The Boeing Company

Ordie Dean Butterfield

Jonathan Martin Saint Clair

David Christien Soreide

James Henry Mabe

Manny S Urcia

Lixin Cai

Alec Adams

Mitchell D Voth

Bentley Edwin Northon

Christopher M La Fata

Jonathan Kenji Brown

Robert Roland Keever

Stephen T Tyahla

John G Castagno

Jeffrey H Hunt

David Arthur Whelan

Frederick Theodore Calkins

Robert Paul Higgins

Glenn Scott Bushnell

Robert W Turner

Robert T Ruggeri

William D Sherman

Stefan Richard Bieniawski

Ian M Gunter

Darin J Arbogast

Stephen A Walls

Ronald N Murata

James Ridgeway Gillis

Robert Griffiths

Grant Joseph Atkinson

Jacklyn Ann Holmes

Frank Bruce Irvine

Daniel Morgenroth

Jonathan M St Clair

Systems, methods, and apparatus for an electromagnetic (EM) panel are disclosed. In one or more embodiments, a disclosed electromagnetic (EM) panel comprises an outer skin, an inner skin, a core disposed between the outer skin and the inner skin, and at least one receiver to receive at least one first signal. In at least one embodiment, at least one receiver is disposed within an opening on the outer skin of the EM panel. At least one receiver is an optical sensor(s) and/or a radio frequency (RF) antenna(s). In one or more embodiments, the EM panel further comprises at least one transmitter to transmit at least one second signal. In at least one embodiment, at least one transmitter is disposed within an opening on the outer skin of the EM panel. At least one transmitter is a laser(s) and/or a RF antenna(s).

Conformal load bearing distributed sensing arrays

A method and apparatus for shaping fuselage sections. A first fuselage section is held in a holding structure in a cradle in a cradle system. Force are applied to the first fuselage section with an actuator system to a portion of the first fuselage section such that a first current shape of the first fuselage section changes towards a first desired shape for the first fuselage section to join the first the fuselage section to a second fuselage section.

Cradle system for shaping fuselage sections

A method and apparatus comprising a group of passive sensor systems, an active sensor system, and a processor unit. The group of passive sensor systems is configured to generate first sensor information from light in an environment around the group of passive sensor systems. The active sensor system is configured to send signals, receive responses from the signals, and generate second sensor information from the responses. The processor unit is configured to control the active sensor system to send the signals in a direction toward an object using the first sensor information and generate information about the object using the second sensor information.

Object detection system for mobile platforms

Within examples, remotely controlled and thermally managed systems for actuation of components in a wind tunnel model are described. A wind tunnel test environment may provide ambient to cryogenic temperature conditions to reproduce aerodynamic flight Reynolds number conditions. Example systems comprise a modular test assembly mounted on a test component, and the test component includes at least one movable surface and is configured for placement in the wind tunnel. An actuator is included within the modular test assembly and coupled to the at least one movable surface of the test component, and a temperature sensor is included to provide temperature of an exterior of the modular test assembly. In addition, a controller is in communication with the actuator and the temperature sensor, and is configured to remotely cause the actuator to move the at least one movable surface through a range of motion.

Remotely controlled and thermally managed system for actuation of components in a wind tunnel model

A method and apparatus comprising a sensor array, a primary lens, and a moveable lens array. The sensor array comprises sensors arranged in an array in which the sensors are configured to generate image data. The primary lens is configured to direct light towards the sensor array. The moveable lens array comprises a number of lenses. The moveable lens array is moveable to a plurality of positions between the primary lens and the sensor array. Each lens in the number of lenses is configured to focus the light.

Scanning zoom system

A rotational actuator assembly employs a first torsion actuator having a shape memory alloy (SMA) tube with a first trained twist direction and a second torsion actuator having a SMA tube with an opposite trained twist direction collinear with the first torsion actuator with abutting proximal ends. A central fitting joins the proximal ends. A control system for temperature control of the first torsion actuator and second torsion actuator about an average temperature provides combined antagonistic rotation of the central fitting.

Remotely actuated wind tunnel model rudder using shape memory alloy

A method of calibrating angle drift of a laser radar system is provided, in one aspect of the present invention. The method includes, providing a plurality of virtual fiducials into an xy scanner; and providing a plurality of auxiliary laser sources into the xy scanner. The method also includes, routing a plurality of auxiliary laser beams from the plurality of auxiliary laser sources into the xy scanner; and calibrating an angular position of a plurality of laser directing means. The methods provides creating a calibration signal for updating the angular position of a plurality of scanning mirrors.

Method and system for correcting angular drift of laser radar systems

A two axis gimbal is provided comprising a support structure, a spherical bearing mounted to the support structure and defining a channel therethrough, and a shaft extending through the channel. The gimbal may also include a reflector connected to the shaft. A drive mechanism, such as a spherical motor, is mounted to the support structure and is adapted to rotate the shaft in two orthogonal axes, i.e., pitch and roll. Power and signal cables are connected to the drive mechanism. The gimbal of the present invention may also include pairs of sensors and sensor triggers for monitoring the position of the shaft and the reflector relative to the pitch and roll axes. The design of the two axis gimbal of the present invention permits the cables to remain stationary during operation of the gimbal.

Two axis gimbal having a spherical bearing

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Bonney Lake, WA, United States of America

Ordie Dean Butterfield