The Boeing Company

Robert L Carlsen

Richard Henry Bossi

Gary E Georgeson

Marc Rollo Matsen

Kay Youngdahl Blohowiak

Mark Alan Negley

Marc Joel Piehl

Stephen G Moore

Geoffrey Allen Butler

Robert A Anderson

Gregory Alan Foltz

Alan Edgar Landmann

Liam S Cavanaugh Pingree

John Mark Gardner

Hong Hue Tat

Michael D Fogarty

William Joseph Tapia

Liam S Pingree

An improved locking device comprising a lock body, a locking plug, and a plurality of tumblers, wherein the tumblers are restricted from moving with respect to the locking plug during the time frame that the locking plug is rotated with respect to the lock body.

Locking device and method

A method of forming a molybdenum composite hybrid laminate is disclosed. The method includes treating a surface of each of a plurality of molybdenum foil layers. The method further includes interweaving the surface treated molybdenum foil layers with a plurality of composite material layers. The method further includes bonding with an adhesive layer each of the surface treated molybdenum foil layers to adjacent composite material layers to form a molybdenum composite hybrid laminate having improved yield strength.

Molybdenum composite hybrid laminates and methods

A method and apparatus for evaluating an object having a wrinkle. Energy is sent into the object at a plurality of locations using an array of transmitting elements. Reflected energy is received at an array of receiving elements in response to a portion of the energy being reflected off a plurality of layers in the object. A three-dimensional model of the wrinkle in the object is created based on the reflected energy received at the array of receiving elements.

Quantification of wrinkles in composite objects

In an embodiment of the disclosure, there is provided a molybdenum composite hybrid laminate. The laminate has a plurality of composite material layers. The laminate further has a plurality of surface treated molybdenum foil layers interweaved between the composite material layers. The laminate further has a plurality of adhesive layers disposed between and bonding adjacent layers of the composite material layers and the molybdenum foil layers.

A method and apparatus are provided to identify unacceptable levels of porosity, microcracking or defects attributable to thermal damage. Ultrasonic signals are introduced into the workpiece, such as by means of an ultrasonic transmitter. The ultrasonic signals propagate along a predefined axis of propagation oriented at an offset angle relative to a predefined reference direction oriented normal to the workpiece. Backscattered signals are received, such as by an ultrasonic receiver, from the workpiece. A measure representative of the cumulative energy of the backscattered signals received over a predefined time interval is then determined, such as integration performed by a processing element. An anomalous response may then be detected based upon the measure representative of the cumulative energy of the backscattered signals. This anomalous response may be representative of at least a predefined amount of porosity, microcracking or thermal damage.

Method and apparatus for inspecting a workpiece with angularly offset ultrasonic signals

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Kent, WA, United States of America

Robert L Carlsen