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公开(公告)号：US10414515B2
公开(公告)日：2019-09-17
申请号：US15359987
申请日：2016-11-23
Applicant: Gulfstream Aerospace Corporation
Inventor： Charles Michaels , Michael Knight , Douglas Klutzke
Abstract: Aircraft, vision sensor systems, and methods of operating deployable vision systems are provided. An aircraft includes a fuselage and a vision sensor system. The fuselage defines an outer mold line and the vision sensor system includes a housing and a vision sensor package. The housing is selectively deployable between a retracted position and a deployed position and is disposed within the outer mold line in the retracted position and outside of the outer mold line in the deployed position. The vision sensor package is associated with the housing and is positioned to collect imaging information when the housing is in the deployed position.
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Patent Agency Ranking
公开(公告)号：US20160294882A1
公开(公告)日：2016-10-06
申请号：US14672639
申请日：2015-03-30
Applicant: Gulfstream, Aerospace Corporation
Inventor： Charles Michaels
CPC classification number: H04L65/1013 , H04L12/40 , H04L12/462 , H04L67/12 , H04L2012/4028
Abstract: An aircraft data network is provided that can include a first Remote Data Concentrator (RDC), a network switch and a second RDC. The first RDC can receive one or more input signals comprising data from a transmitting system, and translate the data per a network protocol to generate translated data having a format in accordance with the network protocol. The network switch can receive the translated data from the first RDC, determine a destination for at least some of the translated data, and route at least some of the translated data toward a first receiving system. The second RDC can receive at least some of the translated data from the network switch, convert at least some of the translated data to generate converted data having a format designed for use by the first receiving system, and communicate the converted data to the first receiving system.
Abstract translation: 提供了可以包括第一远程数据集中器（RDC），网络交换机和第二RDC的飞行器数据网络。 第一RDC可以接收包括来自发射系统的数据的一个或多个输入信号，并且根据网络协议翻译数据以生成具有根据网络协议的格式的转换的数据。 网络交换机可以接收来自第一RDC的翻译数据，确定至少一些翻译数据的目的地，并将至少一些翻译数据路由到第一接收系统。 第二RDC可以从网络交换机接收至少一些翻译的数据，将至少一些转换的数据转换成生成具有被设计为由第一接收系统使用的格式的转换数据，并将转换的数据传送到第一接收 系统。
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公开(公告)号：US20180141678A1
公开(公告)日：2018-05-24
申请号：US15359987
申请日：2016-11-23
Applicant: Gulfstream Aerospace Corporation
Inventor： Charles Michaels , Michael Knight , Douglas Klutzke
CPC classification number: B64D47/08 , B64C1/14 , B64C25/10 , B64D11/0689 , B64D43/00 , H04N5/2252 , H04N5/2253 , H04N5/23203 , H04N5/23293 , H04N7/183
Abstract: Aircraft, vision sensor systems, and methods of operating deployable vision systems are provided. An aircraft includes a fuselage and a vision sensor system. The fuselage defines an outer mold line and the vision sensor system includes a housing and a vision sensor package. The housing is selectively deployable between a retracted position and a deployed position and is disposed within the outer mold line in the retracted position and outside of the outer mold line in the deployed position. The vision sensor package is associated with the housing and is positioned to collect imaging information when the housing is in the deployed position.
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公开(公告)号：US09838436B2
公开(公告)日：2017-12-05
申请号：US14672639
申请日：2015-03-30
Applicant: Gulfstream Aerospace Corporation
Inventor： Charles Michaels
IPC: G06F15/173 , H04L29/06 , H04L12/40 , H04L12/46 , H04L29/08
CPC classification number: H04L65/1013 , H04L12/40 , H04L12/462 , H04L67/12 , H04L2012/4028
Abstract: An aircraft data network is provided that can include a first Remote Data Concentrator (RDC), a network switch and a second RDC. The first RDC can receive one or more input signals comprising data from a transmitting system, and translate the data per a network protocol to generate translated data having a format in accordance with the network protocol. The network switch can receive the translated data from the first RDC, determine a destination for at least some of the translated data, and route at least some of the translated data toward a first receiving system. The second RDC can receive at least some of the translated data from the network switch, convert at least some of the translated data to generate converted data having a format designed for use by the first receiving system, and communicate the converted data to the first receiving system.
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公开(公告)号：US20150353204A1
公开(公告)日：2015-12-10
申请号：US14173156
申请日：2014-02-05
Applicant: Gulfstream Aerospace Corporation
Inventor： Frank Manochio , Jason Meade , Charles Michaels
CPC classification number: B64D43/00 , G09G5/14 , G09G2300/026 , G09G2380/12
Abstract: A display system for use in a flight deck of an aircraft is disclosed herein. The flight deck has an instrument panel. The display system includes, but is not limited to, a display screen that is adapted for mounting to the instrument panel and that is configured to extend along substantially an entire lateral length of the instrument panel without any discontinuity of display capability. The display system includes, but is not limited to, a plurality of image sources associated with the display screen. The plurality of image sources is configured to cause a plurality of images to appear on the display screen.
Abstract translation: 本文公开了一种用于飞行器飞行甲板的显示系统。 驾驶舱有一个仪表板。 显示系统包括但不限于适于安装到仪表板的显示屏，其被配置为沿着仪表板的大致整个横向长度延伸，而没有显示能力的不连续性。 显示系统包括但不限于与显示屏相关联的多个图像源。 多个图像源被配置为使得多个图像出现在显示屏上。
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公开(公告)号：US20150015422A1
公开(公告)日：2015-01-15
申请号：US13941055
申请日：2013-07-12
Applicant: Gulfstream Aerospace Corporation
Inventor： Charles Michaels
IPC: B64D43/00
CPC classification number: B64D43/00
Abstract: A standby flight display system for use on an aircraft is disclosed herein. The aircraft has a primary flight display system that is configured to display a first image on a primary flight display screen. The standby flight display system includes a subsystem configured to determine a dynamic state of the aircraft. The standby flight display system further includes an image generator. The standby flight display system still further includes a processing unit. The subsystem, the image generator, and the processing unit are each independent of the primary flight display system. The processing unit is communicatively coupled with the subsystem and with the image generator and is configured to receive information from the subsystem relating to the dynamic state of the aircraft and to control the image generator to generate a second image overlaying the first image on the primary flight display screen.
Abstract translation: 本文公开了一种在飞行器上使用的备用飞行显示系统。 飞机具有主飞行显示系统，其被配置为在主飞行显示屏幕上显示第一图像。 备用飞行显示系统包括被配置为确定飞行器的动态状态的子系统。 待机飞行显示系统还包括图像发生器。 备用飞行显示系统还包括处理单元。 子系统，图像发生器和处理单元各自独立于主要飞行显示系统。 处理单元与子系统和图像发生器通信地耦合，并被配置为从子系统接收与飞行器的动态状态相关的信息，并且控制图像生成器以生成覆盖主飞行上的第一图像的第二图像 显示屏。
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