Abstract: An armor blast shield for use on the bottom of a vehicle to protect occupants of the vehicle from improvised explosive devices. A preferred embodiment is configured in a V-shaped configuration formed by at least two planar blast resistant panels and an I-beam having channels with inclined walls which receive the panels at an obtuse angle. The panels are adhesively adhered to the I-beam channel walls and at least one bolt is secured through the I-beam and a panel to provide superior blast resistant performance as compared to welded panels.
Type:
Grant
Filed:
December 1, 2010
Date of Patent:
April 29, 2014
Assignee:
Ceradyne, Inc.
Inventors:
Richard L. Allor, Thomas J. Husak, Dainius E. Skiotys
Abstract: A novel fire control system for a bolt action firearm includes a firing pin sear located and controlled at one side of the forward end of the bolt. The sear configuration is optimum for rifles having a bullpup form. The location of the sear also provides clearance under the bolt for the bolt to be moved over a firearm magazine without interference with cartridges in the magazine.
Abstract: Systems and methods for transferring power through an aircraft window and thereby powering temporary externally mounted equipment, such as flight test instrumentation, without cutting or drilling holes in the airplane to run wire for a flight test or experiment. One embodiment uses a light source and a photovoltaic cell to transfer power from inside to outside the aircraft. Another embodiment uses an RF source and a rectenna to transfer power from inside to outside the aircraft.
Type:
Grant
Filed:
August 21, 2009
Date of Patent:
March 18, 2014
Assignee:
The Boeing Company
Inventors:
Brian J. Tillotson, Michael A. Loudiana
Abstract: A rifling angle calculating method according to the present invention expands a rifling angle by combining a Fourier function and a polynomial function to take only the advantages of the two functions, and thus boundary conditions at the start and end points of the rifling angle may be faithfully satisfied, and an optimum rifling angle for minimizing the maximum rifling force may be calculated.
Type:
Grant
Filed:
January 26, 2012
Date of Patent:
January 28, 2014
Assignee:
Agency for Defense Development
Inventors:
Ki Up Cha, Young Hyun Lee, Chang Ki Cho
Abstract: Weapons, weapon housing and methods of producing such weapons and weapon housings are disclosed. An example weapon housing for use with a firearm includes at least two housing shells. Each of the housing shells comprises at least one positioning recess. The example weapon housing also includes at least one connection block comprising connecting pins. On an assembly plane of the connection block, the housing shells are to be positioned and aligned on the connecting pins via the respective positioning recess to enable forces that are to act in or against a direction of fire to be absorbed by surfaces of at least one of the positioning recesses or one or more of the connecting pins.
Abstract: An air path and improved safety valve combination for toy air guns including a housing in the shape of a gun, multiple barrels mounted to the housing, a piston, cylinder and spring combination for generating blasts of compressed air mounted to the housing, an air passageway structure with an air path channel mounted in the housing, and multiple valve elements movable in the air path channel between open rearward positions and closed forward positions. When in the rearward position, each valve element directs a blast of compressed air to an associated barrel because the barrel is loaded with a soft foam dart of proper shape. When the valve element is in a forward position indicating an empty barrel, the valve element causes the blasts of compressed air to cascade to the next valve element of a dart-loaded barrel in sequence and in a very efficient manner.
Abstract: A method and apparatus for managing a flight control surface system. A leading edge section on a wing of an aircraft is extended into a deployed position. A deformable section connects the leading edge section to a trailing section. The deformable section changes from a deformed shape to an original shape when the leading edge section is moved into the deployed position. The leading edge section on the wing is moved from the deployed position to an undeployed position. The deformable section changes to the deformed shape inside of the wing.
Type:
Grant
Filed:
July 17, 2009
Date of Patent:
September 17, 2013
Assignee:
The Boeing Company
Inventors:
Dale M. Pitt, Nicholas Stephen Eckstein
Abstract: A clamp used to attach a flashlight to a firearm having a rail thereon. In the preferred embodiment, the clamp utilizes a sleeve configured to accept a handle of the flashlight. The sleeve has at least one tooth configured to engage the rail on the firearm. A wedge is movably secured to the sleeve such that a simultaneous action by the operator both forces the wedge up a ramp on an interior aspect of the clamp and secures the clamp by compressing the rail between a bracket (which engages both the clamp and the rail) and the tooth on the sleeve.
Type:
Grant
Filed:
November 2, 2011
Date of Patent:
July 23, 2013
Assignee:
Abrams Airborne Manufacturing Inc.
Inventors:
Eric Stephen Kincel, Christopher James Hendryk
Abstract: A system and method for disrupting at least one component of a suspect object is provided. The system includes a source for passing radiation through the suspect object, a screen for receiving the radiation passing through the suspect object and generating at least one image therefrom, a weapon having a discharge deployable therefrom, and a targeting unit. The targeting unit displays the image(s) of the suspect object and aims the weapon at a disruption point on the displayed image such that the weapon may be positioned to deploy the discharge at the disruption point whereby the suspect object is disabled.
Type:
Grant
Filed:
October 26, 2010
Date of Patent:
July 9, 2013
Assignee:
Sandia Corporation
Inventors:
T. Scott Gladwell, Justin R. Garretson, Clinton G. Hobart, Mark J. Monda
Abstract: Breech guides for use with breech assemblies and firearms including such breech guides are disclosed. An example breech guide for use with a breech assembly of a firearm includes a support element positioned within the breech assembly and a control element on the support element, the control element is adapted to control a cartridge-feeder mechanism of the firearm. The example breech guide includes a guide element on the support element. The guide element is adapted to guide the breech assembly relative to guide rails of the firearm. The support element extends along an axis of symmetry substantially perpendicular to a bore axis. The control element and the guide element being substantially coaxially positioned relative to the axis of symmetry.
Abstract: A cartridge gas port selector mechanism for a firearm barrel having a plurality of gas ports extending from the barrel bore and having a gas block with gas passages in communication with a gas tube. A selector valve member is movable within the gas block between an open condition permitting flow of cartridge gas from one or more ports of the firearm barrel to the cartridge gas passage and a closed condition blocking flow of cartridge gas from the barrel bore to the cartridge gas passage. A valve selector or actuator is connected with the valve member and is selectively moveable to position the valve member at the open condition or the closed condition to select the volume and timing of cartridge gas communication from the barrel bore to the gas energized autoloading mechanism of the firearm.
Abstract: A method for assembling a cabin window to a bay in a side wall of an aircraft fuselage, where the cabin window including an outer transparent element and at least one inner transparent element, includes making a non-through hole in a portion of the side wall. The outer transparent element includes a first part having a diameter greater than that of the bay and which is shaped to co-operate with the portion of the side wall to block the outer transparent element in the bay both laterally and longitudinally. A second part of the outer transparent element has a groove that projects into the fuselage. The outer transparent element and the at least one inner transparent element are welded to the fuselage using a strap which presses a seal against at least the fuselage and the inner wall of the groove.
Type:
Grant
Filed:
January 3, 2008
Date of Patent:
February 12, 2013
Assignee:
Airbus Operations SAS
Inventors:
Guillaume Gallant, Damien Aguera, Philippe Bernadet