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公开(公告)号：US12097972B2
公开(公告)日：2024-09-24
申请号：US17648971
申请日：2022-01-26
Applicant: Gulfstream Aerospace Corporation
Inventor： Andrew Martin , Kristin Medin , Scott Bohanan
CPC classification number: B64F1/005 , F02C7/04 , A45B2023/0081 , F05D2220/323 , F05D2230/60
Abstract: 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.
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公开(公告)号：US11440675B2
公开(公告)日：2022-09-13
申请号：US15984658
申请日：2018-05-21
Applicant: Gulfstream Aerospace Corporation
Inventor： Scott Bohanan , Jeffrey Hausmann , Bethany Davis , Andrew Martin , Kristin Medin
IPC: B64D43/00 , G06F3/01 , G06F3/02 , G06F3/0362 , G06F3/04847 , G06F3/04886 , G06F3/14
Abstract: 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.
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公开(公告)号：US20240417104A1
公开(公告)日：2024-12-19
申请号：US18817380
申请日：2024-08-28
Applicant: Gulfstream Aerospace Corporation
Inventor： Andrew Martin , Kristin Medin , Scott Bohanan
Abstract: 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.
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公开(公告)号：US11306664B2
公开(公告)日：2022-04-19
申请号：US16845999
申请日：2020-04-10
Applicant: Gulfstream Aerospace Corporation
Inventor： Craig Ziolkowski , Desmond Ruhan , Todd Abler , Andrew Martin
Abstract: Flight control systems, flight control methods, and aircraft are provided. An aircraft including a system and a method for receiving, via a fuel switch, a first control signal indicative of an off position on a fuel switch, determining a throttle resolver angle of a throttle controller in response to the first control signal, comparing the throttle resolver angle to a threshold throttle angle, and generating a pilot warning in response to the first control signal and the throttle resolver angle exceeding the threshold throttle angle.
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公开(公告)号：US20210317790A1
公开(公告)日：2021-10-14
申请号：US16845999
申请日：2020-04-10
Applicant: Gulfstream Aerospace Corporation
Inventor： Craig Ziolkowski , Desmond Ruhan , Todd Abler , Andrew Martin
Abstract: Flight control systems, flight control methods, and aircraft are provided. An aircraft including a system and a method for receiving, via a fuel switch, a first control signal indicative of an off position on a fuel switch, determining a throttle resolver angle of a throttle controller in response to the first control signal, comparing the throttle resolver angle to a threshold throttle angle, and generating a pilot warning in response to the first control signal and the throttle resolver angle exceeding the threshold throttle angle.
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Patent Agency Ranking
公开(公告)号：US20190352018A1
公开(公告)日：2019-11-21
申请号：US15984658
申请日：2018-05-21
Applicant: Gulfstream Aerospace Corporation
Inventor： Scott Bohanan , Jeffrey Hausmann , Bethany Davis , Andrew Martin , Kristin Medin
IPC: B64D43/00 , G06F3/01 , G06F3/0484 , G06F3/0362 , G06F3/0488 , G06F3/14 , G06F3/02
Abstract: 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.
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公开(公告)号：US10229606B2
公开(公告)日：2019-03-12
申请号：US15246238
申请日：2016-08-24
Applicant: Gulfstream Aerospace Corporation
Inventor： Brendan Moran , Scott Buethe , Andrew Martin , Todd Abler , Thomas Horne
Abstract: Avionics systems, controllers, and aircraft are provided. An avionics system includes a display unit and a controller, and an aircraft includes the avionics system. The display unit is configured to present an image. The controller is communicatively coupled with the display unit and is configured to control the display unit to present the image in a takeoff mode and in a flight mode of the controller. The controller is further configured to receive signals indicating an aircraft attitude, a target attitude, and an aircraft flight path, to generate a marker in the image in the takeoff mode based on an attitude difference between the aircraft attitude and the target attitude, to generate the marker in the image in the flight mode based on the aircraft flight path, and to generate a signal that causes the display unit to present the image.
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公开(公告)号：US20180061250A1
公开(公告)日：2018-03-01
申请号：US15246238
申请日：2016-08-24
Applicant: Gulfstream Aerospace Corporation
Inventor： Brendan Moran , Scott Buethe , Andrew Martin , Todd Abler , Thomas Horne
CPC classification number: G08G5/0065 , B64D43/00 , G01C23/00 , G07C5/0825 , G08G5/0021 , G08G5/0052
Abstract: Avionics systems, controllers, and aircraft are provided. An avionics system includes a display unit and a controller, and an aircraft includes the avionics system. The display unit is configured to present an image. The controller is communicatively coupled with the display unit and is configured to control the display unit to present the image in a takeoff mode and in a flight mode of the controller. The controller is further configured to receive signals indicating an aircraft attitude, a target attitude, and an aircraft flight path, to generate a marker in the image in the takeoff mode based on an attitude difference between the aircraft attitude and the target attitude, to generate the marker in the image in the flight mode based on the aircraft flight path, and to generate a signal that causes the display unit to present the image.
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公开(公告)号：US20230234720A1
公开(公告)日：2023-07-27
申请号：US17648971
申请日：2022-01-26
Applicant: Gulfstream Aerospace Corporation
Inventor： Andrew Martin , Kristin Medin , Scott Bohanan
IPC: F02C7/04
CPC classification number: F02C7/04 , F05D2230/60 , F05D2220/323
Abstract: 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.
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公开(公告)号：US20170259935A1
公开(公告)日：2017-09-14
申请号：US15453005
申请日：2017-03-08
Applicant: Gulfstream Aerospace Corporation
Inventor： Jeffrey Hausmann , Scott Buethe , Andrew Martin
IPC: B64D43/00 , G06F3/041 , G06F3/0362
CPC classification number: B64D43/00 , G06F3/0362 , G06F3/041 , G06F3/04847 , G06F3/0488 , G06F2203/04803 , H03K17/945
Abstract: 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. The controller is configured for: altering an automation state of the aircraft; receiving a target of a flight parameter for the aircraft to achieve when the automation state is active; and generating a functional panel associated with the flight parameter and the hardware knob based on a configuration of the flight guidance panel.
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