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公开(公告)号：US10267889B1
公开(公告)日：2019-04-23
申请号：US15814016
申请日：2017-11-15
申请人： Jurgen R. Ihns
发明人： Jurgen R. Ihns
摘要： A system for detecting a direction of a source of a laser beam includes a pixelated sensor that is sensitive to the laser beam. A mask is disposed between the source of a laser beam and the pixelated sensor. The mask includes an opaque portion that is opaque to the laser beam and a window portion that is at least translucent to the laser beam. When the laser impinges upon the mask an image of the window portion is projected onto the pixelated sensor. A processor determines an angle of incidence of the laser beam with respect to the mask by determining a number of pixels that the image of the window is offset from where the image of the window would be if the laser beam had been normal to the mask.
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公开(公告)号：US20160196752A1
公开(公告)日：2016-07-07
申请号：US15068810
申请日：2016-03-14
申请人： Jurgen R. Ihns
发明人： Jurgen R. Ihns
IPC分类号： G08G5/00 , G09G5/00 , G09G5/02 , G06F3/0489 , G06F3/0362 , B64D43/00 , G06F3/0488
CPC分类号： G08G5/0021 , B64D43/00 , G06F3/0362 , G06F3/04886 , G06F3/04892 , G08G5/0017 , G09G5/006 , G09G5/02 , G09G2370/02 , G09G2380/12 , H04L7/0083
摘要： A system for interfacing a user to a plurality of different avionics devices includes a plurality of communications links. Each link is coupled to a different one of the plurality of different avionics devices and adapted to communicate therewith according to a communications protocol associated with the one of the plurality of different avionics devices to which it is coupled. A front panel includes a display device and a plurality of user input components. A processor that is coupled to each of the plurality of communications links, the processor configured to display data from each of the different avionics devices on the display device so that the data from each of the different avionics devices is shown in a different graphical user interface on the display device and so that each graphical user interface conforms to a common display format, the processor further configured to receive user input for a selected one of the avionics devices through at least one of the plurality of user input components and to transmit the user input to the selected one of the avionics devices through one of the plurality of communication links that is coupled to the selected one of the avionics devices.
摘要翻译： 用于将用户连接到多个不同航空电子设备的系统包括多个通信链路。 每个链路被耦合到多个不同的航空电子设备中的不同的一个，并且适于根据与其所耦合的多个不同航空电子设备中的一个相关联的通信协议进行通信。 前面板包括显示装置和多个用户输入部件。 耦合到所述多个通信链路中的每一个的处理器，所述处理器被配置为在所述显示设备上显示来自所述不同航空电子设备中的每一个的数据，使得来自所述不同航空电子设备中的每一个的数据被显示在不同的图形用户界面 并且使得每个图形用户界面符合公共显示格式，所述处理器还被配置为通过所述多个用户输入组件中的至少一个接收所选择的一个所述航空电子设备的用户输入并且传送所述用户 通过耦合到所选择的一个航空电子设备的多个通信链路中的一个来输入到所选择的一个航空电子设备。
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公开(公告)号：US20210001996A1
公开(公告)日：2021-01-07
申请号：US16816736
申请日：2020-03-12
申请人： Jurgen R. Ihns
发明人： Jurgen R. Ihns
摘要： A cockpit pressurization and oxygen warning system includes a cabin pressure input and an aircraft pressure input. A pilot interface includes a first visual indicator having a first recognizable characteristic disposed in a first position that is made visually perceptible when a first signal is asserted and a second visual indicator having a second recognizable characteristic esthetically different from the first recognizable characteristic and disposed in a second position different from the first position that is made visually perceptible when a second signal is asserted. A control circuit that is responsive to the cabin pressure input and the aircraft pressure input determines an acceptable range for the cabin altitude that corresponds to the aircraft altitude. The control circuit asserts the first signal when the cabin altitude is within the acceptable range and asserts the second signal when the cabin altitude is not within the acceptable range.
