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Gulfstream Aerospace Corporation patents


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

ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "G" | Gulfstream Aerospace Corporation-related inventors


System for controlling a wheel brake of an aircraft

A system is provided having a normal operational mode and a modulated operational mode. The system includes an input device configured to generate a command signal. ... Gulfstream Aerospace Corporation

Systems and methods for controlling a magnitude of a sonic boom

A method of controlling a magnitude of a sonic boom caused by off-design-condition operation of a supersonic aircraft at supersonic speeds includes, but is not limited to the step of operating the supersonic aircraft at supersonic speeds and at an off-design-condition. The supersonic aircraft has a pair of swept wings having a plurality of composite plies oriented at an angle such that an axis of greatest stiffness is non-parallel with respect to a rear spar of each wing of the pair of swept wings. ... Gulfstream Aerospace Corporation

Composite aircraft manufacturing tooling and methods using articulating mandrels

Composite tooling systems and methods of manufacturing composite stringers of aircraft are provided herein. A composite tooling system includes a layup tool and an articulating stringer mandrel. ... Gulfstream Aerospace Corporation

Ultrasonic cable tie system

An ultrasonic cable tie system is disclosed herein. The ultrasonic cable tie system includes a housing having a tying portion for receiving a bundle of wires to be tied into a cable. ... Gulfstream Aerospace Corporation

Aircraft and deployable vision systems for aircraft

Aircraft, vision sensor systems, and methods of operating deployable vision systems are provided. An aircraft includes a fuselage and a vision sensor system. ... Gulfstream Aerospace Corporation

Self-switching dual voltage battery

A self-switching dual voltage battery system includes a plurality of battery cell groups connected in series to provide a first voltage between a negative terminal and a first positive terminal. A switch matrix couples a selected one of the plurality of battery cell groups to a second positive terminal to provide a second voltage. ... Gulfstream Aerospace Corporation

In-flight leveling system

The disclosed embodiments relate to an aircraft having an in-flight leveling system for a seat onboard the aircraft that includes a swivel mechanism providing selective rotational movement of the a rear portion of the seat to compensate for an angle of inclination of the aircraft during flight. A locking mechanism is coupled to the swivel mechanism to retain the seat in a first position for use on the ground and a second position for use during flight. ... Gulfstream Aerospace Corporation

Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system

An arrangement for use with a propulsion system for a supersonic aircraft includes a center body configured for coupling to an inlet and to support a boundary layer formed when the supersonic aircraft is flown at a predetermined altitude supersonic speed. The arrangement further includes a first vortex generator disposed on the center body. ... Gulfstream Aerospace Corporation

Table including a display

A table is provided including a display. The table includes a base section having a first base section end and a second base section end. ... Gulfstream Aerospace Corporation

Coaxial fluid vent and electronic control for a fluid valve for aircraft

A ventilation system for ventilating a passenger compartment of an aircraft, an aircraft, and a method of operating the ventilation system are disclosed herein. The ventilation system includes, but is not limited to, a bezel, a fluid vent, an electronic sensor, and a valve. ... Gulfstream Aerospace Corporation

Airfoil for an aircraft having reduced noise generation

An airfoil is provided having reduced noise generation for use with an aircraft. The airfoil includes a body and a cover. ... Gulfstream Aerospace Corporation

Controllers and aircraft with pitch and flight path based flight director modes

Avionics systems, controllers, and aircraft are provided. An avionics system includes a display unit and a controller, and an aircraft includes the avionics system. ... Gulfstream Aerospace Corporation

Aircraft with cabin acoustic systems having quarter wavelength absorbers

An aircraft includes a fuselage, a cabin surface, and a first chamber. The cabin surface is disposed within the fuselage and defines a first aperture and at least part of a cabin air mass having a first acoustic mode. ... Gulfstream Aerospace Corporation

Composite reinforcement structures and aircraft assemblies comprising composite reinforcement structures

A composite reinforcement structure including a first skin having a first end and a second end and a second skin having a first end and a second end. The first end of the first skin and the first end of the second skin are coupled. ... Gulfstream Aerospace Corporation

02/08/18 / #20180037313

Controlling elevator to stabilizer offload in fly-by-wire aircraft systems

A control unit for controlling movement of a stabilizer and an elevator on an aircraft, the control unit comprising a processor which is configured to receive a pitch reference command from a flight control input device of the aircraft, determine, based on the pitch reference command, an elevator command configured to command the elevator in the aircraft nose-up or nose-down direction, determine a difference between the elevator command and a desired elevator value corresponding to the pitch reference command, determine a threshold value as a desired maximum elevator deflection at a given pitch reference command, compare the difference with the threshold value and in response thereto generate a command signal configured to retain a current position of the stabilizer when the difference is smaller than or equal to the threshold value, and to command the elevator in the aircraft nose-up or nose-down direction based on the pitch reference command.. . ... Gulfstream Aerospace Corporation

