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11.外观设计公开(公告)号：USD1019671S1
公开(公告)日：2024-03-26
申请号：US29788143
申请日：2021-03-29
Applicant: Gulfstream Aerospace Corporation
Designer： Vincent Poudou , Brendan Moran
Abstract: FIG. 1 is a front view of an avionics display screen with graphical user interface for shark tooth auto-throttle anticipation cues showing our new design; and,
FIG. 2 is a second embodiment thereof.
The broken lines showing the avionics display screen form no part of the claimed design.-
公开(公告)号：USD1011570S1
公开(公告)日：2024-01-16
申请号：US29709818
申请日：2019-10-17
Applicant: Gulfstream Aerospace Corporation
Designer： Joe Guthrie , Katherine Young
Abstract: FIG. 1 is a perspective view of an indirect lighting arrangement for a vehicle showing our new design;
FIG. 2 is a bottom view thereof;
FIG. 3 is a top view thereof;
FIG. 4 is a side view looking in a port direction;
FIG. 5 is a side view looking in a starboard direction;
FIG. 6 is a side view looking in an aft direction;
FIG. 7 is a side view looking in a forward direction; and,
FIG. 8 is a sectional view of the indirect lighting arrangement depicted in FIG. 2 along line 8-8.
The broken lines illustrate structure and environment that form no part of the claimed design.-
公开(公告)号：US20230358779A1
公开(公告)日：2023-11-09
申请号：US17662594
申请日：2022-05-09
Applicant: Gulfstream Aerospace Corporation
Inventor： Thomas Landers , Michael Malluck
CPC classification number: G01P5/16 , G01C21/16 , G01P3/00 , G01S19/13 , B64D45/00 , B64C13/503 , B64D43/02
Abstract: A method of checking accuracy of an air data probe system onboard a vehicle is disclosed. An embodiment of the method involves: calculating airspeed measurements from air data provided by the probe system; calculating vehicle speed measurements based on sensor data collected from at least one sensor system onboard the vehicle, wherein the vehicle speed measurements are distinct and independent of the airspeed measurements, and the vehicle speed measurements are calculated without using the air data; comparing a calculated airspeed measurement against a calculated vehicle speed measurement to obtain a speed difference, wherein the calculated airspeed measurement and the calculated vehicle speed measurement correspond to a measurement time during which the vehicle is moving forward; and initiating at least one corrective action onboard the vehicle when magnitude of the speed difference exceeds a threshold value.
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14.发明公开公开(公告)号：US20230335138A1
公开(公告)日：2023-10-19
申请号：US17659199
申请日：2022-04-14
Applicant: Gulfstream Aerospace Corporation
Inventor： Christopher Nusbaum , Brian Toler
CPC classification number: G10L17/22 , G10L17/04 , G10L17/18 , G10L17/06 , G06T13/00 , B64D11/0015 , G01V11/00
Abstract: A system onboard an aircraft includes: a proximity sensor to detect users within an area; a display monitor in the area; a processor; and a processor-readable medium storing executable instructions to perform a method that involves: detecting presence of a user within the area, based on output of the sensor; causing display of an animated digital representation of an assistant on the monitor; controlling the animated digital representation of the assistant to react to speech input; processing speech input of the user to identify at least one action to be carried out onboard the aircraft; controlling the animated digital representation of the assistant to respond to the identified at least one action; and issuing at least one command, instruction, or control signal to the component onboard the aircraft, to initiate the identified at least one action.
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公开(公告)号：US20230320488A1
公开(公告)日：2023-10-12
申请号：US17658736
申请日：2022-04-11
Applicant: Gulfstream Aerospace Corporation
Inventor： Jeremiah Mallette
IPC: A47C7/14
Abstract: An inflatable bladder includes, but is not limited to, a bladder body having a wall, a longitudinal dimension, and a lateral dimension. The wall defines an interior volume enclosing a fluid. The wall further defines an opening in fluid communication with the interior volume. The bladder body is fluid tight when the opening is closed. The wall is configured to facilitate an expansion of the longitudinal dimension during an ingress of the fluid into the interior volume and a contraction of the longitudinal dimension during an egress of the fluid from the interior volume. The wall is further configured to maintain a constant lateral dimension during the ingress of the fluid into the interior volume and a constant lateral dimension during the egress of the fluid from the interior volume.
