Patents Assigned to BOEING COMPANY, THE
-
Publication number: 20120072098Abstract: A method and apparatus for managing aircraft. Data about components for the aircraft is identified. Fuel efficiency of the aircraft is identified using the data about the components for the aircraft and a model of the aircraft. The model of the aircraft identifies fuel use. The aircraft is managed using the fuel efficiency identified for the aircraft.Type: ApplicationFiled: September 21, 2010Publication date: March 22, 2012Applicant: THE BOEING COMPANYInventors: Luigi Peter Righi, Mark A. Talbot, Gregory Mark Wellbrook, John Lyttle, Fred Austin, Douglas Olie Nelson
-
Publication number: 20120072990Abstract: A method, system, and apparatus are disclosed for cost functions for data transmission. In one or more embodiments, the method, system, and apparatus involve assigning costs associated with the data transmission corresponding to risks. The method, system, and apparatus further involve adjusting data transmission performance parameters according to the costs and the risks. The risks are associated with potential danger, harm, and/or data loss. Data transmission operation costs are related to available radio frequency (RF) bandwidth, data transmission levels of service (LoS) and/or data transmission quality of service (QoS). In at least one embodiment, each different LoS has an associated trigger boundary, which is located at a specific distance away from a risk area and indicates where and/or when to begin data transmission.Type: ApplicationFiled: September 22, 2010Publication date: March 22, 2012Applicant: THE BOEING COMPANYInventors: Gregory M. Gutt, David A. Whelan, Wayne R. Howe, Barton G. Ferrell, Rachel Rané Schmalzried
-
Publication number: 20120066882Abstract: A composite structure and an associated exhaust washed structure are provided which may be formed of ceramic matrix composite (CMC) materials. A method of fabricating a composite structure which may include the CMC material is also provided. A composite structure may include a corrugated septum extending in a lengthwise direction. The composite structure may also include a flute within which the corrugated septum is disposed to form, for example, a partitioned flute assembly.Type: ApplicationFiled: September 23, 2011Publication date: March 22, 2012Applicant: THE BOEING COMPANYInventors: Michael L. Hand, Buddhadev Chakrabarti, Leanne L. Lehman, Gopal P. Mathur
-
Publication number: 20120072706Abstract: The different advantageous embodiments provide an apparatus comprising a central processing unit, a microcode store, and a number of functional units. The central processing unit utilizes transport triggered architecture and is configured to execute microcoded instructions that allow a single instruction to be executed as multiple instructions. The microcode store includes a number of microcoded instruction implementations. The number of functional units includes a number of useful entry points into the microcode store.Type: ApplicationFiled: September 21, 2010Publication date: March 22, 2012Applicant: THE BOEING COMPANYInventor: Albert A. Williams
-
Patent number: 8138992Abstract: Methods and apparatus are provided for evoking perceptions of affordances in a user/virtual environment interface. The method involves recognizing the absence or inadequacy of certain sensory stimuli in the user/virtual environment interface, and then creating sensory stimuli in the virtual environment to substitute for the recognized absent or inadequate sensory stimuli. The substitute sensory stimuli are typically communicated to the user (e.g., visually and/or audibly) as properties and behavior of objects in the virtual environment. Appropriately designed substitute sensory stimuli can evoke perceptions of affordances for the recognized absent or inadequate sensory stimuli in the user/virtual environment interface.Type: GrantFiled: June 2, 2009Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventor: David C. Gross
-
Patent number: 8136328Abstract: A panel includes a core and a fastener receptacle extending into the core. The fastener receptacle has an internal hollow and an opening to the internal hollow. The opening is formed by a lip that can engage and structurally support a push-in fastener.Type: GrantFiled: May 28, 2008Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventors: Harold G. Erickson, Douglas A. Brown
-
Patent number: 8139209Abstract: A system for measuring a laser-induced damage threshold in an optical fiber may include a lens to direct a first laser beam through a core of the optical fiber. The system may also include an optical arrangement to direct a second laser beam through an exterior surface of the optical fiber and into the core of the optical fiber at a preselected location of the optical fiber to provide a predetermined power density at the preselected location, wherein the optical arrangement causes the second laser beam to be directed into the optical fiber substantially completely around a perimeter of the optical fiber to provide the predetermined power density.Type: GrantFiled: November 10, 2008Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventor: Oleg M. Efimov
-
Patent number: 8138938Abstract: A system and method for determining the position and orientation of a handheld device relative to a known object is presented. The system comprises a handheld device having an inertial measurement unit and a sighting device, such as a laser pointer, that are used to determine the position of the handheld device relative to a target object, such as a structure, aircraft, or vehicle. The method comprises calibrating a handheld device to find the current location of the handheld device relative to a target object, tracking the movement of the handheld device using an inertial measurement unit, and presenting an updated position of the handheld device relative to a target object.Type: GrantFiled: October 28, 2008Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventors: James J. Troy, Christopher Esposito
