公开(公告)号：US06832138B1

公开(公告)日：2004-12-14

申请号：US10086783

申请日：2002-02-28

申请人： Philip I. Straub ,  Dale R. Langner

发明人： Philip I. Straub ,  Dale R. Langner

IPC分类号： G05D100

CPC分类号： G05D1/0077

摘要： Systems and methods are provided for integrated control, access, and presentation of flight information within the cockpit. Cockpit instrument systems and methods are provided which include a first cockpit instrument panel which has a first display proximately located to a first bezel. The first display is operable to present navigational data, communication data, and flight information data including airspeed, attitude, and altitude. The systems and methods further include a second cockpit instrument panel located adjacent to the first cockpit instrument panel. The second cockpit instrument panel has a second display proximately located to a second bezel. The second display is operable to present navigational data, communication data, and flight information data including detailed engine parameters. When either the first or the second cockpit instrument panel fails, the remaining functional, first or second display, is adapted to provide all of the important flight information data, including airspeed, attitude, altitude, and detailed engine parameters.

摘要翻译： 提供系统和方法，用于在驾驶舱内集成控制，访问和显示飞行信息。 提供了驾驶舱仪器系统和方法，其包括第一驾驶舱仪表板，其具有靠近第一挡板的第一显示器。 第一显示器可操作地呈现导航数据，通信数据和包括空速，姿态和高度的飞行信息数据。 该系统和方法还包括位于第一驾驶舱仪表板附近的第二驾驶舱仪表板。 第二驾驶舱仪表板具有近似位于第二挡板的第二显示器。 第二显示器可操作以呈现导航数据，通信数据和包括详细引擎参数的飞行信息数据。 当第一或第二驾驶舱仪表板出现故障时，剩余的功能，第一或第二显示器适于提供所有重要的飞行信息数据，包括空速，姿态，高度和详细的发动机参数。

公开(公告)号：US06946976B1

公开(公告)日：2005-09-20

申请号：US10086598

申请日：2002-02-28

申请人： Dale R. Langner ,  Philip I. Straub

发明人： Dale R. Langner ,  Philip I. Straub

IPC分类号： G01C21/00 ,  G01C23/00

CPC分类号： G01C23/00

摘要： Systems and methods for cockpit display systems are provided. A cockpit display is segmented into a first and a second region, within the first region flight setting data are presented including communication settings and navigational settings. The second region of the display presents additional settings and graphical data. Moreover, the display is encompassed by a bezel having flight controls and flight sensors integrated in close proximity to the bezel.

摘要翻译： 提供了驾驶舱显示系统的系统和方法。 驾驶舱显示器被分割成第一和第二区域，在第一区域内呈现飞行设置数据，包括通信设置和导航设置。 显示器的第二个区域显示额外的设置和图形数据。 此外，显示器由具有飞行控制器和集成在挡板附近的飞行传感器的挡板所包围。

公开(公告)号：US06842122B1

公开(公告)日：2005-01-11

申请号：US10086996

申请日：2002-02-28

申请人： Dale R. Langner ,  Philip I. Straub

发明人： Dale R. Langner ,  Philip I. Straub

IPC分类号： G01C23/00 ,  G08B21/00

CPC分类号： G01C23/005

摘要： Systems and methods are provided for customized displays and customized presentations of cockpit data. Configurable soft keys or controls located in close proximity to a cockpit display are provided. Each key is configured to perform a desired display function or other function. Labels are displayed adjacent to each of the soft keys to identify each of the soft keys. A display is operable to provide multiple views, each view within the display is adapted to be overlaid with additional cockpit data if so configured. Furthermore, each view is capable of being presented from one or more selectable perspectives as desired.

摘要翻译： 提供系统和方法用于定制显示和驾驶舱数据的定制演示。 提供位于驾驶舱显示屏附近的可配置软键或控件。 每个键配置为执行所需的显示功能或其他功能。 标签与每个软键相邻显示，以标识每个软键。 显示器可操作以提供多个视图，如果配置的话，显示器内的每个视图适合于被附加的驾驶舱数据覆盖。 此外，每个视图能够根据需要从一个或多个可选择的视角呈现。

公开(公告)号：US07626515B1

公开(公告)日：2009-12-01

申请号：US10986336

申请日：2004-11-10

申请人： Dale R. Langner ,  Philip I. Straub

发明人： Dale R. Langner ,  Philip I. Straub

IPC分类号： G01C21/00

CPC分类号： G01C23/00

摘要： Systems and methods are provided for integrated control, access, and customizable presentation of navigation related, flight information data on a multifunction display (MFD) within a cockpit. The MFD includes a bezel having controls located thereon which are adapted for controlling display formats, communication devices, navigational devices, and equipment sensors. A display is located adjacent to the bezel. The display is adapted to include at least one display region having navigation related data. At least one of the controls is operable to variably select a display format for the at least one display region.

