公开(公告)号：US20180238996A1

公开(公告)日：2018-08-23

申请号：US15439158

申请日：2017-02-22

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Saravanakumar Gurusamy ,  Madhava Gadicherla ,  Jayasenthilnathan B ,  Roger W Burgin

IPC: G01S7/24 ,  G09G5/36 ,  G09G5/02 ,  G01S13/95 ,  G01S7/00 ,  G08G5/00

CPC classification number: G01S7/24 ,  G01C23/00 ,  G01S7/003 ,  G01S7/062 ,  G01S7/22 ,  G01S7/52036 ,  G01S7/52071 ,  G01S13/953 ,  G01W1/00 ,  G06F3/0484 ,  G08G5/0008 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0026 ,  G08G5/0052 ,  G08G5/0091 ,  G09G5/02 ,  G09G2320/0666 ,  G09G2380/12

Abstract: A method for presenting weather information onboard an aircraft is provided. The method obtains a first set of weather data from aircraft onboard radar system; obtains a second set of weather data from external sources including one or more external aircraft, a satellite, a remote server, and a ground-based weather station, wherein the communication device is compatible a communication protocol for the external sources, and wherein the communication protocol comprises at least one of a datalink communication protocol, a satellite communication protocol, a very high frequency (VHF) radio communication protocol, and a transponder communication protocol; and presents graphical elements comprising a first set of graphical elements associated with the first set of weather data and a second set of graphical elements associated with the second set of weather data, wherein the second set of graphical elements include visual characteristics distinguishable from the first set of graphical elements.

公开(公告)号：US20200348148A1

公开(公告)日：2020-11-05

申请号：US16800470

申请日：2020-02-25

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Jayasenthilnathan B ,  Saravanakumar Gurusamy ,  Richard Mitchel Meldrum ,  Jerry Ball

IPC: G01C23/00 ,  G08G5/00 ,  G09G5/36 ,  B64D45/00 ,  G06F16/29

Abstract: A graphic rendering system for use with certified avionics software onboard an aircraft is disclosed. The graphic rendering system includes a graphic rendering engine that has been certified by governing governmental authority for use in an aircraft for displaying critical information, wherein the graphic rendering engine is configured to access an aircraft-specific graphical database file and an aircraft-specific geographical database file for graphical and geographical data for use in rendering the graphic for display on the cockpit display. Both the aircraft-specific graphical database file and the aircraft-specific geographical database file have been customized for use on the aircraft. The graphic rendering engine is configured to use the aircraft-specific graphical database file and the aircraft-specific geographical database file for rendering the graphic for displaying critical information on the cockpit display without prior certification by governing governmental authority of either the aircraft-specific graphical database file or the aircraft-specific geographical database file.

公开(公告)号：US10139474B2

公开(公告)日：2018-11-27

申请号：US15439158

申请日：2017-02-22

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Saravanakumar Gurusamy ,  Madhava Gadicherla ,  Jayasenthilnathan B ,  Roger W Burgin

IPC: G01S7/24 ,  G09G5/02 ,  G01S13/95 ,  G01S7/00 ,  G08G5/00 ,  G01S7/52 ,  G06F3/0484

Abstract: A method for presenting weather information onboard an aircraft is provided. The method obtains a first set of weather data from aircraft onboard radar system; obtains a second set of weather data from external sources including one or more external aircraft, a satellite, a remote server, and a ground-based weather station, wherein the communication device is compatible a communication protocol for the external sources, and wherein the communication protocol comprises at least one of a datalink communication protocol, a satellite communication protocol, a very high frequency (VHF) radio communication protocol, and a transponder communication protocol; and presents graphical elements comprising a first set of graphical elements associated with the first set of weather data and a second set of graphical elements associated with the second set of weather data, wherein the second set of graphical elements include visual characteristics distinguishable from the first set of graphical elements.

公开(公告)号：US09747807B2

公开(公告)日：2017-08-29

申请号：US14606337

申请日：2015-01-27

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Subash Samuthirapandian ,  Markus Alan Johnson ,  Pramod Kumar Malviya ,  Jayasenthilnathan B ,  Bretislav Passinger

IPC: G06F19/00 ,  G06G7/70 ,  G06G7/76 ,  G08G5/00 ,  G08G5/06 ,  G01C23/00

CPC classification number: G08G5/0021 ,  G01C23/00 ,  G08G5/0013 ,  G08G5/003 ,  G08G5/0039 ,  G08G5/06

Abstract: A flight display system or method in accordance with this disclosure involves the presentation, on an aircraft, of a “quick preview” notice to airmen (“NOTAM”) display that includes a plurality of stacked flight route portion boxes, each of the plurality of flight route portion boxes pertaining to and being labeled as one of: a departure taxiing portion, a standard instrument departure portion, an en route portion, a standard terminal arrival route portion, an approach portion, and an arrival taxiing portion; each of the plurality of flight route portion boxes graphically displaying flight route symbology pertaining to and labeled as each airport taxiing reference point and/or each aeronautical waypoint that falls within its labeled flight route portion; and wherein at least one of the plurality of flight route portion boxes further graphically displays NOTAM symbology pertaining to at least one of the NOTAMs that are relevant to the flight route.

公开(公告)号：US09547993B2

公开(公告)日：2017-01-17

申请号：US14629017

申请日：2015-02-23

Applicant: Honeywell International Inc.

Inventor： Ratan Khatwa ,  Jayasenthilnathan B

IPC: G08G5/06 ,  G08G5/04 ,  G08G5/00 ,  G01S19/51 ,  G01S13/93 ,  B64D45/04 ,  G05D1/00

CPC classification number: G08G5/04 ,  B64D45/04 ,  G01S13/93 ,  G01S19/51 ,  G05D1/0061 ,  G05D1/0083 ,  G05D1/0676 ,  G08G5/0021 ,  G08G5/045 ,  G08G5/06 ,  G08G5/065

Abstract: This disclosure is directed to methods, systems, and computer program products for automated avoidance of ground threats by an aircraft. In one example, a method includes determining, by one or more processing devices, whether a sufficient evasive maneuver for an aircraft to avoid a detected ground surface threat is performed via pilot controls of the aircraft within a selected threshold after an alert of the ground surface threat is outputted via one or more cockpit systems of the aircraft. The method further includes, in response to determining that a sufficient evasive maneuver via the pilot controls is not performed within the selected threshold, controlling, by the one or more processing devices, one or more flight systems of the aircraft to perform an automated evasive maneuver to avoid the ground surface threat.

Abstract translation: 本公开涉及用于自动避免飞机的地面威胁的方法，系统和计算机程序产品。 在一个示例中，一种方法包括通过一个或多个处理装置来确定在飞机的地面的警报之后是否通过飞行员在所选择的阈值内的飞行员控制来执行用于飞机避免检测到的地面威胁的足够的回避机动 通过飞机的一个或多个驾驶舱系统输出威胁。 该方法还包括响应于确定在所选择的阈值内不执行经由导频控制的足够的回避机动，由一个或多个处理装置控制飞行器的一个或多个飞行系统执行自动回避机动 以避免地面的威胁。