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公开(公告)号：US12072206B2
公开(公告)日：2024-08-27
申请号：US17028036
申请日：2020-09-22
IPC分类号： G06F3/048 , B64D43/00 , G01C5/00 , G01C21/20 , G01C23/00 , G06F3/0482 , G06F3/0483 , G06F3/0484 , G06T11/20 , G08G5/00 , G10L15/26
CPC分类号： G01C23/005 , G01C5/005 , G01C21/20 , G08G5/0021
摘要： Methods and systems of generating a data driven digital chart. The methods and systems include retrieving a data driven chart for a requested terminal area procedure chart from a database of data driven charts. The data driven charts describe digital terminal area procedure charts by way of data elements for each terminal area procedure chart including geodetic straights, arcs, text elements and symbols defined with respect to location. Some of the data elements are further defined with respect to altitude values assuming a standard atmospheric temperature value. The systems and methods include calculating compensated altitude values for the data elements of the retrieved data driven chart based on a deviation between the outside air temperature value and the standard atmospheric temperature value. The methods and systems include generating a presentation for a display device of the aircraft of the terminal area procedure chart.
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公开(公告)号：US11983023B2
公开(公告)日：2024-05-14
申请号：US16252998
申请日：2019-01-21
申请人： The Boeing Company
IPC分类号： G05D23/22 , B29C35/02 , B29C51/42 , B29C51/46 , B29C71/02 , B29C73/34 , B32B17/10 , B64C1/14 , B64F5/40 , G01C23/00 , G05D23/27 , H05B1/02 , H05B3/84 , B29K101/10 , B29K105/00 , B29L31/00 , B29L31/30
CPC分类号： G05D23/22 , B29C35/0288 , B29C51/421 , B29C51/46 , B29C71/02 , B29C73/34 , B32B17/10963 , B64C1/1476 , B64C1/1484 , B64F5/40 , G01C23/005 , G05D23/27 , H05B1/0236 , H05B3/84 , B29K2101/10 , B29K2105/256 , B29K2995/0026 , B29L2031/3052 , B29L2031/778 , B32B2309/025 , B32B2369/00
摘要： Methods systems and apparatuses for reducing or substantially eliminating distortion in a transparent substrate in situ are disclosed.
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3.发明公开公开(公告)号：US20240124153A1
公开(公告)日：2024-04-18
申请号：US18069375
申请日：2022-12-21
CPC分类号： B64D45/00 , G01C23/00 , B64C29/0008
摘要： A method of providing contextual display modes for a vertical takeoff and landing (VTOL) vehicle including obtaining aircraft flight information including a current position and altitude; retrieving vertiport information for a vertiport at the current position of the aircraft; displaying, to one or more operators of the aircraft, a takeoff synthetic vision display mode; transitioning, as the current altitude approaches the transitional altitude, from the takeoff synthetic vision display mode to a cruise synthetic vision display mode, wherein the cruise synthetic vision display mode represents the view from a cruise display viewpoint at the current altitude of the aircraft and at the current position of the aircraft; and displaying, in response to the current altitude equaling or exceeding the transitional altitude, the cruise synthetic vision display mode.
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公开(公告)号：US11959773B2
公开(公告)日：2024-04-16
申请号：US16901943
申请日：2020-06-15
CPC分类号： G01C23/005 , B64D43/00
摘要： A system and method for determining a lateral and vertical path for aircraft guidance from a current aircraft position to a landing runway following a complete loss of engine thrust includes determining, in a processing system, a final approach segment, a deceleration segment, and a driftdown segment. Connecting, in the processing system, the driftdown segment to the deceleration segment, and the deceleration segment to the final approach segment, to form a complete lateral and vertical path from the current aircraft position to the landing runway. And rendering, on a display device, a graphical representation of the complete lateral and vertical path from the current aircraft position to the landing runway, wherein the graphical representation of the complete lateral and vertical path updates as the aircraft travels.
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公开(公告)号：US11940527B2
公开(公告)日：2024-03-26
申请号：US17130553
申请日：2020-12-22
CPC分类号： G01S13/953 , B64D45/00 , B64D47/08 , G01C23/005 , G01S13/867 , G06N20/00
摘要： A synthetic visual system for an aircraft may comprise: a camera in electronic communication with a controller; a radar system in electronic communication with the controller; a three-dimensional cockpit display in electronic communication with the controller via a synthetic weather system; and a tangible, non-transitory memory configured to communicate with the controller. The three-dimensional cockpit display may be configured to display a three-dimensional weather image based on correlated data between the radar system and the camera.