02/01/18 / #20180029714

Seat track assemblies for vibration isolation of floor mounted components

Aircraft, vibration isolation assemblies, and methods of assembling vibration isolation assemblies are provided. An aircraft includes a vibration isolation assembly. ... Gulfstream Aerospace Corporation

12/07/17 / #20170352977

Backshell installation guide

An installation guide for a backshell installation guide is disclosed herein. The installation guide includes a first feature formed therein to receive at least a portion of the backshell to retain the backshell in the installation guide. ... Gulfstream Aerospace Corporation

11/16/17 / #20170331216

Backshell guard for an avionics unit

A guard for a backshell of an aircraft avionics unit is disclosed herein. The guard includes a guard body having a first feature formed therein to slidably receive a first portion of the backshell, a second feature formed therein to slidably receive a second portion of the backshell and a third feature formed therein to protectively cover a mating connector area when the backshell has been slid into the guard body.. ... Gulfstream Aerospace Corporation

10/12/17 / #20170294132

Wearable aircraft towing collision warning devices and methods

The disclosed embodiments describe collision warning devices, controllers, and computer readable media. A collision warning device for towing vehicles includes a housing, a scanning sensor, a display, and a controller. ... Gulfstream Aerospace Corporation

10/12/17 / #20170291722

Methods and systems for providing a data-driven aircraft health report

In one embodiment, a method for monitoring performance of an aircraft against maximum aircraft performance specifications during flight is provided. The method receives, by a processor on the aircraft, a plurality of sensor signals from a respective plurality of sensors onboard the aircraft and individually compares each of the plurality of sensor signals to a respective maximum aircraft performance specification. ... Gulfstream Aerospace Corporation

10/12/17 / #20170291716

Cockpit augmented vision system for aircraft

The disclosed embodiments relate to a cockpit augmented vision unit (cavu) is provided that includes a video signal feed, a housing configured to house a display, and an attachment mechanism coupled to the housing that is configured to secure the housing and the display to an oxygen mask. The video signal feed can be communicatively coupled to at least one source of a video signal, and the display can be coupled to the video signal feed. ... Gulfstream Aerospace Corporation

10/05/17 / #20170283093

Emission-capturing apparatus and method for capturing emissions from an ejection port

An emission-capturing apparatus includes a tank having an inlet and an outlet. The apparatus further includes a muffler fluidly coupled with the outlet to intercept fluid exiting the outlet, permit passage of gas through the muffler, and inhibit passage of liquid through the muffler. ... Gulfstream Aerospace Corporation

10/05/17 / #20170283076

Arrangements and methods for supplying heated air to a wing anti-icing system

An arrangement for supplying heated air to a wing anti-icing system on an aircraft propelled by a jet engine includes, but is not limited to, an ejector that is configured for coupling to a wing anti-icing system. The ejector is further configured to receive a first flow of air, to entrain a second flow of air with the first flow of air, the second flow of air having a lower temperature than the first flow of air, to mix the first flow of air with the second flow of air to form a combined flow having a temperature and a volume suitable for use by the wing anti-icing system, and to exhaust the combined flow into the wing anti-icing system.. ... Gulfstream Aerospace Corporation

10/05/17 / #20170282411

Composite tools and methods for fabricating composite tools

Methods for fabricating composite tools and composite tools are provided. In an exemplary embodiment, a method for fabricating a composite tool includes providing a master mold and forming a low temperature cured resin laminate overlying the master mold. ... Gulfstream Aerospace Corporation

10/05/17 / #20170280871

Method for machining drawers of an article of furniture

A method for machining a plurality of surfaces of a respective plurality of drawers in an article of furniture includes mounting the article of furniture to a support structure to form a work piece, positioning the work piece on a base of a vertical gantry router in an orientation such that the plurality of surfaces are generally perpendicular to a cutting head of the vertical gantry router, and machining the plurality of surfaces with the vertical gantry router until the plurality of surfaces are substantially flat and substantially coplanar with one another.. . ... Gulfstream Aerospace Corporation

09/28/17 / #20170275934

Tunable stay for aircraft compartment closure

A tunable stay device for an aircraft closure has a mounting base that is mountable to the closure or in an area of the aircraft in close proximity to the closure. The mounting base extends, at least in part, along a mounting axis. ... Gulfstream Aerospace Corporation

