-
1.发明申请公开(公告)号：US20150259075A1
公开(公告)日：2015-09-17
申请号：US14216335
申请日：2014-03-17
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Timothy John Case , John Meeker
Abstract: A method and system for maintaining visual vertical reference on a rotorcraft display during rotorcraft landing is provided. The method generates vertical poles and positions them on the rotorcraft display such that vertical reference as well as roll information may be quickly and easily comprehended by a pilot.
Abstract translation: 提供了一种用于在旋翼飞机着陆期间在旋翼飞机显示器上维持视觉垂直参考的方法和系统。 该方法产生垂直极点并将其定位在旋翼航空器显示器上，使得垂直参考以及滚动信息可以被飞行员快速且容易地理解。
-
Patent Agency Ranking
2.发明授权公开(公告)号：US10053224B2
公开(公告)日：2018-08-21
申请号：US15171417
申请日：2016-06-02
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dave Pepitone , John Meeker , Mark Giddings , Ivan Sandy Wyatt , John Suddreth , Aaron Gannon
CPC classification number: B64D43/00 , G01C23/005 , G06F3/04817 , G06F3/14 , G06T11/60 , G06T2210/36 , G06T2210/61 , G08G5/003 , G09G5/02 , G09G5/391 , G09G2320/10 , G09G2340/0407 , G09G2380/12
Abstract: A system method for providing aircraft lateral navigation system capability feedback to a pilot includes determining, in a processor, when a flight plan has been received that includes a flight leg that needs to be captured by the aircraft. A determination is made, in the processor, when an armed signal has been received, where the armed signal indicating that an aircraft autopilot navigation mode (NAV) has been armed. The processor is used to command a display device to render the flight leg using a first display paradigm when the armed signal has not been received, and to render the flight leg using a second display paradigm when the armed signal has been received.
-
3.发明授权System and method for displaying vertical reference on a rotorcraft system 有权用于在旋翼飞机系统上显示垂直参考的系统和方法公开(公告)号：US09340282B2
公开(公告)日：2016-05-17
申请号：US14216335
申请日：2014-03-17
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Timothy John Case , John Meeker
Abstract: A method and system for maintaining visual vertical reference on a rotorcraft display during rotorcraft landing is provided. The method generates vertical poles and positions them on the rotorcraft display such that vertical reference as well as roll information may be quickly and easily comprehended by a pilot.
Abstract translation: 提供了一种用于在旋翼飞机着陆期间在旋翼飞机显示器上维持视觉垂直参考的方法和系统。 该方法产生垂直极点并将其定位在旋翼航空器显示器上，使得垂直参考以及滚动信息可以被飞行员快速且容易地理解。
-
公开(公告)号：US10810888B2
公开(公告)日：2020-10-20
申请号：US16003328
申请日：2018-06-08
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Aaron James Gannon , Ivan Sandy Wyatt , John Meeker
Abstract: A system and method for providing automatic from-waypoint updating includes determining when a flight plan has been received that includes rendering a lateral map image that includes an aircraft icon and a flight leg to be captured. A variable position user input device supplies a signal representative of its position. A processor processes the signal from the variable position user input device and commands a display device to render a trajectory line graphic that (a) extends from the aircraft icon in a direction that corresponds to the position of the variable user input device and (b) intersects the at least one flight leg to be captured. The flight plan is automatically updated to designate the waypoint at the start of the at least one flight leg as a from-waypoint.
-
公开(公告)号：US20190378420A1
公开(公告)日：2019-12-12
申请号：US16003328
申请日：2018-06-08
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Aaron James Gannon , Ivan Sandy Wyatt , John Meeker
Abstract: A system and method for providing automatic from-waypoint updating includes determining when a flight plan has been received that includes rendering a lateral map image that includes an aircraft icon and a flight leg to be captured. A variable position user input device supplies a signal representative of its position. A processor processes the signal from the variable position user input device and commands a display device to render a trajectory line graphic that (a) extends from the aircraft icon in a direction that corresponds to the position of the variable user input device and (b) intersects the at least one flight leg to be captured. The flight plan is automatically updated to designate the waypoint at the start of the at least one flight leg as a from-waypoint.
-
6.发明申请公开(公告)号：US20170349295A1
公开(公告)日：2017-12-07
申请号：US15171417
申请日：2016-06-02
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dave Pepitone , John Meeker , Mark Giddings , Ivan Sandy Wyatt , John Suddreth , Aaron Gannon
CPC classification number: B64D43/00 , G01C23/005 , G06F3/04817 , G06F3/14 , G06T11/60 , G06T2210/36 , G06T2210/61 , G08G5/003 , G09G5/02 , G09G5/391 , G09G2320/10 , G09G2340/0407 , G09G2380/12
Abstract: A system method for providing aircraft lateral navigation system capability feedback to a pilot includes determining, in a processor, when a flight plan has been received that includes a flight leg that needs to be captured by the aircraft. A determination is made, in the processor, when an armed signal has been received, where the armed signal indicating that an aircraft autopilot navigation mode (NAV) has been armed. The processor is used to command a display device to render the flight leg using a first display paradigm when the armed signal has not been received, and to render the flight leg using a second display paradigm when the armed signal has been received.
-
-
-
-
-
Search Results
6
records
(took 0.01 seconds)