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公开(公告)号：US10440293B1
公开(公告)日：2019-10-08
申请号：US16105271
申请日：2018-08-20
申请人： Jurgen R. Ihns
发明人： Jurgen R. Ihns
摘要： An aircraft imaging apparatus includes a thermal imaging camera, a control circuit, an image generating circuit and a display. The thermal imaging camera includes an array of pixels and that senses thermal radiation within the scene. The a control circuit is programmed to: detect an area of high thermal energy within the image; define a region of interest having a predetermined number of pixels within the area of high thermal energy; determine an average temperature sensed by the predetermined number of pixels; and adjust each of the plurality of adjustable parameters to optimal settings corresponding to the average temperature. The image generating circuit is operationally coupled to the thermal imaging camera and generates image data corresponding to a portion of the scene so that the image data is based on the optimal settings for the plurality of adjustable parameters. The display displays the image data.
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公开(公告)号：US09483949B2
公开(公告)日：2016-11-01
申请号：US15068810
申请日：2016-03-14
申请人： Jurgen R. Ihns
发明人： Jurgen R. Ihns
IPC分类号： G08G5/00 , B64D43/00 , H04L7/00 , G06F3/0362 , G06F3/0488 , G06F3/0489 , G09G5/00 , G09G5/02
CPC分类号： G08G5/0021 , B64D43/00 , G06F3/0362 , G06F3/04886 , G06F3/04892 , G08G5/0017 , G09G5/006 , G09G5/02 , G09G2370/02 , G09G2380/12 , H04L7/0083
摘要： A system for interfacing a user to a plurality of different avionics devices includes a plurality of communications links. Each link is coupled to a different one of the plurality of different avionics devices and adapted to communicate therewith according to a communications protocol associated with the one of the plurality of different avionics devices to which it is coupled. A front panel includes a display device and a plurality of user input components. A processor that is coupled to each of the plurality of communications links, the processor configured to display data from each of the different avionics devices on the display device so that the data from each of the different avionics devices is shown in a different graphical user interface on the display device and so that each graphical user interface conforms to a common display format, the processor further configured to receive user input for a selected one of the avionics devices through at least one of the plurality of user input components and to transmit the user input to the selected one of the avionics devices through one of the plurality of communication links that is coupled to the selected one of the avionics devices.
摘要翻译： 用于将用户连接到多个不同航空电子设备的系统包括多个通信链路。 每个链路被耦合到多个不同的航空电子设备中的不同的一个，并且适于根据与其所耦合的多个不同航空电子设备中的一个相关联的通信协议进行通信。 前面板包括显示装置和多个用户输入部件。 耦合到所述多个通信链路中的每一个的处理器，所述处理器被配置为在所述显示设备上显示来自所述不同航空电子设备中的每一个的数据，使得来自所述不同航空电子设备中的每一个的数据被显示在不同的图形用户界面 并且使得每个图形用户界面符合公共显示格式，所述处理器还被配置为通过所述多个用户输入组件中的至少一个接收所选择的一个所述航空电子设备的用户输入并且传送所述用户 通过耦合到所选择的一个航空电子设备的多个通信链路中的一个来输入到所选择的一个航空电子设备。
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公开(公告)号：US09293053B2
公开(公告)日：2016-03-22
申请号：US14198556
申请日：2014-03-05
申请人： Jurgen R. Ihns
发明人： Jurgen R. Ihns
CPC分类号： G08G5/0021 , B64D43/00 , G06F3/0362 , G06F3/04886 , G06F3/04892 , G08G5/0017 , G09G5/006 , G09G5/02 , G09G2370/02 , G09G2380/12 , H04L7/0083
摘要： The disclosure describes an aircraft avionics management and control system, including apparatuses and methods, for consolidating aircraft avionics management and control operations and for allowing universal management, control, and operation of a plurality of communications systems, navigation systems, transponder systems, and other avionics systems with a single device. The communication systems may comprise a plurality of military radios, civilian radios, or other communication systems of different types and may have different manufacturers. Similarly, the navigation systems and transponder systems may comprise navigation systems and transponder systems of different types and may have different manufacturers. The communication systems, navigation systems, transponder systems, and other avionics systems may be communicatively connected to the aircraft avionics management and control system via different types of communication links having different communications protocols and/or different standards.
