Gulfstream Aerospace Corporation

Kristin Medin

Scott Bohanan

Jeffrey Hausmann

Jim Jordan

Matthew Wallace

Stephen Spencer

Andrew Martin

Dean Knight

Ozan Ates

Timothy O'Hara

Michael Knight

John Bullock

Sean Thornton

Scott Martin

Bethany Davis

Nicholas Kershaw

Josh Tatum

Christopher Watkins

Jeffrey Good

Gary Freeman

Colleen Nilson

Melissa Curtis

Zachary Grether

Kamen Kostov

Preeti Menon

Kenneth Carden

Theron Mcdaniel

A throttle quadrant system for an aircraft includes: a first throttle handle to control a first engine of the aircraft, the first throttle handle having a first activatable visual indicator integrated therein; a second throttle handle to control a second engine of the aircraft, the second throttle handle comprising a second activatable visual indicator integrated therein; and at least one controller to control activation and operation of the first activatable visual indicator and the second activatable visual indicator. The at least one controller responds to first engine data related to operating status of the first engine to selectively activate the first activatable visual indicator. The at least one controller also responds to second engine data related to operating status of the second engine to selectively activate the second activatable visual indicator.

Aircraft throttle quadrant assembly with integrated visual indicator feature

An engine inlet cover and a method for covering an engine inlet are provided. A method for covering an engine inlet includes providing a collapsible cover comprising a connection pin defining an axis; a frame including interconnected arms; and a web. Further, the method includes storing the collapsible cover in a stowed configuration in which the arms are aligned. Also, the method includes rotating the arms from the stowed configuration to an operating configuration in which the arms are radially spaced about the axis, enclosing the frame in the operating configuration with the web to define an interior volume, and placing the cover over the engine inlet.

Collapsible cover for engine inlet and method for covering engine inlet

A flight guidance panel for an aircraft includes a subpanel display, a joystick, rotary encoders, a deflection sensor, and a processor. The subpanel display indicates autopilot modes and flight value goals and has a top-level state and a subpanel control state. The joystick is for user interaction with the subpanel display. The rotary encoder is coupled with the joystick to receive rotation inputs from a user of the joystick. The deflection sensor is coupled with the joystick to detect a deflection input from the user of the joystick. The processor is programmed to: change a state of the subpanel display to the subpanel control state corresponding to a selected subpanel in response to receiving the deflection input while the subpanel display is in the top-level state; and change the flight value goals in response to receiving the rotation inputs while the subpanel display is in the subpanel control state.

Flight guidance panels with joystick controls

A method and apparatus for providing an occupant tracking lighting system including a first light, a second light and a third light within an aircraft cabin including detecting, by a sensor, a location and a velocity of a moving occupant, generating, by a processor, a control signal to illuminate the first light and the second light in response to determining that the location is proximate to the first location and that the velocity being towards the second location, and illuminating, by a controller, the first light and the second light in response to the control signal.

Occupant tracking lighting system

An aircraft includes a video display, first and second wireless pairing transmitters, and a media distribution processor. The video display is associated with an audio content stream and a seating location in the aircraft. The first wireless pairing transmitter is associated with the video display and has a first wireless coverage volume. The second wireless pairing transmitter has a second wireless coverage volume that overlaps the first wireless coverage volume. The media distribution processor is programmed and configured to: associate a wireless speaker device with the seating location; pair the first wireless pairing transmitter with the wireless speaker device in response to associating the wireless speaker device with the seating location; and direct the audio content stream through the first wireless pairing transmitter to the wireless speaker device in response to connecting the first wireless pairing transmitter with the wireless speaker device.

Aircraft wireless speaker pairing management with multiple pairing transmitters

Flight control information systems, flight guidance display, and aircraft are provided. A navigational information system includes an input configured to receive a flight plan wherein the flight plan includes a first waypoint, a second waypoint, a third waypoint, and future waypoints, a user interface operative to generate a control signal in response to a user input, a display configured to display a graphical user interface, a processor operative to receive the flight plan from the input, to generate the graphical user interface to include to the first waypoint and the second waypoint and to couple the graphical user interface to the display, the processor being further operative to generate the graphical user interface in to include the first waypoint and the third waypoint in response to the control signal and to couple the graphical user interface to the display.

Advanced flight guidance panel with display of future waypoints and constraints

A flight guidance panel for an aircraft includes a first user input portion, a second user input portion, a display, and a controller. The display is disposed between the first user input portion and the second user input portion. The controller is configured for generating a first functional panel associated with a first flight parameter for presentation on the display. The controller is further configured for generating a second functional panel associated with a second flight parameter for presentation on the display.

Aircraft flight guidance panels with a display disposed between two input portions

Interior panels for interiors of aircraft, aircraft, and methods from making interior panels for interiors of aircraft are provided. In one example, the interior panel includes an outer covering that has a first surface. The first surface is configured to be exposed to the interior of the aircraft. A second surface is disposed opposite the first surface. The second surface has a first pattern formed therein that is hidden from the first surface. A first light source is operative to generate a first light and is disposed adjacent to the second surface generally aligned with the first pattern. When the first light source generates the first light, a first illuminated pattern corresponding to the first pattern formed in the second surface is visible on the first surface.

Interior panel for an interior of an aircraft and a method for making the same

An aircraft includes a display, a support system, and an avionics system. The support system includes at least one operable component, where at least one of the support system and the at least one operable component is configured to operate with an operating value falling within a predefined normal operating range. The avionics system is programmed to: calculate a rate of change of a value of at least one of the support system and the at least one operable component; determine whether the value will exit a predetermined normal operating range within a predetermined time based on the rate of change of the value; and indicate on the display that the value is expected to exit the predetermined normal operating range. The avionics system can leverage this function to declutter displays, and then present additional information to the crew when a value is trending out of range.

Trend indications for avionics systems

The present application teaches methods and apparatuses related to providing dynamic auxiliary port power management including providing a first current to a first auxiliary port and a second current to a second auxiliary port, determining a system power level in response to the first current and the second current, comparing the system power level to a system power level threshold, and providing a third current to the second auxiliary port in response to the system power level exceeding the system power level threshold, the third current having a lower amperage than the second current.

Method and apparatus for dynamic auxiliary port power management

A flight guidance panel includes a housing, a first flight guidance display, a second flight guidance display, a standby display, and a controller. The housing defines a first longitudinal side and a second longitudinal side. The first flight guidance display is disposed in the first longitudinal side of the housing and the second flight guidance display is disposed in the second longitudinal side of the housing. The standby display is disposed between the first flight guidance display and the second flight guidance display. The controller is configured for generating at least one functional panel indicating flight parameters on the first flight guidance display and on the second flight guidance display. The controller is further configured for generating standby flight information for presentation on the standby display.

Aircraft flight guidance panels with integrated standby displays

The present application relates to providing auxiliary port function distinction by illuminating a first light emitting diode around a data transfer capable port wherein the first light emitting diode is illuminated in a first color, illuminating a second light emitting diode around a charge only port, receiving a first data connection request at the charge only port, illuminating the first light emitting diode a second color in response to the data connection request, receiving a second data connection request at the data transfer capable port, initiating a data connection handshake between a device connected to the data transfer capable port and a processor in response to the second data connection request, and illuminating the first light emitting diode the second color in response to the initiation of the data connection handshake.

Growing community of inventors

Savannah, GA, United States of America

Kristin Medin