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The Boeing Co patents (2014 archive)


Recent patent applications related to The Boeing Co. The Boeing Co is listed as an Agent/Assignee. Note: The Boeing Co may have other listings under different names/spellings. We're not affiliated with The Boeing Co, we're just tracking patents.

ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "T" | The Boeing Co-related inventors


12/25/14 / #20140380485

Methods and systems for use in analyzing cyber-security threats in an aviation platform

Methods and systems for use in in analyzing cyber-security threats for an aircraft are described herein. One example method includes generating an interconnection graph for a plurality of interconnected aircraft systems. ... The Boeing Co

12/25/14 / #20140380215

Aircraft comparison system with synchronized displays

A method and apparatus for comparing aircraft parts. A first model is identified for a first aircraft with first customer options. ... The Boeing Co

12/25/14 / #20140379401

Benchmarking progressive systems for solving combinatorial problems

A system is provided for benchmarking a progressive combinatorial solver. The system may initialize a parametric model collector, and perform a plurality of parametric trials associated with respective numbers of sub-part iterations of the progressive combinatorial solver. ... The Boeing Co

12/25/14 / #20140377510

Ceramic composite thermal protection system

An apparatus comprises a thermal protection element, a number of washers, a ceramic layer, a number of blind fasteners, and a number of tabs. The thermal protection element has an upper surface, a lower surface, and a plurality of sides. ... The Boeing Co

12/25/14 / #20140377076

Joint assembly and method of forming thereof

A joint assembly is provided. The joint assembly includes a first component formed from a first material and a second component including a portion that extends at least partially into the first component and that has an uneven outer profile. ... The Boeing Co

12/25/14 / #20140377073

Systems and methods for blade attachment

Systems and methods for blade attachment are proved. The systems and methods include an aircraft system having a rotor hub including a blade connector and a composite blade including a lug fitting assembly. ... The Boeing Co

12/25/14 / #20140377018

Systems and methods for delivery of devices along a transport path

Systems and methods for delivery of device along a transport path are provided. One system includes a transport tube having a feed end and a point of use end and a plurality of device carriers operable to move through the transport tube from the feed end to the point of use end. ... The Boeing Co

12/25/14 / #20140376768

Systems and methods for tracking location of movable target object

An automated process uses a local positioning system to acquire location (i.e., position and orientation) data for one or more movable target objects. In cases where the target objects have the capability to move under computer control, this automated process can use the measured location data to control the position and orientation of such target objects. ... The Boeing Co

12/25/14 / #20140376546

Switch routing algorithm

A method using a computer in conjunction with a non-transitory computer readable storage medium is provided comprising a computer receiving a message for forwarding at an ingress switch of a multi-stage circuit switching network. The method also comprises computer executing a first routing algorithm in transmitting the message, the algorithm comprising the computer determining at least one availability matrix for each middle switch, wherein a given middle switch comprises a switch between ingress and egress switches of the network. ... The Boeing Co

12/25/14 / #20140375794

Apparatuses and methods for accurate structure marking and marking-assisted structure locating

Working equipment includes a tool configured to work a structure at a working location thereon, with the structure having an applied marking at a known location with a known relationship with the working location. A computer system is configured to determine placement of the structure, and accordingly position the tool into at least partial alignment with the working location, and which in at least one instance, the tool is aligned with a second, offset location. ... The Boeing Co

12/25/14 / #20140375331

Fault detection of four wire variable differential transformer sensors

Apparatus and methods of detecting failures in systems having a four-wire variable differential transformer sensor. In one embodiment, a method of detecting failures includes monitoring a source frequency of an alternating current (ac) voltage applied to an input of a four-wire variable differential transformer sensor, and monitoring an output frequency for an output of the sensor. ... The Boeing Co

12/25/14 / #20140375309

Apparatus and method for eddy current inspection of structures

There is provided a probe apparatus. The probe apparatus has a first end configured to connect to a rotating scanner device. ... The Boeing Co

12/25/14 / #20140374946

Staggered bevel for continuous compression molding tooling dies

Continuous compression molded process and apparatus for fabricating thermoplastic composite parts from pre-formed thermoplastic composite laminates with tooling dies have a staggered bevel feature at an entry side of the tooling dies. Staggering the length of the bevel feature in each section between bends in a surface contour along the width of the incoming edge of the tooling dies prevents excess material from being trapped and forming wrinkles in the finished thermoplastic part. ... The Boeing Co

12/25/14 / #20140374532

Modular vehicle lift system

Apparatus, systems, and methods provide for a modular vehicle system utilized for lifting and maneuvering payloads. According to aspects of the disclosure, any number of individual lift vehicles may be connected to create a unified lift vehicle. ... The Boeing Co