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公开(公告)号：US11927460B2
公开(公告)日：2024-03-12
申请号：US16757603
申请日：2018-10-24
申请人： BAE SYSTEMS plc
CPC分类号： G01C23/005 , B64D45/00
摘要： Diverse types of crew interfaces (400, 430, 450) are provided for outputting visible, audio and tactile information to a pilot for flight control. A unified estimation of the current aircraft state and of a current phase of flight are made (110), based on flight status information. Respective coordinated visible, audio and tactile presentations for the diverse types of crew interfaces are generated, (120) coordinated so that they provide mutually consistent indications of the unified estimation of the current aircraft state, according to the unified estimation of current flight phase. The respective coordinated presentations are output (130) by the diverse types of crew interfaces to the pilot. By coordinating crew interface outputs across sight, sound and touch senses, this can relieve the pilot of workload in interpreting unsynchronised or incoherent outputs from different types of interfaces.
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公开(公告)号：US20230406533A1
公开(公告)日：2023-12-21
申请号：US18459096
申请日：2023-08-31
IPC分类号： B64D43/00 , A42B3/30 , G06F3/01 , G01C23/00 , G08G5/00 , B64C13/18 , B64C13/22 , A42B3/04 , A42B3/22 , G06T19/00 , G02B27/01 , B64D11/06 , B64C13/04 , B64C1/06 , B64C1/18 , B64C1/40
CPC分类号： B64D43/00 , A42B3/30 , G06F3/012 , G06F3/017 , G01C23/005 , G08G5/0004 , G08G5/0017 , G08G5/0039 , G08G5/0091 , G08G5/0047 , B64C13/18 , B64C13/22 , A42B3/042 , A42B3/0433 , A42B3/228 , G06T19/006 , G01C23/00 , G08G5/0021 , G02B27/017 , B64D11/0647 , B64C13/044 , B64C13/042 , B64D11/0689 , B64D11/0626 , B64C1/066 , B64C1/18 , B64C1/40 , G06F3/044
摘要： The present invention achieves technical advantages as an aircraft having an augmented reality flight control system integrated with and operable from the pilot seat and an associated pilot headgear unit, wherein the flight control system is supplemented by flight-assisting artificial intelligence and geo-location systems. The present invention includes an augmented reality flight control system incorporating real-world objects with virtual elements to provide relevant data to a pilot during aircraft flight. A translucent substrate is disposed in the pilot's field of view such that the pilot can see therethrough, and observe virtual elements displayed on the substrate. The system includes a headgear that is worn by the pilot. A flight assistance module is configured to receive data related to the aircraft and provide predictive assistance to the pilot during flight based on the received data based in part on a pilot profile having preferences related to the pilot.
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公开(公告)号：US20230376049A1
公开(公告)日：2023-11-23
申请号：US18228273
申请日：2023-07-31
申请人： BETA AIR, LLC
IPC分类号： G05D1/10 , B64D27/24 , B64D43/00 , G01C23/00 , G05D1/00 , G06F21/60 , G06F16/22 , G06F3/14 , H04L9/40
CPC分类号： G05D1/101 , B64D27/24 , B64D43/00 , G01C23/005 , G05D1/0038 , G06F21/602 , G06F16/22 , G06F3/14 , H04L63/0884 , G06Q50/30
摘要： A system for automated flight plan reporting for an electric aircraft, the system including a flight controller coupled to the electric aircraft configured to receive a digital datum from a remote device, generate a plan adjustment datum as a function of the digital datum, and transmit the plan adjustment datum to a pilot display, a pilot display coupled to the electric aircraft, wherein the pilot display is configured to receive the plan adjustment datum from the flight controller, display the plan adjustment datum to a user; and receive a confirmation datum from the user.
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公开(公告)号：US11816996B1
公开(公告)日：2023-11-14
申请号：US16714299
申请日：2019-12-13
CPC分类号： G08G5/0021 , G01C23/005 , G01H17/00 , G08G5/006 , G08G5/0039
摘要： A system for predicting pressure waves in a sonic boom footprint calculates alternative footprints and pressure waves along a flight path based on speed and altitude modifiers. The available, adjustable parameters are bounded within a flight envelope and along an approved flight corridor. The system receives and incorporates data from external sources, such as weather data, that impacts sonic boom pressure wave predictions and aircraft performance characteristics.
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公开(公告)号：US11796558B2
公开(公告)日：2023-10-24
申请号：US17081439
申请日：2020-10-27
申请人： AIRBUS HELICOPTERS
发明人： Jean-Paul Petillon
摘要： A method and apparatus for estimating an airspeed of a rotorcraft by analyzing its rotor. The rotorcraft includes a fuselage and a main rotor that is equipped with a plurality of blades and that rotates about an axis of a hub of the rotor, and in which the free end or “tip” of each blade describes a path in the vicinity of a tip-path plane. The method makes it possible to determine said airspeed of the rotorcraft in a frame of reference united with the tip-path plane by solving a model of the rotor that puts a pitch angle of at least one blade relative to the tip-path plane into relation with the airspeed of the rotorcraft and with an auxiliary speed. The auxiliary speed may be an induced velocity of the air flowing through the rotor or else an axial airspeed at the upstream infinity of the rotorcraft.
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