-
1.发明申请公开(公告)号：US20210354808A1
公开(公告)日：2021-11-18
申请号：US17304150
申请日：2021-06-15
申请人： AeroData, Inc.
摘要： A system and method of displaying an Engine Failure Awareness Chart (EFAC) for aircraft with at least one engine out is shown and described herein. The EFAC may display lines and zones indicative of levels of risk of obstacles on the ground. The obstacles may be either man-made or natural structures. The EFAC may update continuously providing the pilot with a real-time awareness of the risks around the aircraft during an engine failure. Using the EFAC the pilot may navigate the aircraft to a landing area or back to the airport for landing.
-
2.发明授权Determining a profile for an aircraft prior to flight using a fuel vector and uncertainty bands 有权在飞行前使用燃料矢量和不确定带确定飞机的轮廓公开(公告)号：US09361486B2
公开(公告)日：2016-06-07
申请号：US14088682
申请日：2013-11-25
申请人： AeroData, Inc.
摘要： A weight and center-of-gravity profile for an aircraft is determined prior to flight. An uncertainty band is determined for each of a plurality of points along a fuel vector for the planned flight. Each of the points along the fuel vector is compared to a predetermined flight limit (e.g., an FAA certified envelope). This comparison is used to decide whether the profile is suitable for flight of the aircraft. If so, an indication is provided to a user (e.g., on a display or by a text message) that the profile is suitable and the aircraft is ready for flight.
摘要翻译： 在飞行前确定飞机的重量和重心剖面。 沿着用于计划飞行的燃料矢量的多个点中的每个点确定不确定性带。 将沿着燃料矢量的每个点与预定的飞行限制（例如，FAA认证的信封）进行比较。 该比较用于确定轮廓是否适合飞行器的飞行。 如果是这样，则向用户（例如，在显示器上或通过文本消息）提供该配置文件是合适的并且飞机准备好飞行的指示。
-
3.发明申请Determining a Profile for an Aircraft Prior to Flight Using a Fuel Vector and Uncertainty Bands 有权使用燃料矢量和不确定性带确定飞行前的飞机的轮廓公开(公告)号：US20150148992A1
公开(公告)日：2015-05-28
申请号：US14088682
申请日：2013-11-25
申请人： AeroData, Inc.
摘要： A weight and center-of-gravity profile for an aircraft is determined prior to flight. An uncertainty band is determined for each of a plurality of points along a fuel vector for the planned flight. Each of the points along the fuel vector is compared to a predetermined flight limit (e.g., an FAA certified envelope). This comparison is used to decide whether the profile is suitable for flight of the aircraft. If so, an indication is provided to a user (e.g., on a display or by a text message) that the profile is suitable and the aircraft is ready for flight.
摘要翻译： 在飞行前确定飞机的重量和重心剖面。 沿着用于计划飞行的燃料矢量的多个点中的每个点确定不确定性带。 将沿着燃料矢量的每个点与预定的飞行限制（例如，FAA认证的信封）进行比较。 该比较用于确定轮廓是否适合飞行器的飞行。 如果是这样，则向用户（例如，在显示器上或通过文本消息）提供该配置文件是合适的并且飞机准备好飞行的指示。
-
4.发明授权公开(公告)号：US11066181B2
公开(公告)日：2021-07-20
申请号：US16948854
申请日：2020-10-02
申请人： AeroData, Inc.
摘要： A system and method of displaying an Engine Failure Awareness Chart (EFAC) for aircraft with at least one engine out is shown and described herein. The EFAC may display lines and zones indicative of levels of risk of obstacles on the ground. The obstacles may be either man-made or natural structures. The EFAC may update continuously providing the pilot with a real-time awareness of the risks around the aircraft during an engine failure. Using the EFAC the pilot may navigate the aircraft to a landing area or back to the airport for landing.
-
公开(公告)号：US20210101674A1
公开(公告)日：2021-04-08
申请号：US16948853
申请日：2020-10-02
申请人： AeroData, Inc.
摘要： A system and method of planning and displaying takeoff brake release points, landing autobrake points, autobrake settings, and last touchdown points based on aircraft-specific performance is shown and described herein. Aircraft information and environmental information may be obtained from aircraft and airport systems. Takeoff brake release points may be determined based on thrust and economic savings for the aircraft and displayed to the pilot. Further, landing autobrake points, autobrake settings, and last touchdown points may be determined and displayed for the aircraft during landing.
-
6.发明授权公开(公告)号：US11851166B2
公开(公告)日：2023-12-26
申请号：US17304150
申请日：2021-06-15
申请人： AeroData, Inc.
CPC分类号： B64C25/426 , B60T8/1703 , B64D43/00 , B64D45/08
摘要： A system and method of displaying an Engine Failure Awareness Chart (EFAC) for aircraft with at least one engine out is shown and described herein. The EFAC may display lines and zones indicative of levels of risk of obstacles on the ground. The obstacles may be either man-made or natural structures. The EFAC may update continuously providing the pilot with a real-time awareness of the risks around the aircraft during an engine failure. Using the EFAC the pilot may navigate the aircraft to a landing area or back to the airport for landing.
-
7.发明申请公开(公告)号：US20210101695A1
公开(公告)日：2021-04-08
申请号：US16948854
申请日：2020-10-02
申请人： AeroData, Inc.
IPC分类号： B64D43/00
摘要： A system and method of displaying an Engine Failure Awareness Chart (EFAC) for aircraft with at least one engine out is shown and described herein. The EFAC may display lines and zones indicative of levels of risk of obstacles on the ground. The obstacles may be either man-made or natural structures. The EFAC may update continuously providing the pilot with a real-time awareness of the risks around the aircraft during an engine failure. Using the EFAC the pilot may navigate the aircraft to a landing area or back to the airport for landing.
-
-
-
-
-
-
搜索结果
7 条记录 (耗时 0.012 秒)
