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1. Instrument flight rules (IFR) training device

申请号: US859883

申请日: 1992-03-30

公开（公告）号: US5252069A

公开（公告）日: 1993-10-12

发明人: Richard A. Lamb; Jack J. Gilbert

An Instrument Flight Rules (IFR) Training Device for use during aircraft pilot training in conjunction with a headset having a pair of earphones supported by earphone stirrups. In its most preferred embodiment, the training device includes, at least, a mask member for partially occluding a pilot's vision, two arm members extending rearwardly from connections with opposing sides of the mask member, and headset connecting clamps for pivotally connecting the arm members to the headset stirrups, wherein the training device is supported by the headset and movable to a location up and away from a pilot's primary field of vision.

2. Universal aircraft panel with a dynamically symmetrical series of displays for the directional and rate flight instruments

申请号: US09428452

申请日: 1999-10-28

公开（公告）号: US06255964B1

公开（公告）日: 2001-07-03

发明人: Gordon H. Steele, Jr.

An integrated and dynamic symmetrical display of flight instruments for universal use in aircraft, wherein key instruments indicating with respect to aircraft direction are specifically arrayed with respect to key instruments indicating aircraft rate, wherein flight under instrument flight rules may be more easily learned, undertaken, and practiced with greater safety and ease of pilot workload, as compared with asymmetrical and random conventional flight instrument displays. Specifically, directional instruments are positioned in an aligned row above similarly arranged aircraft rate instruments for quick, reliable pilot scan and information utilization.

3. System and method for extending the life of aircraft anti-collision lights

申请号: US765955

申请日: 1991-09-26

公开（公告）号: US5206644A

公开（公告）日: 1993-04-27

发明人: Robert M. Dempsey

A system and method for extending the useful life of anti-collision lights comprising inert gas flash tubes and which are included on commercial, military, and business jet aircraft. When the aircraft is cruising in high altitude tightly controlled airspace (where instrument flight rules are controlling, i.e., at altitudes above 18,000 feet), and when the aircraft is not undergoing a substantial change in altitude, the power input to the anti-collision lights is reduced. The reduction in the power provides a significant increase in the useful life of the flash tube while causing only slight reduction in the intensity of the light output of the flash tube.

4. FLIGHT WATCH WITH MULTIPLE TIMERS AND ALARMS

申请号: PCT/US0020307

申请日: 2000-07-27

公开（公告）号: WO0209490A8

公开（公告）日: 2002-02-28

发明人: REISMAN JOHN

A timepiece to be worn by pilots of aircraft which provides a means to alert the pilot of multiple sequenced event occurrences, in a failsafe manner, via multiple alarm means including visual (29-32), auditory (36), and tactile (37) ability. The six in-flight timers (61-65), accessible through buttons (1-4), allow the pilot comprehensive user programmable features in order to meet the needs of a given flight. The watch also provides instant access to Zulu time and all forty two zones around the world. The watch is designed to assist the pilot in his awareness of engine time, countdown run time, fuel tank switching time, final approach fix to missed approach point time, countdown to instrument flight rule minimums, time to fix, timed turns, holding patterm timing, and time to close flight plan.

5. Pilot pad

申请号: US09829627

申请日: 2001-04-10

公开（公告）号: US20020145019A1

公开（公告）日: 2002-10-10

发明人: Christopher Ulibarri

A pad for allowing a user to write comfortably and legibly on a leg. The pad includes a plurality of sheets adapted to be written upon, each sheet having a plurality of spaced diagonal writing guide lines extending across a width thereof. A base section is provided with a clip connected thereto for selectively retaining the sheets on the base. A latching mechanism releasably secures the base section to a leg of a user allowing notes to be written between the lines on a top sheet while seated with an arm in a comfortable writing position. The plurality of lines on each sheet extend upward from a left side to a right side to accommodate a right hand person or extend downward from a left side of to a right side to accommodate a left handed person. The lines are preferably inclined at an angle of between substantially twenty five to substantially thirty five degrees. A heading is printed near a top edge of each sheet, the heading being a visual flight rules/instrument flight rules form. The base section further includes a base and a knee board connected to the base in an angularly adjustable manner, the clip selectively securing the sheets to the knee board.

6. Flight watch with multiple timers and alarm indicating means

申请号: US184928

申请日: 1998-11-02

公开（公告）号: US06144619A

公开（公告）日: 2000-11-07

发明人: John P. Reisman

An improved timepiece to be worn by pilots of aircraft which provides a means to alert the pilot of multiple sequenced event occurrences, in a failsafe manner, via multiple alarm means including visual (29-32), auditory (36), and tactile (37) ability. The six in-flight timers, accessible through buttons (1-4), allow the pilot comprehensive user progranmable features in order to meet the needs of a given flight. This watch solves previously unrecognized problems with regard to in-flight timing needs in general aviation. This watch is an electronic watch, specifically designed for pilots to address the plurality of in-flight timing needs, and includes a failsafe method by which to alert the wearer of time reliant in-flight, and post-flight, event occurrences. This watch also provides instant access to Zulu time and all forty-two time zones around the world. This watch is designed to assist the pilot in his awareness of engine run time, fuel tank switching time, final approach fix to missed approach point time, countdown to instrument flight rule and visual flight rule minimums, time to fix, timed turns, holding pattern timing, and time to close flight plan.

7. Chart instrument for displaying real time vehicle position relative to information on charts

申请号: US421972

申请日: 1989-10-16

公开（公告）号: US5089816A

公开（公告）日: 1992-02-18

发明人: Lawrence Holmes, Jr.

