649 patents
Page 29 of 33
Utility
Acceptance testing system
16 Mar 20
A system for acceptance testing includes a data acquisition system operable to receive a plurality of sensor inputs from a component under test.
James N. Rozak, Michael C. Kingsley, Michael G. Mastrianni, Daniel Alfred Ciaburri
Filed: 14 Jun 15
Utility
Distributed multi-aperture camera array
16 Mar 20
In one embodiment, an electronic camera assembly includes a circuit board and a plurality of sensor facets.
Mark A. Lamkin, Kyle Martin Ringgenberg, Jordan David Lamkin
Filed: 6 Feb 18
Utility
High speed image registration system and methods of use
9 Mar 20
The invention is directed to systems and methods for image capturing technologies and, more particularly, to a high speed image registration system and respective processes to achieve high quality images.
Alexander M. Elhage
Filed: 16 May 18
Utility
Bond fixture for root end laminate or rotor blade
2 Mar 20
A bond assembly includes a fixture having a first section movably coupled to a second section.
Sven Roy Lofstrom, Ryan Lehto
Filed: 8 Aug 16
Utility
Cockpit control of a fixed wing aircraft
2 Mar 20
A device and method for flying an aircraft is disclosed.
Michael Paul Baran, Nicholas Charles Visinski, Igor Cherepinsky
Filed: 18 May 17
Utility
Multi core vehicle management system and methods
2 Mar 20
A flight management system (FMS) including a plurality of FMS components that can include a civil FMS component and a tactical FMS component.
Lester J. Pangilinan, John Olsen
Filed: 13 Aug 17
Utility
Integrated bifilar system that absorbs vibrations in both vertical and in-plane directions
2 Mar 20
A dual axis bifilar vibration absorber system including a first bifilar vibration absorber having a first support provided with a first cantilevered end including a first opening and a second cantilevered end including a second opening.
Z. Kevin Wang, Larry B. Eastman
Filed: 19 Mar 18
Utility
Electric propulsion system with overrunning clutch for a rotary-wing aircraft
2 Mar 20
An electric propulsion system for use with a mast defining an axis of rotation and one or more rotor blades which rotate about the axis of rotation, includes a yoke assembly, electric motor, motor support housing, and overrunning clutch.
Timothy Fred Lauder
Filed: 15 Feb 17
Utility
Active rotor damping system
2 Mar 20
An aircraft is provided and includes a non-rotating frame, an engine disposed in the non-rotating frame, a rotating frame, which is drivable by the engine to rotate relative to the non-rotating frame to generate lift and thrust, the rotating frame including a hub and rotor blades extending outwardly from the hub, an actuation system including electro-mechanical actuators (EMAs) respectively disposed in the rotating frame between the hub and the rotor blades, each EMA including a rotary inductive device, a gear train associated with each EMA and the corresponding rotary inductive device to convert linear displacements of a piston responsive to rotor blade lead/lag into rotation of the rotary inductive device and a controller that controls the rotary inductive device to operate, in a first mode, as a motor which drives the gear train, and, in a second mode, as a generator which is driven by the gear train.
James Orbon
Filed: 25 Jan 16
Utility
Tailorable polyorbital-hybrid ceramics
2 Mar 20
In an embodiment, a method includes producing a mixed feedstock of at least three halogenated monomer feedstocks.
David Glen Findley
Filed: 11 May 17
Utility
Active sensing system and method of sensing with an active sensor system
2 Mar 20
An active sensing system includes an agent and at least one sensor operatively associated with the agent.
Michael Aaron Connor
Filed: 15 Jun 16
Utility
Systems, devices, and methods for photonic to radio frequency conversion
2 Mar 20
A system, method, and device for RF upconversion.
Andrew F. Schaefer, Paul T. Coyne, John C. Ceccherelli
Filed: 26 Nov 17
Utility
Supplemental power for reduction of prime mover
24 Feb 20
Embodiments are directed to selecting, by a computing device comprising a processor, the size of at least one prime mover associated with an aircraft to satisfy a baseline power requirement for operation of the aircraft during a steady state load condition, selecting at least one power source configuration to supplement power provided by the at least one prime mover during a transient load condition associated with the operation of the aircraft, and selecting, by the computing device, a parameter of the at least one power source configuration to provide a total power in an amount that is greater than a threshold during the transient condition.
Joseph Lawrence Simonetti, Mark Denton Bystry, Michael Joseph DeVita, Matthew J. Tarascio, Michael Peter Strauss, Hayden M. Reeve, Niranjan Desai, Brian St. Rock, Charles E. Lents, Lawrence E. Zeidner, Alfred Russell Smiley
Filed: 4 May 14
Utility
Apparatus and methods for making rotorcraft rotor blades
24 Feb 20
A method of making a rotor blade assembly includes receiving a sheath assembly and a blade body at a blade assembly tool.
David Littlejohn, Sven Roy Lofstrom, Eric C. Boyle
Filed: 29 Jun 16
Utility
System and materials for corrosion detection
24 Feb 20
A system configured for detection of corrosion of a metal substrate is disclosed.
Mark R. Jaworowski, Haralambos Cordatos, Lubomir A. Ribarov
Filed: 9 Jan 14
Utility
Lubricant level sensing for an actuator
24 Feb 20
According to one aspect, a lubricant level sensing system for an actuator is provided.
Claude G. Matalanis, Ulf J. Jonsson, John D. Cannata, Brian E. Wake
Filed: 26 Aug 15
Utility
Buoy array of magnetometers
24 Feb 20
A system includes a plurality of magnetometers that are each configured to generate a vector measurement of a magnetic field.
Jay Hansen, John B. Stetson, Michael DiMario
Filed: 28 Feb 17
Utility
High trim demand relief
17 Feb 20
A flight control system includes a flight control computer operable in a flight state and a ground state.
Anthony Litwinowicz, Kenneth S. Wittmer
Filed: 10 Apr 17
Utility
Main rotor trim tab retention system, an aircraft employing same and a method of replacing a trim tab assembly from blade housing
17 Feb 20
A main rotor trim tab retention system includes, a blade housing having flanges separated by a cavity defined between the flanges, and a trim tab assembly.
Krzysztof Kopanski, Frank Caputo
Filed: 5 Nov 15
Utility
AFT exhaust system for rotary wing aircraft
17 Feb 20
An exhaust system for reducing infrared emissions of a rotary wing aircraft includes a duct assembly having an inlet portion and an outlet portion; the inlet portion configured to receive exhaust from an engine of the aircraft; and the outlet portion coupled to the inlet portion, the outlet portion having an outlet duct with an outlet opening, the outlet duct configured expel an emission containing engine exhaust proximate to a tail fairing of the rotary wing aircraft.
Joseph Pantalone, III, Ashley DeVito, John S. Chapkovich, III, Steven D. Weiner
Filed: 8 Oct 13