Launcher Movable Relative To Storage Means Patents (Class 89/1.802)
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Patent number: 9878762Abstract: A system for launching and recovering an underwater vehicle (18), which system comprises a crane (16) and a storage location for at least one underwater vehicle (18), wherein the crane (16) is attached to the bottom of a first container (12) and the storage location is provided in a second container (14), said first container (12) being arranged on the second container (14) during an operation of launching or an operation of recovering.Type: GrantFiled: March 23, 2016Date of Patent: January 30, 2018Assignee: Fraunhofer-Gesellschaft zur Foerderung der angewandten Forschung e. V.Inventors: Torsten Pfuetzenreuter, Thomas Rauschenbach, Gunnar Brink
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Patent number: 9157717Abstract: Systems, a ballistic device, and methods of use are provided herein. The system includes at least one first ballistic device having a first payload configured to detonate, and a second ballistic device configured to track at least one of a position and a movement of an object, and enable the at least one first ballistic device to identify at least one of the position and the movement of the object. The second ballistic device includes a second payload configured to detonate.Type: GrantFiled: January 22, 2013Date of Patent: October 13, 2015Assignee: The Boeing CompanyInventors: Galen Duff Carroll, Eric M. Greuner
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Patent number: 8297165Abstract: Apparatuses, vehicles, and methods to reduce loads applied to a store when the store is launched from the vehicle are disclosed. A particular apparatus includes a launch chamber and a flap. The launch chamber has a first portion configured to receive a store. A second portion is configured to be positioned over an opening in a hull of a vehicle. The chamber has a forward end and an aft end. The flap is positioned a distance from the aft end of the launch chamber. The flap has a first end rotatably mounted proximate to the first portion of the launch chamber and has a second end extending toward the second portion of the launch chamber. The flap is configured to rotate about the first end when the store impacts the flap due to the forces applied to the store by the fluid when the store is launched.Type: GrantFiled: January 21, 2011Date of Patent: October 30, 2012Assignee: The Boeing CompanyInventor: Matt H. Travis
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Patent number: 7905169Abstract: Stores launch tubes and vehicles equipped with stores launch tubes are disclosed. According to a particular illustrative example, a stores launch tube includes a tube member and a flexible seal. The flexible seal couples an exterior of the tube member to a hull. The flexible seal acts as a pressure barrier against an ambient environment.Type: GrantFiled: August 27, 2009Date of Patent: March 15, 2011Assignee: The Boeing CompanyInventor: Matt H. Travis
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Patent number: 7597038Abstract: An exemplary stores launch tube includes an outer tube and an inner tube. The inner tube is disposed interior the outer tube and is configured to reduce load as a store exits therefrom. The inner tube may be made of a flexible material. At least one load-reducing device may be disposed between the inner tube and the outer tube. The inner tube may be received within a canister that has an outer casing that is attachable to the outer tube. Alternately, the inner tube may be attached directly to the outer tube. The inner tube may include more than one tube section. If desired, filler material, such as foam, may be disposed between the inner tube and the outer tube. The outer tube may have a substantially circular cross-section, or an oval cross-section, or any cross-section as desired to accommodate structural considerations.Type: GrantFiled: January 31, 2007Date of Patent: October 6, 2009Assignee: The Boeing CompanyInventor: Matt H. Travis
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Publication number: 20060086241Abstract: 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.Type: ApplicationFiled: March 29, 2004Publication date: April 27, 2006Inventors: Stephen Miller, Steven Fox, David Feild, Richard Bauernschub, Justin Mettee
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Patent number: 7032493Abstract: A rocket launcher system and a method for controlling a rocket launcher system. The rocket launcher system is placed below deck on a ship to improve the ship's stealth capability and includes a launcher, a charger and a magazine containing one or more different types of rocket missiles. According to the method for controlling the rocket launcher system, an operating signal including preparation data is transferred to the rocket launcher system from one or more operators. The preparation data is transferred to a rocket missile and a charger takes the rocket missile from a magazine and charges a launcher. A hatch in the ship's deck is opened, and the launcher sights the rocket missile at a target area.Type: GrantFiled: December 7, 2001Date of Patent: April 25, 2006Assignee: Forsvarets MaterielverkInventor: Dean Fowler
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Patent number: 6382072Abstract: A support and alignment assembly for use on a moving vehicle having a fixed receiver mounted thereon. The assembly comprises a support assembly including (i) a loading tray for supporting a missile, (ii) a storage structure for supporting the loading tray, and (iii) mounts resiliently connecting the storage structure to the vehicle.Type: GrantFiled: October 1, 2001Date of Patent: May 7, 2002Assignee: The United States of America as represented by the Secretary of the NavyInventor: Jeffrey L. Cipolla