Bizarre Patents
Dining Table Having Integral Dishwasher
A space-saving dishwasher, which may be installed within a counter top or table, having a dish-carrying rack that is vertically shiftable through the open top of the dishwasher for facilitating loading and unloading of the dishes.
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| Number | Title | Issue Date |
| 7679037 | Personal rifle-launched reconnaisance system A reconnaissance system includes a projectile having an opening through which images of a target area are acquired, a portable launcher having a mechanism for affixing the launcher to a rifle for launching the projectile to fly along and above the target area, an im... | 03/16/2010 |
| 7671311 | Gimbal system with airflow Systems, including apparatus and methods, for driving airflow along a surface of a gimbal. The systems may comprise a gimbal apparatus including a payload and also including a gimbal mount supporting a first gimbal and a second gimbal. The first gimbal may be couple... | 03/02/2010 |
| 7645969 | Low voltage device for the generation of plasma discharge to operate a supersonic or hypersonic apparatus A method, device, and projectile having a device for guiding or piloting projectiles or missiles (self-propelled or non-self-propelled), to deflect, in a direction Y, a hypervelocity projectile operating in a gas, such as a shell, a bullet, or a missile, having a no... | 01/12/2010 |
| 7582853 | Method and device for producing an optical link using light flashes The invention relates to a method and device for producing an optical link using light flashes. According to the invention, an arrangement (13) comprising a plurality of capacitors (C1 to C5) is provided in order to power a flash lamp (3)... | 09/01/2009 |
| 7550697 | Systems and methods for boresight adapters Boresighting systems and methods are disclosed. In one embodiment, an assembly adapted for boresighting a launch system includes first and second elongated members adapted to be coupled to the launch system. First and second alignment members are coupled to and exte... | 06/23/2009 |
| 7547865 | Optical element mount and method thereof for a gun-launched projectile An optical element mount is effective in high G environments to protect brittle optical elements in which tensile stresses are generated on surface S2 without degrading optical performance. A flexible spacer formed of a relatively low-stiffness material suppo... | 06/16/2009 |
| 7541563 | Magnetic gyro-projectile device with electronic combustion, turbogeneration and gyro stabilization A hollow cylinder has an electromagnet to hold back a canister and either an induction heating linear actuator or a firing pin to ignite the primer-containing combustive material inside the canister to eject a locked piston from the cylinder. There is a motor-includ... | 06/02/2009 |
| 7521655 | Method and system of automatic control A method and apparatus for protecting a civil aircraft from missiles with infrared seeker heads includes detecting a launch of a missile from a location of launch, the missile having an infrared seeker head with an infrared sensitivity range, a power and an operatio... | 04/21/2009 |
| 7511252 | Multihypothesis threat missile propagator for boost-phase missile defense A fire control system for a boost phase threat missile includes sensors for generating target-missile representative signals, and a multi-hypothesis track filter, which estimates the states of various target hypotheses. The estimated states are typed to generate hyp... | 03/31/2009 |
| 7495198 | System and method for improving nighttime visual awareness of a pilot flying an aircraft carrying at least one air-to-air missile A method for improving nighttime visual awareness of a pilot flying an aircraft carrying an air-to-air missile including one or more one gimbaled imaging sensor. The method includes providing a helmet for the pilot, a helmet tracking system for determining the attit... | 02/24/2009 |
| 7473876 | Boost phase intercept missile fire control system architecture A fire control system for a boost phase threat missile includes sensors for generating target-missile representative signals, and a multi-hypothesis track filter, which estimates the states of various target hypotheses. The estimated states are typed to generate hyp... | 01/06/2009 |
| 7446291 | Augmented proportional navigation guidance law using angular acceleration measurements A method guides an interceptor missile toward an accelerating target. The method sets up a line-of-sight between the interceptor and the target, and monitors the acceleration of the angle of the line-of-sight. The acceleration is multiplied by a gain factor dependen... | 11/04/2008 |