摘要翻译： 提供系统和方法，用于在驾驶舱内的多功能显示器（MFD）上集成控制，访问和可定制的与导航有关的飞行信息数据。 MFD包括其上具有控制器的挡板，其适于控制显示格式，通信设备，导航设备和设备传感器。 显示屏位于挡板旁边。 显示器适于包括具有导航相关数据的至少一个显示区域。 控制器中的至少一个可操作以可变地选择用于至少一个显示区域的显示格式。

公开(公告)号：US06842672B1

公开(公告)日：2005-01-11

申请号：US10785545

申请日：2004-02-24

申请人： Philip I. Straub ,  Dale R. Langner

发明人： Philip I. Straub ,  Dale R. Langner

IPC分类号： G05D1/00

CPC分类号： G05D1/0077

摘要： Systems and methods are provided for integrated control, access, and presentation of flight information within the cockpit. Cockpit instrument systems and methods are provided which include a first cockpit instrument panel which has a first display proximately located to a first bezel. The first display is operable to present navigational data, communication data, and flight information data including airspeed, attitude, and altitude. The systems and methods further include a second cockpit instrument panel located adjacent to the first cockpit instrument panel. The second cockpit instrument panel has a second display proximately located to a second bezel. The second display is operable to present navigational data, communication data, and flight information data including detailed engine parameters. When either the first or the second cockpit instrument panel fails, the remaining functional, first or second display, is adapted to provide all of the important flight information data, including airspeed, attitude, altitude, and detailed engine parameters.

摘要翻译： 提供系统和方法，用于在驾驶舱内集成控制，访问和显示飞行信息。 提供了驾驶舱仪器系统和方法，其包括第一驾驶舱仪表板，其具有靠近第一挡板的第一显示器。 第一显示器可操作地呈现导航数据，通信数据和包括空速，姿态和高度的飞行信息数据。 该系统和方法还包括位于第一驾驶舱仪表板附近的第二驾驶舱仪表板。 第二驾驶舱仪表板具有近似位于第二挡板的第二显示器。 第二显示器可操作以呈现导航数据，通信数据和包括详细引擎参数的飞行信息数据。 当第一或第二驾驶舱仪表板出现故障时，剩余的功能，第一或第二显示器适于提供所有重要的飞行信息数据，包括空速，姿态，高度和详细的发动机参数。

公开(公告)号：US06985801B1

公开(公告)日：2006-01-10

申请号：US10987274

申请日：2004-11-12

申请人： Philip I. Straub ,  Dale R. Langner

发明人： Philip I. Straub ,  Dale R. Langner

IPC分类号： G05D1/00

CPC分类号： G01C23/00

摘要： Systems and methods are provided for integrated control, access, and presentation of flight information within the cockpit. Cockpit instrument systems and methods are provided which include a first cockpit instrument panel which has a first display proximately located to a first bezel. The first display is operable to present navigational data, communication data, and flight information data including airspeed, attitude, and altitude. The systems and methods further include a second cockpit instrument panel located adjacent to the first cockpit instrument panel. The second cockpit instrument panel has a second display proximately located to a second bezel. The second display is operable to present navigational data, communication data, and flight information data including detailed engine parameters. When either the first or the second cockpit instrument panel fails, the remaining functional, first or second display, is adapted to provide all of the important flight information data, including airspeed, attitude, altitude, and detailed engine parameters.

摘要翻译： 提供系统和方法，用于在驾驶舱内集成控制，访问和显示飞行信息。 提供了驾驶舱仪器系统和方法，其包括第一驾驶舱仪表板，其具有靠近第一挡板的第一显示器。 第一显示器可操作地呈现导航数据，通信数据和包括空速，姿态和高度的飞行信息数据。 该系统和方法还包括位于第一驾驶舱仪表板附近的第二驾驶舱仪表板。 第二驾驶舱仪表板具有近似位于第二挡板的第二显示器。 第二显示器可操作以呈现导航数据，通信数据和包括详细引擎参数的飞行信息数据。 当第一或第二驾驶舱仪表板出现故障时，剩余的功能，第一或第二显示器适于提供所有重要的飞行信息数据，包括空速，姿态，高度和详细的发动机参数。

公开(公告)号：US06867711B1

公开(公告)日：2005-03-15

申请号：US10086573

申请日：2002-02-28

申请人： Dale R. Langner ,  Philip I. Straub

发明人： Dale R. Langner ,  Philip I. Straub

IPC分类号： G01C21/00 ,  G01C23/00

CPC分类号： G01C23/00

摘要： Systems and methods are provided for integrated control, access, and customizable presentation of navigation related, flight information data on a multifunction display (MFD) within a cockpit. The MFD includes a bezel having controls located thereon which are adapted for controlling display formats, communication devices, navigational devices, and equipment sensors. A display is located adjacent to the bezel. The display is adapted to include at least one display region having navigation related data. At least one of the controls is operable to variably select a display format for the at least one display region.

