Patents Assigned to Boeing Company
  • Patent number: 6995575
    Abstract: Apparatus and methods of measuring the electrical resistance of electrically-conductive materials are disclosed. In one aspect, an apparatus includes a substrate, and first, second, third, and fourth elongated conductive members. Each conductive member includes a first portion at least partially disposed on the substrate and a second portion. Each of the first portions is spaced apart from one or more adjacent first portions and is engageable with the electrically-conductive material along a contact length. The apparatus may include a source operatively coupled to the second portions of the first and fourth conductive members, and a meter operatively coupled to the second portions of second and third conductive members.
    Type: Grant
    Filed: April 30, 2003
    Date of Patent: February 7, 2006
    Assignee: The Boeing Company
    Inventor: Carl B. Gifford
  • Patent number: 6994762
    Abstract: A single crystal piezo (SCP) apparatus and method of forming same. The apparatus is ideally suited for actuator and energy harvesting applications. The apparatus includes an SCP layer bonded to a surface of a flexible metal layer while the metal layer is held flattened within a press or other tool. Once the bonding process is complete, the metal layer imparts a compressive strain to the SCP layer bonded thereto. A layer of uniaxial graphite may also be bonded to the SCP layer to eliminate the poison's ratio tension that would otherwise be created in the SCP layer.
    Type: Grant
    Filed: February 10, 2003
    Date of Patent: February 7, 2006
    Assignee: The Boeing Company
    Inventors: Dan J. Clingman, A. Dean Jacot
  • Patent number: 6994378
    Abstract: The apparatus for joining and sealing conduits, includes edge trim, a sleeve, and a retaining element. The edge trim is shaped to mount upon and engage an end of a conduit. The sleeve extends between the conduits and at least partially surrounds the edge trim. The sleeve may be made of compressible material, such that when the retaining element surrounds a portion of the sleeve and the edge trim, the retaining element generally compresses the portion of the sleeve portion underlying the retaining element and displaces the sleeve material to expand on either side of the retaining element and limit movement of the retaining element. The method of joining and sealing conduits includes mounting the edge trim and a retaining element upon an end of a conduit, extending a sleeve between the conduits, and sliding the retaining element over the sleeve toward the end of the conduit.
    Type: Grant
    Filed: October 30, 2003
    Date of Patent: February 7, 2006
    Assignee: The Boeing Company
    Inventors: Jayant D. Patel, Alfred R. Wiratunga
  • Patent number: 6994242
    Abstract: A rotatable tool for friction stir welding a workpiece and an associated apparatus and method are provided. The tool includes a first pin portion that extends from a shoulder and defines a contour surface opposite the shoulder. A second pin portion extends from the contour surface of the first pin portion. The contour surface, which mixes the material of the workpiece during welding, can increase the mixing of the material at the interface, thereby increasing the strength of the joint.
    Type: Grant
    Filed: December 9, 2003
    Date of Patent: February 7, 2006
    Assignee: The Boeing Company
    Inventors: Christian B. Fuller, Murray W. Mahoney, William H. Bingel
  • Patent number: 6995536
    Abstract: The present invention discloses a robotic manipulator, comprising at least one joint, each joint having a drive axis and at least one microelectromechanical system (MEMS) inertial sensor aligned with at least one drive axis providing sensing of a relative position of the drive axis. The robotic manipulator can include an inertial measurement unit (IMU) coupled to the robotic manipulator for determining the end effector position and orientation. A controller can be used, receiving a signal from at least one MEMS inertial sensor and controlling at least one joint drive axis in response to the signal to change the relative position of the joint drive axis. Rate information from MEMS sensors can be integrated to determine the position of their respective drive axes.
    Type: Grant
    Filed: April 7, 2003
    Date of Patent: February 7, 2006
    Assignee: The Boeing Company
    Inventor: A. Dorian Challoner
  • Patent number: 6993971
    Abstract: There is provided an ultrasonic inspection device that provides a locking mechanism for inspecting components at preset angles. The inspection device can inspect a component along an arc by inspecting the component at each preset angle, which provides complete and repeatable inspection results. The inspection device comprises a housing with a channel for the passage of an ultrasonic signal and an ultrasonic transducer to transmit and receive the ultrasonic signals. The housing also includes a rotating reflector to reflect the ultrasonic signal. Using a handle on the housing rotatably attached to the rotating reflector, a technician can rotatably position and lock the rotating reflector at a preset angle. The rotating reflector can be rotatably locked by a spring-loaded ball that is selectively received in detents defined by the rotating reflector or handle.