-
Patent number: 8139944Abstract: A method and apparatus for clearing an optical channel for transmitting data through free space between a first and second location includes a light beam, wherein the light beam has a spatially and/or time-dependent modulated intensity profile, and is substantially collimated so that the intensity profile is conserved over a specified distance of operation. The light beam includes a cross-sectional profile having regions of low and high intensity, portions of which are provided for the transmission of an optical data signal. A light source wavelength and intensity are selected for types of obscurant particles having optical properties whereby the radiation pressure acts on the particles, and the particles may then be either attracted into or repelled from portions of the spatially modulated optical beam, leaving certain portions of the optical channel beam absent of obscurant particles, thereby enabling transmission of optical data through the cleared optical channel with low attenuation.Type: GrantFiled: February 25, 2008Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventors: Barbara A Capron, William A McNeely, Kishan Dholakia, Antonia Erika Carruthers
-
Patent number: 8138773Abstract: A sensor for monitoring and testing for both possible fractures and corrosion in structural elements is disclosed. A frangible material layer including a thin breakable conductor sense loop and a resilient material layer including a conductive corrosion sense loop bonded on top of the frangible layer form an assembly which is bonded to a structural element to be tested. Portions of the conductive corrosion sense loop are exposed through weep holes in the resilient material layer. A fracture in the bonded structural element induces a disruption in both the frangible membrane and the thin breakable conductor sense loop and corrosion of the conductive corrosion sense loop changes its electrical properties. Measured electrical property changes of the disrupted conductor sense loop and/or the conductive corrosion sense loop reveal possible damage. Both sensor layers may utilize a single shared wireless communications tag to couple to an electrical measuring device.Type: GrantFiled: September 2, 2008Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventors: Matthew K. Fay, Greg L. Sheffield
-
Patent number: 8136475Abstract: A painting apparatus for applying a coating material to a member surface of a member comprises a housing, at least one slide rail, a rack assembly, a cross beam and a spraying device. The slide rail may be mountable within the housing and may have a plurality of rack positions. The rack assembly is mountable within the housing at one of the rack positions. The rack assembly is configured to support the member such that the member surface is exposed. The cross beam may be coupled to the slide rail. The cross beam is movable along the slide rail and is positionable at the rack positions. The spraying device is mountable on the cross beam and is configured to move along the cross beam while spraying the coating material onto the member surface.Type: GrantFiled: January 6, 2009Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventors: Bruce R. Davis, Michael M. Stepan
-
Patent number: 8137755Abstract: The invention is a high-strength, pre-coated, aluminum or aluminum-alloy component comprising an aluminum or aluminum-alloy article having ultra-fine, submicron grain microstructure and an organic coating of phenolic resin applied to the surface of the article. The article is prepared from a coarse grain aluminum or aluminum-alloy material that is cryomilled into an ultra-fine, submicron grain material, degassed, and densified. The densified material is formed into an article, and coated with an organic coating containing phenolic resin prior to installation or assembly.Type: GrantFiled: April 20, 2005Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventors: Steven G. Keener, Patrick B. Berbon
-
Patent number: 8139558Abstract: A mobile ad hoc network, a mobile ad hoc network node and a method for establishing a system time within a mobile ad hoc network are provided. The network nodes may include a global positioning system (GPS) receiver for receiving GPS signals and for providing a GPS time derived from the GPS signals. The GPS time may be employed by the network node as the system time. Even though the network nodes of a mobile ad hoc network independently determine the GPS time and, in turn, the system time, the system time will be common for each of the network nodes. Mobile ad hoc network nodes may therefore join and leave the mobile ad hoc network with each network node being able to determine the system time prior to its joinder based upon the GPS time provided by the respective GPS receiver.Type: GrantFiled: May 2, 2008Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventors: Mark D. Hall, Timothy M. Force
-
Patent number: 8139111Abstract: A method, apparatus, and computer program product are present for identifying a location in a scene. An image of the scene is displayed on a display device. A cursor on the image is moved in relation to a number of corresponding directions in a model of the scene in response to a manipulation of a number of controls associated with the cursor. A base location in the scene is identified corresponding to a particular point in response to a user input selecting the particular point in the image. A selected point in the image is selected for the scene and a displacement of the selected point is identified from the base location in response to another user input occurring after an identification of the base location. An offset location in the scene is identified corresponding to the selected point in the image using the base location and the displacement.Type: GrantFiled: December 4, 2008Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventor: Lawrence Andrew Oldroyd