12/25/14 / #20140374013

Fabrication of stiffened composite panels

A stiffened composite panel is fabricated using modular tooling. Composite pre-preg is laid up and formed over forming block modules each of which is assembled by co-linearly arranging a plurality of forming block segments. ... The Boeing Co

12/25/14 / #20140374010

Fuselage mandrel insert and method

An apparatus for use in formation of a composite structure about a mandrel. A generally flexible pneumatic tool and a generally rigid insert are inserted end to end in a cavity of the mandrel. ... The Boeing Co

12/18/14 / #20140372979

Methods and systems for deploying software applications

A method for assembling a plurality of software modules for executing at least one task is described. The method includes selecting at least one software module from a plurality of available software modules, the one or more software modules selected based on at least one task to be performed, if more than one software module is selected, then configuring the selected software modules to function together in a manner to perform the at least one task to be performed, and generating a cyber package including the at least one software module, the cyber package conforming to a pre-defined protocol.. ... The Boeing Co

12/18/14 / #20140372116

Robotic system with verbal interaction

A method and apparatus for moving an object. A verbal instruction for moving the object is received. ... The Boeing Co

12/18/14 / #20140371956

Systems and methods for moving a load using unmanned vehicles

An actual position of a load tethered with a tether to a vehicle is determined using a plurality of sensors disposed on the vehicle. A required tether tension and required tether angle of the tether is determined to move the load from the actual position to a commanded position. ... The Boeing Co

12/18/14 / #20140370227

Self-balancing pressure bulkhead

A pressure bulkhead may include a bulkhead wall having a radially inner disk and a radially outer compression ring, the outer compression ring being reinforced to balance meridional and hoop stresses sustained by the bulkhead wall in response to a pressure differential across the pressure bulkhead; and the radially inner disk being unitary with the outer compression ring and being made of the same material as the outer compression ring.. . ... The Boeing Co

12/18/14 / #20140369634

Joint bearing lubricant system

A bearing assembly is disclosed having a wearing surface formed from an alloying including tin, a wear material configured to be contacted by the wearing material during use, the wear material having a smoothed surface; and a lubricant composition comprising one or more additives having an affinity for tin. A method of providing superlubricious performance of a bearing assembly is also provided.. ... The Boeing Co

12/18/14 / #20140368637

Control surface calibration system

A method and apparatus for calibrating a set of transducers. In one illustrative embodiment, an apparatus comprises a target device, an imaging device, and a calibrator. ... The Boeing Co

12/18/14 / #20140368316

Positioning systems and methods

Manufacturing systems and methods are disclosed. In one example, a system includes a track to be positioned proximate a structure. ... The Boeing Co

12/18/14 / #20140367822

Systems and methods for dry etching a photodetector array

Systems and methods for dry eteching a photodetector array based on inassb are provided. A method for fabricating an array of photodetectors includes receiving a pattern of an array of photodetectors formed from inassb, the pattern including at least one trench defined between adjacent photodetectors, and dry etching the at least one trench with a plasma including brcl3 and ar.. ... The Boeing Co

12/18/14 / #20140367520

Attitude control of an aircraft in a ditching condition

Configurations provide rapid adjustment to an aircraft attitude in the water upon an emergency water landing. In one configuration, an aircraft fuselage has a forward compartment that includes a water intake and an air vent. ... The Boeing Co

12/18/14 / #20140367512

Honeycomb cores with splice joints and methods of assembling honeycomb cores

Honeycomb cores for use in aerospace applications include two honeycomb core sections operably joined at a splice joint, the splice joint defined by a foam adhesive that is sandwiched between a sheet of film adhesive. Methods of assembling honeycomb cores also are disclosed herein.. ... The Boeing Co

12/18/14 / #20140367481

High viscosity fluid dispensing system

A method and apparatus for depositing a fluid over an interface. A nozzle may comprise a body having a first end and a second end, an input located at the first end of the body, an output located at the second end of the body, and a plurality of channels located within the body. ... The Boeing Co

12/18/14 / #20140367480

High viscosity fluid dispensing system

A method and apparatus for dispensing a fluid. In one illustrative embodiment, an apparatus may comprise a housing comprising a chamber, a dispensing device, and a nozzle system. ... The Boeing Co

12/18/14 / #20140367039

Systems and methods for compacting a charge of composite material

Systems and methods for compacting a charge of composite material. These systems and methods may utilize a vacuum compaction device to compact the charge of composite material on a supporting surface. ... The Boeing Co

12/18/14 / #20140367037

Flexible material transfer devices, flexible vacuum compaction devices, flexible vacuum chucks, and systems and methods including the same

Flexible material transfer devices, flexible vacuum compaction devices that include the flexible material transfer devices, flexible vacuum chucks that include the flexible vacuum compaction devices, and systems and methods including the same. The flexible material transfer devices include a flexible substrate that is configured to selectively and repeatedly transition between a stowed conformation and a deployed conformation. ... The Boeing Co








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