| 7434762 | Retractable thrust vector control vane system and method A retractable thrust vector control system (10) for a rocket motor (26) that can generate an exhaust plume comprises at least one control vane (12) connectable to an attitude control assembly (20) that rotates the vane (12) about a... | 10/14/2008 |
| 7431237 | Guided projectile with power and control mechanism A projectile has the ability to generate and provide power to components located in two sections of the projectile which have relative rotation to each other. The projectile has a pair of generators allowing the powering of components in two sections. The projectile... | 10/07/2008 |
| 7425918 | System and method for the measurement of full relative position and orientation of objects Methods are provided where: a signal is transmitted from an illuminating source and received cavity waveguides disposed on an object; a position and/or orientation of the object is determined based on the signal received in the waveguides; and data representing the ... | 09/16/2008 |
| 7425693 | Spectral tracking A method of tracking a target. The method includes the steps of acquiring a first spectral image of a scene that includes the target, designating a spectral reference window, in the first spectral image, that includes a respective plurality of pixel vectors, acquiri... | 09/16/2008 |
| 7423245 | Nose cover A nose cover (10) for a dome (12) through which radiation can pass, for a missile, the nose cover having an outer structure (22) through which radiation can pass and which is aerodynamically better than a spherical shape, and having correction o... | 09/09/2008 |
| 7422175 | Apparatus and method for cooperative multi target tracking and interception The invention described herein provides an apparatus and a method to cooperatively track and intercept a plurality of highly maneuvering asymmetric threats using networks of small, low-cost, lightweight, airborne vehicles that dynamically self-organize into an ad ho... | 09/09/2008 |
| 7416154 | Trajectory correction kit The Trajectory Correction Kit (TCK) is a completely self-contained retrofit kit that is externally and fixedly mounted as an add-on to the rear (aft of the tailfins) of an existing, unguided rocket. The TCK continuously measures the pitch and yaw of the rocket as it... | 08/26/2008 |
| 7412930 | Frictional roll control apparatus for a spinning projectile The invention relates generally to a roll damping apparatus for a spinning projectile having a first section and a second section rotatably attached about a roll axis. The roll damping apparatus comprises a first portion attached to the front section, and a second p... | 08/19/2008 |
| 7410119 | Rotating missile emitting light pulses The invention concerns a rotating missile emitting light pulses. The invention is characterized in that means are provided to interrupt said light pulses (5) when the rotational movement (3) of the missile (2) about its longitudinal axis (L-L) s... | 08/12/2008 |
| 7400289 | Plume-to-hardbody offset compensation in boosting missiles A methodology determines the offset distance between a threat missile plume and its hardbody during boost phase to aid in guiding a kinetic weapon (KW) or interceptor missile to the threat missile hardbody using the KW infrared sensor of the interceptor missile in c... | 07/15/2008 |
| 7400287 | Smart chaff Missile deflector systems for protecting a vehicle from threats that use an infrared sensor for guidance are disclosed. An exemplary missile deflector system can include, for example, a radiation source and one or more deployable smart chaff elements. The light sour... | 07/15/2008 |
| 7395987 | Apparatus and appertaining method for upfinding in spinning projectiles using a phase-lock-loop or correlator mechanism The invention relates to the field of gun-launched guidance systems and to a navigation system based on inertial sensors mounted in a spinning projectile using at least one rotation sensing device with input components perpendicular to the spinning body's longitudin... | 07/08/2008 |
| 7394046 | Tracking of a moving object A system for determination of kinematics of a moving object comprising: a sensor producing angular data for the object at a number of observation times, a state initialization unit, receiving angular data from the sensor and on basis thereof determining a first kine... | 07/01/2008 |
| 7394047 | Interceptor guidance for boost-phase missile defense A fire control system for a boost phase threat missile includes sensors for generating target-missile representative signals, and a multi-hypothesis track filter, which estimates the states of various target hypotheses. The estimated states are typed to generate hyp... | 07/01/2008 |