摘要翻译： 提供系统和方法，用于在驾驶舱内的多功能显示器（MFD）上集成控制，访问和可定制的与导航有关的飞行信息数据。 MFD包括其上具有控制器的挡板，其适于控制显示格式，通信设备，导航设备和设备传感器。 显示屏位于挡板旁边。 显示器适于包括具有导航相关数据的至少一个显示区域。 控制器中的至少一个可操作以可变地选择用于至少一个显示区域的显示格式。

公开(公告)号：US06696980B1

公开(公告)日：2004-02-24

申请号：US10086951

申请日：2002-02-28

申请人： Dale Langner ,  Philip I. Straub

发明人： Dale Langner ,  Philip I. Straub

IPC分类号： G01C2100

CPC分类号： G01C23/00

摘要： Systems and methods are provided for integrating cockpit controls and data associated with the controls into a single interface having a bezel surrounding a single display. Furthermore in one embodiment, a system includes two bezels having individual and duplicate controls affixed thereon, where each bezel surrounds a display operable to present data related to the controls. Moreover, the bezels are proximate to one another. Additionally in one embodiment, a system, having an audio control panel interposed between two bezels, is provided.

摘要翻译： 提供了系统和方法，用于将驾驶舱控制和与控制相关联的数据集成到具有围绕单个显示器的边框的单个接口中。 此外，在一个实施例中，系统包括两个边框，其上贴有单独和重复的控件，其中每个边框围绕可操作以显示与控件有关的数据的显示器。 此外，边框彼此靠近。 另外在一个实施例中，提供了一种具有介于两个边框之间的音频控制面板的系统。

公开(公告)号：US06859688B1

公开(公告)日：2005-02-22

申请号：US10274246

申请日：2002-10-18

申请人： Roger A. Orf ,  Philip I. Straub

发明人： Roger A. Orf ,  Philip I. Straub

IPC分类号： G01C25/00 ,  G05D1/00

CPC分类号： G01C25/00 ,  G06F9/44505

摘要： Data structures and systems are provided for configuring avionic equipment with profile data. Profile data is defined, stored, and/or retrieved. The profile data is used to configure one or more display fields of the avionic equipment, display units of measure, identify flight plans, define map settings, set navigation fields, define communication transceiver spacing, define data/time setup, to configure one or more timers, alarms, and/or to configure other communication, navigation, or surveillance settings associated with avionic equipment. Furthermore, instances of the profile data are associated with unique identifiers for storage and retrieval purposes.

摘要翻译： 提供了数据结构和系统，用于配置具有轮廓数据的航空电子设备。 配置文件数据被定义，存储和/或检索。 配置文件数据用于配置航空电子设备的一个或多个显示区域，显示测量单位，识别飞行计划，定义地图设置，设置导航区域，定义通信收发器间距，定义数据/时间设置，配置一个或多个 定时器，报警器和/或配置与航空电子设备相关联的其他通信，导航或监视设置。 此外，简档数据的实例与用于存储和检索目的的唯一标识符相关联。

公开(公告)号：US20090009363A1

公开(公告)日：2009-01-08

申请号：US12115365

申请日：2008-05-05

申请人： Roger A. Orf ,  Philip I. Straub

发明人： Roger A. Orf ,  Philip I. Straub

IPC分类号： G01C23/00 ,  G06F3/048 ,  G06F7/10 ,  G06F17/30

CPC分类号： G01C25/00 ,  G06F9/44505

摘要： Methods, data structures, and systems are provided for configuring avionic equipment with profile data. Profile data is defined, stored, and/or retrieved. The profile data is used to configure one or more display fields of the avionic equipment, display units of measure, identify flight plans, define map settings, set navigation fields, define communication transceiver spacing, define data/time setup, to configure one or more timers, alarms, and/or to configure other communication, navigation, or surveillance settings associated with avionic equipment. Furthermore, instances of the profile data are associated with unique identifiers for storage and retrieval purposes.

摘要翻译： 提供了方法，数据结构和系统，用于配置具有配置文件数据的航空电子设备。 配置文件数据被定义，存储和/或检索。 配置文件数据用于配置航空电子设备的一个或多个显示区域，显示测量单位，识别飞行计划，定义地图设置，设置导航区域，定义通信收发器间距，定义数据/时间设置，配置一个或多个 定时器，报警器和/或配置与航空电子设备相关联的其他通信，导航或监视设置。 此外，简档数据的实例与用于存储和检索目的的唯一标识符相关联。