The Boeing Company

Stephen N Provost

Dale M Pitt

Mark Joseph Clemen, Jr

Roger David Bernhardt

Donald V Drouin, Jr

Donald V Drouin Jr

Mark J Clemen

Donald V Drouin

Mark J Clemen Jr

A visual obscurant system for obscuring object from an observer having a field of view (FOV) is disclosed. The system comprises a sensor for detecting characteristics that indicate a presence of the object, a light source for emitting light in an electromagnetic spectrum, a source, and a controller. The source releases an obscurant into atmosphere to create a cloud. The obscurant attenuates a portion of the electromagnetic spectrum. The cloud is positioned within the FOV of the observer so as to obscure the object when the light emitted from the light source is directed towards the cloud. The controller is in communication with at least the sensor and the source. The controller modulates the light source at a frequency sufficient such that the observer interprets the light as being constant when energized.

System for visual obscuration of an object and dissipating energy of a laser weapon

A monitoring system for an aircraft which includes a laser secured to a fuselage of the aircraft and a laser beam target device secured to a wing of the aircraft, wherein the laser is positioned to emit a laser beam onto the laser beam target device for ascertaining a deflection of the wing. A method is also provided for sensing the deflection of a portion of a wing of an aircraft which includes the steps of emitting a laser beam from a laser secured to the fuselage of an aircraft and receiving the laser beam at a laser beam target device secured to a wing of the aircraft. The method further includes the step of transmitting location information of the position of the laser beam at the laser beam target device to a controller of a gimbal wherein the gimbal secures the laser to the fuselage of the aircraft.

Apparatus and method to detect aircraft wing deflection and twist during flight

A system which includes a first light beam locating sensor associated with a first position to be located on a wing of an aircraft. The first light beam locating sensor senses a first light beam at an identifiable position on the first light beam locating sensor. A processor is configured to receive a first signal from the first light beam locating sensor wherein the first signal includes a first identifiable position on the first light beam locating sensor. The processor is configured to determine a location of the first position on the wing and perform a first comparison of the location of the first position on the wing to a predetermined analyzed location of the first position on the wing.

System and method for correcting wing twist of an aircraft

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St. Louis, MO, United States of America

Stephen N Provost