摘要翻译： 本公开描述了一种用于整合航空电子设备管理和控制操作并允许多个通信系统，导航系统，应答器系统和其他航空电子设备的通用管理，控制和操作的飞行器航空电子管理和控制系统，包括装置和方法 具有单个设备的系统。 通信系统可以包括多个军事无线电，民用无线电或其他不同类型的通信系统，并且可以具有不同的制造商。 类似地，导航系统和应答器系统可以包括不同类型的导航系统和应答器系统，并且可以具有不同的制造商。 通信系统，导航系统，应答器系统和其他航空电子系统可以经由具有不同通信协议和/或不同标准的不同类型的通信链路与飞行器航空电子管理和控制系统通信地连接。
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公开(公告)号：USD989719S1
公开(公告)日：2023-06-20
申请号：US29809120
申请日：2021-09-25
申请人： Jurgen R. Ihns
设计人： Jurgen R. Ihns
摘要： FIG. 1 is a top isometric view of a portion of a toggle switch guard showing my new design.
FIG. 2 is a left side elevational view thereof.
FIG. 3 is a right side elevational view thereof.
FIG. 4 is a top plan view thereof.
FIG. 5 is a bottom plan view thereof.
FIG. 6 is a font elevational view thereof.
FIG. 7 is a back elevational view thereof; and,
FIG. 8 is an isometric view thereof with a section cut away taken along line 8-8 in FIG. 6.
The broken lines in the drawings depict environmental structure associated with the toggle switch guard that form no part of the claimed design.-
公开(公告)号：US11377227B2
公开(公告)日：2022-07-05
申请号：US16816736
申请日：2020-03-12
申请人： Jurgen R. Ihns
发明人： Jurgen R. Ihns
摘要： A cockpit pressurization and oxygen warning system includes a cabin pressure input and an aircraft pressure input. A pilot interface includes a first visual indicator having a first recognizable characteristic disposed in a first position that is made visually perceptible when a first signal is asserted and a second visual indicator having a second recognizable characteristic esthetically different from the first recognizable characteristic and disposed in a second position different from the first position that is made visually perceptible when a second signal is asserted. A control circuit that is responsive to the cabin pressure input and the aircraft pressure input determines an acceptable range for the cabin altitude that corresponds to the aircraft altitude. The control circuit asserts the first signal when the cabin altitude is within the acceptable range and asserts the second signal when the cabin altitude is not within the acceptable range.
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公开(公告)号：USD945974S1
公开(公告)日：2022-03-15
申请号：US29749223
申请日：2020-09-03
申请人： Jurgen R. Ihns
设计人： Jurgen R. Ihns
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公开(公告)号：US20190308743A1
公开(公告)日：2019-10-10
申请号：US16006178
申请日：2018-06-12
申请人： Jurgen R. Ihns
发明人： Jurgen R. Ihns
摘要： A cockpit pressurization and oxygen warning system includes a cabin pressure input and an aircraft pressure input. A pilot interface includes a first visual indicator having a first recognizable characteristic disposed in a first position that is made visually perceptible when a first signal is asserted and a second visual indicator having a second recognizable characteristic esthetically different from the first recognizable characteristic and disposed in a second position different from the first position that is made visually perceptible when a second signal is asserted. A control circuit that is responsive to the cabin pressure input and the aircraft pressure input determines an acceptable range for the cabin altitude that corresponds to the aircraft altitude. The control circuit asserts the first signal when the cabin altitude is within the acceptable range and asserts the second signal when the cabin altitude is not within the acceptable range.
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