    Type: Grant
    Filed: December 12, 2003
    Date of Patent: February 7, 2006
    Assignee: The Boeing Company
    Inventors: Richard H. Bossi, Martin Freet, Gary E. Georgeson, Stanley W. Richardson
  • Patent number: 6995658
    Abstract: A power line modem interface includes a modem that modulates an RF signal with digital data and demodulates an RF signal to recover digital data. A filter is connected to the modem and to a DC power line that supplies power to a local power supply. The filter couples the RF signals from the modem to the DC power line and filters the RF signals out of the local power supply. The filter includes: a first inductance connected to a hot side of the DC power line; a second inductance connected in series with the first inductance and connected to the local power supply; and a capacitance with a first plate connected between the first inductance and the second inductance and a second plate connected to the modem so that the RF signal is passed between the modem and the DC power line.
    Type: Grant
    Filed: June 11, 2003
    Date of Patent: February 7, 2006
    Assignee: The Boeing Company
    Inventors: Ronald M. Tustison, Mark A. Shelton
  • Patent number: 6995690
    Abstract: A flight information display for the flight deck of an aircraft showing a pictorial side view of the flight path or the area directly in front of the aircraft area having a selected distance of at least 0.5 nautical miles, comprising (a) a pictorial representation to scale of the profile of the highest elevations of a swath of terrain along said path or area, (b) an icon positioned on the left or right side of the display representing the aircraft, the altitude of which is to scale with the height of the terrain, and (c) an altitude reference scale; wherein the width of the swath is at least 0.1 nautical miles and no greater than the distance of the minimum accuracy of the means for determining the aircraft's location.
    Type: Grant
    Filed: July 27, 2000
    Date of Patent: February 7, 2006
    Assignee: The Boeing Company
    Inventors: Sherwin S. Chen, Julianne M. Fox, Neal D. Molloy, John Wiedemann
  • Patent number: 6993849
    Abstract: An aerospace system includes a leveling device defining two plane levels (yz-plane and xz-plane). The plane levels are included within an inertial measurement unit and each of the plane levels includes two capacitance controlled oscillators. Each of the capacitance controlled oscillators includes a quad capacitor bubble sensor.
    Type: Grant
    Filed: November 5, 2004
    Date of Patent: February 7, 2006
    Assignee: The Boeing Company
    Inventors: Ray F. Campbell, Joan D. Wada, Michael J. Costello
  • Patent number: 6994297
    Abstract: A method of controlling movement of a vehicle including generating a fluid jet adjacent an aerodynamic surface of the vehicle, and changing at least one of a strength and a position of a shock wave traveling over the aerodynamic surface of the vehicle by directing the jet into a boundary layer flow of air attached to the aerodynamic surface.
    Type: Grant
    Filed: October 27, 2004
    Date of Patent: February 7, 2006
    Assignee: The Boeing Company
    Inventors: Ahmed A. Hassan, Garry Billman
  • Patent number: 6996058
    Abstract: An interconnect fabric module (“IFM”) with high-speed switching capabilities. An interconnect fabric module can be dynamically configured to interconnect its communications ports so that data can be transmitted through the interconnected ports. Multiple interconnect fabric modules can be connected to form an interconnect fabric through which nodes (e.g., computer systems) can be interconnected. In one embodiment, data is transmitted through the interconnect fabric as frames such as those defined by the Fiber Channel and InfiniBand standards. The interconnect fabric module allows the creation of an interconnect fabric that is especially well suited for interconnecting devices utilizing multiple information types such as might be required by the devices of an enterprise data network (“EDN”).
    Type: Grant
    Filed: October 26, 2001
    Date of Patent: February 7, 2006
    Assignee: The Boeing Company
    Inventors: Michael S. Foster, Michael A. Dorsett
  • Publication number: 20060021654
    Abstract: A temperature controlled hydraulic fluid supply circuit (12) includes a first hydraulic fluid reservoir (18), that has an initial hydraulic fluid (20), and a temperature controlled housing (45). A second hydraulic fluid reservoir (26) is fluidically coupled to the first hydraulic fluid reservoir (18), resides within the temperature controlled housing (45), and has a controlled hydraulic fluid (14) that is supplied to a test device (16). A circulation device (60) circulates a temperature altering fluid (62) through the temperature controlled housing (45) and adjusts the temperature of the controlled hydraulic fluid (14).
    Type: Application
    Filed: July 29, 2004
    Publication date: February 2, 2006
    Applicant: THE BOEING COMPANY
    Inventors: Scott Maxwell, Dale Smith, Marcus Topp
  • Publication number: 20060022087
    Abstract: A crewmember rest support system (10) includes a berth mattress (32). A support structure (34) is coupled to and supports the berth mattress (32). A pneumatic system (36) is coupled to the support structure (34). The pneumatic system (36) includes an inflatable member (100) that has one or more inflatable states. A pump (102) actuates the inflatable member (100) and articulates a portion of the support structure (34).
