04-04 | CARLBERG ROBERT E |
| 60 | Combination dolly-launcher for missiles | US81018659 | 1959-04-30 | US2949823A | 1960-08-23 | ROSS WILLIAM J; WALKER WILLIAM A |
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