A lap top navigation instrument, suitable for aircraft, includes a chart compartment covered by a transparent window containing a liquid crystal display as part of the window through which a conventional map or chart in the compartment can be viewed and a computer whereby an image can be generated in the display above the chart in the compartment and, through inputs to the computer from the aircraft's instruments, the computer generated image in the display will be continuously repositioned above the surface of the chart so as pilot using the device has a continuous visual indication of the position of his aircraft over the topography depicted on the chart in the compartment. Directional components may be added to the image giving the pilot additional information in reference to the heading of the aircraft relative to the chart's display of "North" showing how the image is actually tracking over the chart in the compartment. Further, in this device, the chart in the compartment is always visible to the pilot though the window. Should the instrument fail a pilot continues to have access to all the flight information contained on the chart without interruption. As a result, the instrument is very useful for instrument flight rules [IFR] procedures and instrument approaches for landings in that it is failsafe.

8. 具有固定默认模式的飞行器约束系统

申请号: CN201811479471.X

申请日: 2018-12-05

公开（公告）号: CN109941441B

公开（公告）日: 2023-01-03

发明人: 埃里克·A·西努萨斯; 奥列弗·安德烈·布瓦韦尔; 纪尧姆·诺伊瑟-布歇; 史蒂夫·洛夫兰; 塞巴斯蒂安·杜瓦尔

一种用于飞行器的座位的乘员的模式约束系统，包括：带供给单元；以及能够选择性地收回到带供给单元中以及从带供给单元延伸的带。带能够邻近乘员定位以将乘员安置在带与座位之间。带供给单元适于在包括固定模式和非固定模式的多个模式之间切换。在固定模式下，带基本上不能从带供给单元延伸。在非固定模式下，带能够从带供给单元延伸并且能够收回到带供给单元中。带供给单元默认处于固定模式。带供给单元能够进行操作以响应于用户输入而切换至非固定模式，从而增加乘员相对于飞行器座位的移动的自由度。

9. 具有未固定默认模式的飞行器约束系统

申请号: CN201811465820.2

申请日: 2018-12-03

公开（公告）号: CN109941440A

公开（公告）日: 2019-06-28

发明人: 埃里克·A·西努萨斯; 奥列弗·安德烈·布瓦韦尔; 纪尧姆·诺伊瑟-布歇; 史蒂夫·洛夫兰; 塞巴斯蒂安·杜瓦尔

本发明涉及一种飞行器的用于座椅乘员的模式约束系统，该模式约束系统包括带条供给器单元和带条，带条能够选择性地收回到带条供给器单元中并且能够选择性地从带条供给器单元伸出。带条能够邻近乘员定位成将乘员至少部分地置于带条与座椅之间。带条供给器单元适于在包括未固定模式和固定模式的多个模式之间进行切换。带条在所述未固定模式中能够从带条供给器单元伸出并且能够收回到带条供给器单元中。带条在固定模式中基本上不能从带条供给器单元伸出。带条供给器单元默认处于未固定模式。带条供给器单元能够操作成响应于预防性事件而切换至固定模式，从而减小乘员相对于飞行器的座椅运动的自由度。

10. 具有固定默认模式的飞行器约束系统

申请号: CN201811479471.X

申请日: 2018-12-05

公开（公告）号: CN109941441A

公开（公告）日: 2019-06-28

发明人: 埃里克·A·西努萨斯; 奥列弗·安德烈·布瓦韦尔; 纪尧姆·诺伊瑟-布歇; 史蒂夫·洛夫兰; 塞巴斯蒂安·杜瓦尔

11. 模式约束系统以及飞行器

申请号: CN201811465820.2

申请日: 2018-12-03

公开（公告）号: CN109941440B

公开（公告）日: 2022-05-17

发明人: 埃里克·A·西努萨斯; 奥列弗·安德烈·布瓦韦尔; 纪尧姆·诺伊瑟-布歇; 史蒂夫·洛夫兰; 塞巴斯蒂安·杜瓦尔

12. 用于在飞行期间辅助飞行员的飞行器系统和方法

申请号: CN202010242821.1

申请日: 2020-03-31

公开（公告）号: CN111798704A

公开（公告）日: 2020-10-20

发明人: 奥利维耶·勒贝格; 伯诺伊特·奥莱特

用于在飞行期间辅助飞行员的飞行器系统和方法。本文公开了用于在飞行器飞行期间辅助飞行员的方法和系统。所述方法包括：接收指示所述飞行器在飞行期间的当前位置的数据以及指示飞行边界的数据；以及确定所述飞行边界与所述飞行器相关。所述方法还包括使显示装置相对于所述飞行器的当前位置显示表示所述飞行边界的表面。

13. 一种基于卫星导航的通用航空GNGP飞行程序保护区划设方法

申请号: CN202210667307.1

申请日: 2022-06-14

公开（公告）号: CN115047897A

公开（公告）日: 2022-09-13

发明人: 赵赶超; 雷晶晶; 向小军; 王亮; 闫东峰; 段铁城; 张林; 张小强

本发明公开了一种基于卫星导航的通用航空GNGP飞行程序保护区划设方法，解决了通用航空器在飞行过程中不能做到全空域仪表飞行的导航而导致通用航空器不能够很好的控制飞行和升降的问题，本发明包括步骤1)采集已有机场内外周围的数据；步骤2)通用航空器的GNGP软件检测驱动通用航空器运行能力；步骤3)将步骤1)和步骤2)融合，通用航空器的GNGP软件生成卫星导航的飞行‑离场保护区程序；步骤4)GNGP软件生成具有卫星导航飞行‑进近保护区程序；步骤5)最后GNGP软件生成使通用航空器飞行和着陆的保护区程序，本发明具有通用航空器GNGP软件程序生成以及导航的控制，使通用航空的升降以及飞行区域被限定，通用航空在升降和飞行过程中能够在设定的区域范围内运行的优点。