    Type: Application
    Filed: July 27, 2004
    Publication date: February 2, 2006
    Applicant: THE BOEING COMPANY
    Inventors: Riccardo Defilla, Luigi Crocco, Simone Messeri
  • Publication number: 20060022090
    Abstract: A carry-on luggage system (450) for an airport includes a carry-on interface station (453). A carry-on transport module (452) is disposed and accessible within the carry-on interface station (453) and includes multiple stowage units (467) for carry-on items. A transport mechanism (451) transports the carry-on transport module (452) between the airport interface terminal (14) and an aircraft. A method of loading and unloading carry-on items on and off an aircraft includes providing access to a stowage unit (467). The stowage unit (467) is on a carry-on transport module (452) at a carry-on interface station (453). Access to the stowage unit (467) allows for placement of at least one carry-on item therein. The carry-on transport module (452) is transported between the carry-on interface station (453) and an aircraft.
    Type: Application
    Filed: October 18, 2005
    Publication date: February 2, 2006
    Applicant: THE BOEING COMPANY `
    Inventors: William McCoskey, Richard Johnson
  • Patent number: 6993431
    Abstract: One aspect is a method which determines a float remaining figure (for example, a float remaining circle) for a manufactured pattern of features. In some embodiments, the size and relative location of two or more float remaining figures, each for a different part (each part typically designed in accordance with a different pattern of features), are compared and optionally also transformed to provide a quantifiable measure of whether the two parts fit (or can be modified to fit) and if so how well the parts fit. Other aspects are systems programmed to perform any embodiment of the method, and computer readable media which store code for implementing any embodiment of the method.
    Type: Grant
    Filed: June 1, 2004
    Date of Patent: January 31, 2006
    Assignee: The Boeing Company
    Inventors: Paul C. Hollingshead, Bruce A. Wilson
  • Patent number: 6990863
    Abstract: The present invention discloses a resonator gyroscope including an isolated resonator. One or more flexures support the isolated resonator and a baseplate is affixed to the resonator by the flexures. Drive and sense elements are affixed to the baseplate and used to excite the resonator and sense movement of the gyroscope. In addition, at least one secondary element (e.g., another electrode) is affixed to the baseplate and used for trimming isolation of the resonator. The resonator operates such that it transfers substantially no net momentum to the baseplate when the resonator is excited. Typically, the isolated resonator comprises a proof mass and a counterbalancing plate.
    Type: Grant
    Filed: April 25, 2003
    Date of Patent: January 31, 2006
    Assignees: The Boeing Company, California Institute of Technology
    Inventors: A. Dorian Challoner, Kirill V. Shcheglov
  • Patent number: 6991371
    Abstract: A computed tomography (CT) image quality phantom for use in calibrating explosive detection systems (EDS) at airports. A foam core block containing up to five right cylinder rod members is positioned in a housing member which is adapted to be passed through an airport luggage scanning machine. The rod members are of different lengths in order to create different data slices for analysis. The housing has a lead-in member at least at one end in order to allow passage through an EDS more easily and provide accurate CT calibrating.
    Type: Grant
    Filed: October 14, 2003
    Date of Patent: January 31, 2006
    Assignee: The Boeing Company
    Inventors: Gary E. Georgeson, James M. Nelson, Richard H. Bossi
  • Patent number: 6993288
    Abstract: A method of coordinating communications between ground stations and fixed beam satellites is provided, wherein each beam of a satellite antenna is assigned a color to create a color pattern that matches a frequency reuse pattern for the antenna, thereby using the same frequencies in a different beam with the same color. In operation, a ground station requests a virtual channel number from a resource manager, which sends a virtual channel number that is not used by another ground station within a beam diameter of the requesting ground station. The ground station then determines the position of the satellite, the beam and beam color, and further computes the frequency, polarization, and time slot, among other information, to communicate with the satellite. A method is also provided for managing virtual channels that comprises a network manager that groups ground stations and limits the number of virtual channels per group.
    Type: Grant
    Filed: July 17, 2002
    Date of Patent: January 31, 2006
    Assignee: The Boeing Company
    Inventors: Michael de La Chapelle, David C. Morse, Leonard J. Quadracci
  • Patent number: 6991235
    Abstract: A gas-buffered brush seal assembly and associated method are provided. The seal assembly includes at least one brush seal that defines an interface with a rotatable member. The seal assembly is configured to deliver a gas to the interface so that the gas at least partially prevents the flow of a fluid therethrough. In addition, the seal assembly can be adjustable so that the flow of the fluid is controlled by adjusting the flow rate of the gas through the seal assembly.
    Type: Grant
    Filed: November 7, 2003
    Date of Patent: January 31, 2006
    Assignee: The Boeing Company
    Inventors: Stephan J. Ebert, James D. Goss, Neil G. Hicks, Scott E. McVey, Jozsef L. Moharos, Dean J. Nunez
  • Patent number: D513998
    Type: Grant
    Filed: November 5, 2004
    Date of Patent: January 31, 2006
    Assignee: The Boeing Company
    Inventors: R. Blake Emery, Kenneth J. Dowd, Kee Sook Jeon