The Boeing Company

William John Sweet

Kevin Richard Housen

Jason Scott Damazo

Eddie Kwon

Philipp Andreas Boettcher

Arthur C Day

John Ralph Hull

Richard Henry Bossi

Mark Alan Negley

Michael Strasik

Marc Joel Piehl

Alan Frank Stewart

Lee Charles Firth

Douglas Allen Frisch

Timothy Leroy Williams

Bret A Voss

Eldon C Rogers

Jean-Michel I Fouard

Dennis Yee

Michael Howard-Edward Ware

Michael D Gonzales

Neal J McCluskey

Charles G Bloch

An ignition suppressing enclosure configured to contain an ignition source is disclosed and includes a body portion defining an inner surface, an outer surface, and an enclosed volume containing a flammable gaseous mixture. The enclosed volume is sized to contain the ignition source. The enclosed volume of the ignition suppressing enclosure is surrounded by an exterior combustible environment also containing the flammable gaseous mixture. The ignition suppressing enclosure includes one or more vent paths that extend between the inner surface and the outer surface of the body portion, where each individual vent path includes an effective diameter based on at least a minimum ignition energy of the flammable gaseous mixture. The effective diameter of the individual vent path is selected to quench a flame that occurs within the enclosed volume of the ignition suppressing enclosure.

Ignition suppressing enclosure having vent paths for flame quenching

A system for detecting a leak in a duct is disclosed, including a sheath covering a duct section, a fluid concentrating device and a sensor. The sheath is attached to a boundary portion of the duct section and forms an inner space between an outer surface of the duct section and the sheath. The fluid concentrating device has an opening through the sheath connecting the inner space to an external space outside the sheath. The inner space is sealed except for the opening through the sheath. The sensor is stationed outside the opening of the fluid concentrating device and is configured to detect fluid flow from the inner space through the opening at a level corresponding to a duct leak in a pre-burst condition.

Systems and methods for early detection of pneumatic transport element leaks

Gas-flammability sensing systems and methods may be used to determine the flammability of gas mixtures in measurement volumes such as a fuel tank (e.g., an aircraft fuel tank). Gas-flammability sensing systems include a test cell structured to receive a gas sample, a heater in thermal communication with the test cell, and a gas meter configured to measure a physical property of the gas sample within the test cell related to the combustion state of the gas sample. The heater is configured to heat the gas sample to an elevated temperature less than the autoignition temperature of the gas sample. Methods of determining the flammability of a gas sample include collecting the gas sample, heating the gas sample to the elevated temperature, measuring the physical property of the gas sample after heating, and determining the flammability of a gas sample based upon the measured physical property.

Gas-flammability sensing systems and methods

A method and apparatus for measuring a dynamic tensile stress and/or tensile strain response of a material such as an elastic material and/or a ductile material. The apparatus may include a striker bar, a stretcher bar, and a drive assembly configured to propel the striker bar toward the stretcher bar. The apparatus may further include a stationary specimen mount and a movable specimen mount that receive a test sample. The striker bar and the stretcher bar of the apparatus may provide a continuous stress on the test sample and an accurate tensile stress/strain measurement.

Device for measuring the dynamic stress/strain response of ductile materials

An apparatus and a method for simulating a mechanical stress applied to a sealant from a lightning strike upon an aircraft is provided. The apparatus comprises a specimen, a test fixture, and a capacitor. The specimen comprises an electrically non-conductive sealant for an aircraft fuel tank having a cylindrical shape, and an electrically conductive wire centered axially within the sealant. The test fixture secures the specimen during testing. The capacitor is electrically coupled to the test fixture, and simulates a lightning strike upon the aircraft by vaporizing the wire with a current to generate a mechanical shock to the sealant.

Sealant testing for aircraft fuel tanks

Methods and systems for duct protection of a vehicle are provided. The methods and systems provided include an apparatus for containing a flow of fluid discharged from a fracture in a duct. The apparatus includes a ballistic containment layer and an insulation sheath coupled to the ballistic containment layer. The insulation sheath includes a first air containment layer, an insulation layer, and a second air containment layer.

Systems and methods for duct protection of a vehicle

A bond inspection system may include a material that reacts to applied activation energy by creating a compression wave, the material positioned adjacent a surface of a structure having a bond to be inspected and shaped in a predetermined pattern, such that reaction of the material causes compression waves to travel through the surface and structure; a source of activation energy capable of directing the activation energy at the material; and a controller programmed to actuate the source of activation energy to direct the activation energy at discrete portions of the predetermined pattern of material in a predetermined sequence selected to create a plurality of the compression waves so that the compression waves reflect from an opposite side of the structure as a plurality of tension waves that combine at substantially the same time at a bondline of the structure to be inspected.

Bond inspection system and method

A system and methods are provided for evaluating a bond between structures. The system includes an assembly of at least two bonded structures. The assembly has a front surface, a back surface, a thickness, and a bond disposed between the front surface and the back surface. At least one delay component is attached to the front surface of the assembly having a body having a front face, a back face, and a thickness. The system further includes a laser source capable of depositing laser energy onto a front face of the delay component, where a first portion of the laser energy is absorbed by the front face of the delay component to generate a first compression wave that propagates through the body of the delay component. A second portion of the laser energy is absorbed by the back face of the component to generate a second compression wave that reflects off of the back surface of the assembly to produce a tensile wave that stresses the bond.

Method for controlling tensile stress during evaluation of a bond between structures

A method and apparatus for testing a test object. A stress wave is generated in a fluid within a cavity in a structure. The stress wave is directed through the fluid within the cavity into the test object.

Hydroshock inspection system

Systems and methods described herein provide for the protection of personnel within vehicles and structures from handheld grenades and other threats. According to one aspect of the disclosure provided herein, a countermeasure system includes an expandable countermeasure having a flexible body with a number of weighted projectiles attached around a perimeter of the body. A threat detection and launch control system detects incoming threats and, in response, triggers a launch of the expandable countermeasure from the launcher to intercept and neutralize the threat.

Growing community of inventors

Seattle, WA, United States of America

William John Sweet