-
Patent number: 8136845Abstract: A coupling apparatus for coupling free ends of a pair of tubular ducts in flow communication with one another, and where the free ends of the ducts are separated by an axial gap. The apparatus may have a sleeve having a length sufficient to span the gap and to overlap portions of the free ends of the ducts when the sleeve is secured to the free ends of the ducts. The sleeve may include a first stretchable ply of material, a non-stretchable ply of material, and a second stretchable ply of material sandwiched together. The non-stretchable ply of material may be disposed between the first and second stretchable plies of material to form a unitary assembly. The non-stretchable ply of material may have an axial length of no more than approximately a length of the axial gap to overlay the axial gap.Type: GrantFiled: December 21, 2007Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventors: Jayant D. Patel, Clifford J. Petersen, Maggie E. Fuselier, Alfred R. Wiratunga, Annette D. Motherwell, Vitor M. Amorim
-
Patent number: 8136988Abstract: A temperature sensor is described that includes a base, a first set of posts attached to the base having a first coefficient of thermal expansion, a second set of posts attached to the base and having a second coefficient of thermal expansion, and two substantially parallel conductive plates forming a capacitor. The first of the conductive plates is fixed to the first set of posts and the second of the conductive plates is fixed to the second set of posts. Temperature changes cause the first set of posts and the second set of posts to elongate at different rates, thereby changing a distance between the conductive plates and therefore the resulting capacitance. A system and method are also described for determining resonant frequency associated with the sensor which correlates to the temperature at the sensor when multiple sensors are networked across a system.Type: GrantFiled: January 15, 2009Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventors: William Preston Geren, Brian Kenneth Kormanyos, Kathryn A. Masiello, Gerardo Pena
-
Publication number: 20120065881Abstract: A method and apparatus for managing a flight of an aircraft. Conditions in an environment around the aircraft are monitored during the flight of the aircraft on a route having a number of target points. In response to detecting a condition requiring a change to the route of the aircraft, current resources for the aircraft are identified. A determination is made as to whether changing the route reduces the number of target points that can be reached based on the current resources for the aircraft. In response to a determination that changing the route reduces the number of target points that can be reached, the route is changed to include a portion of the number of target points using the condition and a policy.Type: ApplicationFiled: September 14, 2010Publication date: March 15, 2012Applicant: THE BOEING COMPANYInventors: John L. McIver, Alan Eugene Bruce, Daniel J. Gadler, Charles B. Spinelli
-
Publication number: 20120060491Abstract: 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.Type: ApplicationFiled: September 10, 2010Publication date: March 15, 2012Applicant: The Boeing CompanyInventors: Ian Gunter, Robert T. Ruggeri, James H. Mabe, Darin Arbogast, Ordie D. Butterfield, Daniel Morgenroth
-
Publication number: 20120061512Abstract: Structures and methods for joining composite fuselage sections and other panel assemblies together are disclosed herein. In one embodiment, a shell structure configured in accordance with the present invention includes a first panel portion positioned adjacent to a second panel portion. The first panel portion can include a first stiffener attached to a first composite skin, and the second panel portion can include a second stiffener attached to a second composite skin. The shell structure can further include a fitting extending across a first edge region of the first panel portion and a second edge region of the second panel portion. A first end portion of the fitting can be attached to the first stiffener and the first composite skin, and a second end portion of the fitting can be attached to a second stiffener and a second composite skin, to join the first panel portion to the second panel portion.Type: ApplicationFiled: November 18, 2011Publication date: March 15, 2012Applicant: THE BOEING COMPANYInventors: Jeffrey F. Stulc, Wallace C. Chan, Brian C. Clapp, Neal G. Rolfes
-
Patent number: 8135776Abstract: A system for managing the communication of multi-page documents. The system may use a software module document splitter adapted to receive a multi-page document being uploaded as a single file and to split the multi-page document into a plurality of independent files, with each independent file representing a single page of the document. The software module document splitter may also associate meta data with each single page that enables the single pages to be downloaded, one at a time, by an electronic device being used by a user, from a file storage device remote from the electronic device. This provides the appearance to the user that the electronic device is in possession of single, multi-page file.Type: GrantFiled: November 24, 2008Date of Patent: March 13, 2012Assignee: The Boeing CompanyInventor: John F. Bremer, Jr.