The Boeing Company

Hrl Laboratories, LLC

Thr Boeing Company

Dejan Nikic

James A Grossnickle

Mark Joseph Clemen, Jr

Arthur C Day

Yuan-Jye Wu

Carl Roy McIver

Mark D Severson

Michelle Galgana

Yuri Owechko

John Ralph Hull

Swarup S Medasani

Alan Frank Stewart

Eddie Kwon

Shahriar Khosravani

Jason Scott Damazo

Kevin Bowcutt

Philipp Andreas Boettcher

Thommen Korah

Dominic Martinez

Farrah Tan

Jason Wu

Mark Joseph Clemen Jr

Carl Roy Mciver

Kevin G Bowcutt

A system for calibrating the light sensitivity of a camera includes a light emitter for emitting a light pulse, a fiber splitter for receiving the light pulse via an input port and providing first and second portions of the light pulse to respective first and second output ports, and a light collector for receiving the first portion from the first output port and converting the first portion to a first signal representative of a light characteristic of the first portion. A first fiber optic cable connects the light emitter and the input port, a second fiber optic cable connects the first output port and the light collector, and a third fiber optic cable has a first cable end connected with the second output port and a second cable end for emitting the second portion of the light pulse for capture by the camera. A related method is also provided.

System and method for calibrating the light sensitivity of a camera

Systems and methods for enabling charged (ionized) air mass measurement for reliable air data computation onboard an aircraft. Ionic charge sensing may be used to derive air data having improved reliability. The systems and methods for ionic charge sensing employ an emitter electrode and two or more collector electrodes, which electrodes are disposed in proximity to the exterior skin of the aircraft and exposed to ambient air. The emitter electrode is positioned forward of the collector electrodes. The system further includes a solid-state ionic air data module that converts currents from the collector electrodes into air data parameter values. More specifically, the ionic air data module is configured to sense currents induced in the collector electrodes in response to corona discharge produced by the high-voltage emitter electrode.

Charged air mass measurement for air data computation

Systems include a test object that comprises a surface having a non-planar topographical feature, and an electrode comprising a non-linear segment that is proximate to the non-planar topographical feature of the surface of the test object. The electrode is positioned proximate to but not in contact with the surface of the test object such that the perpendicular distances between the electrode and the surface of the test object are uniform across the electrode. The electrode is further configured to (i) be translated across the surface of the test object while maintaining the perpendicular distances between the electrode and the surface of the test object, and (ii) impart a layer of charge across the surface of the test object when the test object is translated across the surface.

Surface charging systems and method for charging a non-planar surface

A neutron generator includes a fuel source configured to provide a neutron-producing fuel. The neutron generator includes a plasma confinement device coupled to the fuel source and configured to generate a z-pinch of the neutron-producing fuel.

Plasma pinch neutron generators and methods of generating neutrons

A single-use neutron generator includes a power supply. The single-use neutron generator includes a fuel source configured to provide neutron-producing fuel. The single-use neutron generator includes a plasma confinement device coupled to the power supply and the fuel source and configured to generate a plasma pinch of the neutron-producing fuel. At least one component of the single-use neutron generator is configured for single use.

Single-use plasma pinch neutron generators

A scramjet includes a converging inlet, a combustor configured to introduce a fuel stream into an air stream in a combustion chamber and to combust the fuel air mixture stream to create an exhaust stream, and a diverging exit nozzle configured to accelerate the exhaust stream. The combustor includes a fuel injection system including at least one arcjet. A method of creating thrust for an aircraft includes compressing a supersonic incoming air stream in a converging inlet, injecting a fuel stream into the air stream in a combustion chamber to create a fuel air mixture stream, igniting the fuel air mixture stream to create an exhaust stream, and exhausting the exhaust stream from a diverging exit nozzle. The injecting the fuel stream into the air stream includes injecting the fuel stream at a fuel speed sufficient to create shear between the fuel stream and the air stream.

Scramjets and associated aircraft and methods

A micro-hollow cathode discharge device. The device includes a first electrode layer comprising a first electrode. A hole is disposed in the first electrode layer. The device also includes a dielectric layer having a first surface that is disposed on the first electrode layer. The hole continues from the first electrode layer through the dielectric layer. The device also includes a semi-conducting layer disposed on a second surface of the dielectric layer opposite the first surface. The semi-conducting layer is a semiconductor material that spans across the hole such that the hole terminates at the semi-conducting layer. The device also includes a second electrode layer disposed on the semi-conducting layer opposite the dielectric layer.

Semiconductor micro-hollow cathode discharge device for plasma jet generation

A plurality of magnetic field sensors, for example arranged in an array, is operative to measure changes in magnetic field strength proximate the surface(s) of a test structure. The test structure may approximate the geometry of an airplane fuselage, wing, or the like. An electric current is applied to the test structure, and the magnetic field sensors sense changes in a magnetic field caused by the current. A corresponding plurality of integrators convert the sensor outputs to magnetic field strength values. From the plurality of magnetic field strength values and corresponding sensor locations, a current density over the target surface is inferred.

Large surface magnetic field sensor array

A nondestructive bond strength testing method, including: coupling an expendable device to a structure under test, the expendable device including a patterned planar array of exploding bridge wires; simultaneously vaporizing the patterned planar array of exploding bridge wires by applying a pulse of electrical energy to the patterned planar array of exploding bridge wires; and sensing an initial disbonding signature of the structure under test.

Bond strength testing systems and methods and compression wave producing devices for use therein

Laser amplification utilizing plasma confinement of a gas laser gain media is described. The gas laser gain media is compressed into plasma utilizing a self-reinforcing magnetic field referred to a plasma pinch (e.g., a flow stabilized z-pinch). In the plasma pinch, the gas laser gain media is compressed to a high density, which improves the gain of the media. An optical resonator partially surrounds the plasma pinch and utilizes the laser gain media compressed within the plasma pinch to generate an output of coherent light.

Optical resonators that utilize plasma confinement of a laser gain media

An example method for plasma cleaning a container includes generating plasma flowing within the container, applying a magnet to an exterior surface of the container causing the plasma within the container to be attracted to the magnet, and moving the magnet in a motion over the exterior surface to control movement of the plasma within the container and to clean one or more areas of the container with the plasma according to the motion. An example system for plasma cleaning a container includes a power source, a gas inlet on the container for dispersing a gas within the container, and based on current flowing, the gas converts to plasma. The system also includes a robotic manipulator having an end effector coupled to a magnet to move the magnet in a motion over an exterior surface of the container causing the plasma within the container to be attracted to the magnet.

Methods and systems for plasma cleaning a container using a magnet

Propagating brush discharge testing systems include an initiation electrode, a high-voltage switch, a sensor, and a controller. The initiation electrode has an exposed tip positioned adjacent to a surface of a test article. The high-voltage switch is configured to selectively isolate the initiation electrode from ground potential. The sensor is positioned and configured to detect a propagating brush discharge between the initiation electrode and the test article. The controller is programmed to operate the high-voltage switch to ground the initiation electrode.

Systems and methods for propagating brush discharge testing

A method for placing electrical conductors interior to a composite structure prior to curing. A laminate stack is formed by assembling one or more composite layers, wherein the composite layers are pre-impregnated with a resin. One or more electrical conductors are placed on at least one of the composite layers prior to curing the laminate stack. One or more electrical insulators is optionally placed in proximity to one or more of the electrical conductors in at least one of the composite layers prior to curing the laminate stack. The laminate stack, including the composite layers, the electrical conductors, and the electrical insulators, is then cured to create the composite structure.

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Seattle, WA, United States of America

Dejan Nikic