| 7378626 | Directed infrared countermeasures (DIRCM) system and method An agile, high-power, reliable DIRCM system that is easily extended to address sophisticated UV or UV-visible capable multi-band threats includes a missile warner having missile warning receivers (MWRs), one or two-color suitably in the mid-IR range, that detect lik... | 05/27/2008 |
| 7367525 | Munition with integrity gated go/no-go decision A munition is presented which includes an integrity verification system that measures the integrity of the munition. When an integrity threshold is not met, engagement of the munition with a predetermined target is aborted. Also presented is a methodology for gating... | 05/06/2008 |
| 7354017 | Projectile trajectory control system Trajectory is controlled by a control system having fins that de-spin a section of the control system relative to a projectile or missile. The control system also includes aero-surfaces that produce a lift when brought to rotation speed of about 0 Hz relative to a r... | 04/08/2008 |
| 7350744 | System for changing warhead's trajectory to avoid interception A system for increasing a warhead's chance of hitting a target comprises a system for causing the warhead to deviate from its projected trajectory so that it will have an increased chance of avoiding intercepting force such as a kill vehicle a missile, an airplane, ... | 04/01/2008 |
| 7353090 | System, bus monitor assembly and method of monitoring at least one data bus of an aircraft A system is provided for monitoring at least one data bus of an aircraft. The system includes an aircraft adapted to control the operation of stores of a second predetermined type (e.g., Harpoon Block I missiles). However, the aircraft is also capable of carrying a ... | 04/01/2008 |
| 7347147 | Braking device for a trajectory-correctable spin-stabilized artillery projectile In order to move a textile braking element (16) which is in the form of an annular disk and which is deployed radially under the effect of centrifugal force rapidly into a contour which is stable in respect of shape and which is always properly defined even u... | 03/25/2008 |
| 7348918 | Mobile ballistic missile detection and defense system The present invention is directed towards a ballistic missile detection and defense system. The system of the present invention comprises a ship based interceptor or antiballistic missile, a missile launch detection and tracking system, and a signal processing syste... | 03/25/2008 |
| 7345265 | Enhancement of aimpoint in simulated training systems Embodiments of the invention, therefore, provide improved systems and methods for tracking targets in a simulation environment. Merely by way of example, an exemplary embodiment provides a reflected laser target tracking system that tracks a target with a video came... | 03/18/2008 |
| 7341221 | Attitude determination with magnetometers for gun-launched munitions A system and method for performing attitude determination for projectiles comprises a projectile; a plurality of magnetometers arranged orthogonally to one another in the projectile, wherein the plurality of magnetometers are adapted to take first flight vector meas... | 03/11/2008 |
| 7338009 | Apparatus and method for cooperative multi target tracking and interception The invention described herein provides an apparatus and a method to cooperatively track and intercept a plurality of highly maneuvering asymmetric threats using networks of small, low-cost, lightweight, airborne vehicles that dynamically self-organize into an ad ho... | 03/04/2008 |
| 7339537 | Capacitive drive antenna and an air vehicle so equipped Disclosed are antenna embodiments and air vehicles so equipped that include a first antenna component, and a second antenna component, separated by a free space gap, where the antenna embodiments are adapted to capacitively couple the first antenna component and the... | 03/04/2008 |
| 7335865 | Dome The present invention relates to process for producing a transparent missile dome having a spanning angle larger than 180°, comprising the step of: (a) growing from single crystals of a ceramic material a first dome portion, said first dome portion being a portion ... | 02/26/2008 |
| 7333044 | Rocket-powered sensor target assembly A rocket tube for housing a reloadable rocket motor is connected to a spacer element and a wire-rider element. A sensor target for reflecting radar signals is screwably attached to the rocket tube. The sensor target is provided with a plug for effectively sealing on... | 02/19/2008 |
| 7328644 | System and method for intercepting a projectile A system has a containment blanket. The system further has a launcher configured to launch the containment blanket and logic configured to deploy the containment blanket. The containment blanket is configured to encompass an incoming projectile. ... | 02/12/2008 |