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Patent Agency Ranking
16.发明公开公开(公告)号：US20230312129A1
公开(公告)日：2023-10-05
申请号：US17658067
申请日：2022-04-05
Applicant: Gulfstream Aerospace Corporation
Inventor： Brian Toler
IPC: B64D43/00 , H04N5/232 , H04N13/302 , H04N13/239 , B64D47/08 , G02B27/01
CPC classification number: B64D43/00 , H04N5/23229 , H04N13/302 , H04N13/239 , B64D47/08 , G02B27/0101 , G02B2027/0138 , G02B2027/014
Abstract: A display system is provided for a vehicle having a windshield and vehicle structure outside the windshield. The vehicle structure is visible within a field of view defined by the windshield. Certain embodiments of the display system include: a camera to capture image data for a visually obstructed portion of an environment outside the vehicle, wherein the visually obstructed portion of the environment is hidden by the vehicle structure; a controller configured to process the image data captured by the camera into a head-up display (HUD) image that represents the visually obstructed portion of the environment; a HUD element configured to present projected images that are visible to an occupant of the vehicle; and a projector coupled to the controller and configured to project the HUD image toward the HUD element, such that the HUD image is visible overlying the vehicle structure.
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公开(公告)号：US20230306856A1
公开(公告)日：2023-09-28
申请号：US18324016
申请日：2023-05-25
Applicant: Gulfstream Aerospace Corporation
Inventor： Sergio Ferreira , Brendan Moran
CPC classification number: G08G5/0086 , G08G5/0013 , G08G5/0021 , G08G5/025
Abstract: Vertical resolution and/or vertical accuracy of terrain elevation data near an aircraft runway is adjusted by obtaining local terrain data, yielding a first elevation value for a query location. A processor receptive of the first elevation value computes plane equations based on a predetermined standard model adapted to geometrically conform to the aircraft runway, yielding a second elevation value for the query location. The processor selectively uses the first and second elevation values to generate an adjusted elevation value that is supplied to a terrain avoidance and warning system.
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公开(公告)号：US20230249837A1
公开(公告)日：2023-08-10
申请号：US17650318
申请日：2022-02-08
Applicant: Gulfstream Aerospace Corporation
Inventor： Donald Freund , Derek Muzychka , Douglas Klutzke
Abstract: An inlet arrangement for a propulsion system includes an actuator, a linkage and an inlet assembly. The inlet assembly includes (1) a lip, (2) a cowl extending downstream from the lip, the cowl defining an external surface of the inlet assembly, (3) an inlet duct extending downstream from the lip, the inlet duct disposed radially inward of the cowl, and (4) a movable component associated with the lip, the cowl, or the inlet duct. An outer surface of the inlet duct and an inner surface of the cowl define a gap therebetween. The linkage is disposed in the gap and coupled with the moveable component. The linkage is configured to move within the gap and to move the moveable component when the linkage moves. The actuator is coupled with the linkage and moves the linkage when the actuator is actuated. The actuator is mounted remotely from the inlet assembly.
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公开(公告)号：US20230245576A1
公开(公告)日：2023-08-03
申请号：US18295124
申请日：2023-04-03
Applicant: Gulfstream Aerospace Corporation
Inventor： Kevin Prosser , Thomas Landers , Abhishek Vaidya , Alborz Sakhaei , Blake Finlayson
CPC classification number: G08G5/045 , G05D1/106 , G08G5/0086
Abstract: The aircraft threat envelope protection system employs a threat envelope data structure in a computer-readable medium that stores at least one trigger condition for each of a plurality of different types of threats associated with the aircraft, and modeled using a common schema. A processor computes plural different projected trajectories representing different possible aircraft paths through spacetime. The processor associates at least some of the plurality of the threats to specific trigger points in spacetime along each of the projected trajectories. The processor will deprecate ones of the projected trajectories when they are deemed not viable to recover from a threat. The processor initiates an aircraft protective response when all projected trajectories but one have been deprecated and the aircraft is within a predetermined proximity to the closest trigger point in spacetime along the non-deprecated trajectory.
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公开(公告)号：US11649032B2
公开(公告)日：2023-05-16
申请号：US16949182
申请日：2020-10-19
Applicant: Gulfstream Aerospace Corporation
Inventor： John Bullock , Gregg Kendryna , Laburn DeBenion Saxon
Abstract: Interior panels for an interior of a vehicle, vehicles, and methods for making interior panels for an interior of a vehicle are provided. In one example, the interior panel includes an outer covering having a first surface exposed to the interior and a second surface disposed opposite the first surface. The second surface has a pattern formed therein that is covered by the first surface. A board assembly is disposed proximate the second surface and has a third surface facing towards the second surface. The board assembly includes a light source that is generally aligned with the pattern. An adhesive layer is disposed between the second surface and the third surface and couples the second surface and the third surface together. When the light source generates light, the light passes through the adhesive layer and the pattern to produce an illuminated pattern on the first surface.
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