09/28/17 / #20170275017

Electronic checklists with dynamic visibility of annotations

Display systems, controllers, and methods are provided. A display system for an aircraft includes a display unit, an input device, and a controller. ... Gulfstream Aerospace Corporation

09/14/17 / #20170259935

Reconfigurable flight guidance panels for transport category aircraft

Flight guidance panels and vehicle guidance panels are provided. A flight guidance panel for an aircraft includes a hardware knob, a display proximate the hardware knob, and a controller. ... Gulfstream Aerospace Corporation

07/27/17 / #20170210460

Aircraft door with retractable header

The disclosed embodiments relate to an aircraft having an interior cabin door with a retractable header. Accordingly to non-limiting embodiments, an interior cabin door for an aircraft includes a door panel having an opening in a top portion thereof. ... Gulfstream Aerospace Corporation

07/27/17 / #20170210459

Aircraft air stair support

Air stair support systems, stair support cable assemblies, and hooks are disclosed herein. A stair support system includes, but is not limited to, an aircraft fuselage, a door seal, a stair door, and a stair support cable assembly. ... Gulfstream Aerospace Corporation

07/13/17 / #20170197726

Aircraft instrumentation systems for displaying electronic circuit breaker information

Aircraft instrumentation systems and controllers are provided. An aircraft instrumentation system includes a display and a controller. ... Gulfstream Aerospace Corporation

06/22/17 / #20170174358

Systems and methods for multilingual aircraft towing collision warning

Collision warning systems, collision warning devices, and methods of operating collision warning systems are disclosed herein. A collision warning system includes, but is not limited to, a plurality of proximity sensors and a computer device. ... Gulfstream Aerospace Corporation

06/22/17 / #20170174356

Auxiliary power unit inlet duct assembly for mitigating noise

An auxiliary power unit inlet assembly includes an inlet duct having a first end and a second end. The auxiliary power unit inlet assembly further includes a door associated with the second end of the inlet duct. ... Gulfstream Aerospace Corporation

06/15/17 / #20170165907

Composite aircraft manufacturing tooling and methods using articulating mandrels

Composite tooling systems and methods of manufacturing composite stringers of aircraft are provided herein. A composite tooling system includes a layup tool and an articulating stringer mandrel. ... Gulfstream Aerospace Corporation

04/13/17 / #20170101067

Integrated power distribution, data network, and control architectures for a vehicle

An integrated power distribution, data network, and control architecture for a vehicle is provided that includes nodes distributed throughout the vehicle. Each node includes power distribution (pd) and data collection and distribution (dcd) components. ... Gulfstream Aerospace Corporation

03/30/17 / #20170089471

Ventilation systems and gasper valves with flexible components

Ventilation systems and gasper valves for ventilating passenger compartments of aircraft are disclosed herein. The ventilation system includes, but is not limited to, an air supply conduit and a gasper valve. ... Gulfstream Aerospace Corporation

03/30/17 / #20170088285

Aircraft instrumentation systems for displaying electronic circuit breaker information

Aircraft instrumentation systems and controllers are provided. An aircraft instrumentation system includes a display and a controller. ... Gulfstream Aerospace Corporation

03/23/17 / #20170081044

Load assembly and method for lifting a load into an aircraft

A load assembly for use with an aircraft includes a support sub-assembly and a lifting sub-assembly. The support sub-assembly is configured for removable coupling to a structural member of the aircraft. ... Gulfstream Aerospace Corporation

02/16/17 / #20170043859

Trailing edge components, aircraft structures including trailing edge components and methods for manufacturing trailing edge components

Trailing edge components of aircraft structures, aircraft structures comprising such trialing edge components, and methods of manufacturing such trailing edge components are provided. In an exemplary embodiment, a trailing edge component includes a first skin comprising a first plurality of plies of carbon fiber reinforced polymer material and having a first mating region. ... Gulfstream Aerospace Corporation

02/02/17 / #20170029137

Methods for manufacturing an i-stringer of an aircraft and devices for use in such methods

Methods for manufacturing a reinforced composite structure for an aircraft and devices used in such methods are provided. A device includes a base, a first support member fixedly attached to the base, and a second support member fixedly attached to the base and aligned longitudinally with the first support member. ... Gulfstream Aerospace Corporation

01/12/17 / #20170008608

Self-adjusting door jamb for an aircraft door

The disclosed embodiments relate to an aircraft having an interior door with a self-adjusting door jamb. The self-adjusting door jamb includes a door jamb configured to receive the interior door and a bias mechanism coupled to the door jamb and facilitating movement of the door jamb along an axis. ... Gulfstream Aerospace Corporation








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