21. 一种飞机电子飞行仪表系统模拟器

申请号: CN201921331633.5

申请日: 2019-08-16

公开（公告）号: CN210535046U

公开（公告）日: 2020-05-15

发明人: 钟宁伟

本实用新型涉及一种飞机电子飞行仪表系统模拟器，包括机箱，机箱的前端设置有电子飞行仪表系统控制面板，电子飞行仪表系统控制面板的下方设置有背光板，机箱内设置有电源模块和控制板，电源模块用于供电给控制板，控制板上设置有降压模块，降压模块用于将电源模块提供的电压进行降压，并供电给背光板和电子飞行仪表系统控制面板，控制板上还设置有微处理器，电子飞行仪表系统上设置有电门和显示屏，微处理器还与数据终端和飞机方式控制面板模拟器进行通信。本实用新型真实性强，结构简单紧凑，设计合理，成本较低，逼真度高，模拟效果显著，具有良好的体验效果。

22. 用于航空电子飞行仪表的自动检测仪

申请号: CN200720072269.6

申请日: 2007-07-06

公开（公告）号: CN201072597Y

公开（公告）日: 2008-06-11

发明人: 董选绳; 骆新平; 石丰年

本实用新型涉及一种用于航空电子飞行仪表的自动检测仪，包括工业控制计算机、信号模拟及控制装置、接口装置、供电装置、监测装置，所述的工业控制计算机与信号模拟及控制装置通讯连接，所述的信号模拟及控制装置、供电装置均与接口装置通讯连接，所述的监测装置与工业控制计算机、信号模拟及控制装置、接口装置通讯连接。与现有技术相比，本实用新型具有操作简单、工作性能稳定可靠、维护方便等优点。

23. 电子飞行仪表系统测试设备的装载机构

申请号: CN03241260.6

申请日: 2003-04-09

公开（公告）号: CN2611873Y

公开（公告）日: 2004-04-14

发明人: 邓福生

一种电子飞行仪表系统测试设备的装载机构，它包括底座、支座、移动工作台、工作台支架、传动轴、螺旋槽凸轮、活动框、碗形压块、控制杆、圆杆，在底座的前端立着支座，支座的上端连接位移座，底座上连接工作台支架，其特征是工作台支架中间连接传动轴，传动轴中间连接螺旋槽凸轮，前端用并帽固定，工作台支架上端连接圆杆，圆杆两端用档圈固定，移动工作台连在圆杆上，移动工作台上有个活动框，活动框下端有个凸轮，凸轮连接控制杆。本实用新型结构紧凑、性能稳定、维修方便、操作简单、定位准确，能确保所有接触点有良好接触，大大提高了电子飞行仪表系统在检测中的可靠性。

24. Flight instrument

申请号: US32536252

申请日: 1952-12-11

公开（公告）号: US2701473A

公开（公告）日: 1955-02-08

发明人: FIELDGATE IVAN O

25. Flight instrument

申请号: US601823

申请日: 1975-08-04

公开（公告）号: US4008618A

公开（公告）日: 1977-02-22

发明人: James R. Younkin

Aircraft altitude is visually displayed at a front panel of a flight instrument in analog form by a rotating pointer and in digital form by means of a rotary drum digital indicator. Barometric pressure is converted into rectilinear motion to drive a mechanical-to-electrical transducer providing a signal to a servo amplifier having an output coupled to a servomotor. The servomotor drives both the rotating pointer and the rotary drum digital indicator. Also coupled to the mechanical-to-electrical transducer is a manually adjustable set input signal to correct for atmospheric pressure along a given flight path with respect to sea level. Temperature and altitude error corrections are also coupled to the transducer to correct the servomotor drive signal to give a true indicated altitude display. Also driven by the servomotor is a pressure altitude encoder for providing absolute altitude digital signals for transmission to a ground station. As a further extension, the servomotor drives a velocity generator that functions integrally with an altitude selector to provide vertical velocity control signals to the aircraft autopilot system.

26. Flight instrument

申请号: US454305

申请日: 1974-03-25

公开（公告）号: US3940990A

公开（公告）日: 1976-03-02

发明人: James R. Younkin

Aircraft altitude is visually displayed at a front panel of a flight instrument in analog form by a rotating pointer and in digital form by means of a rotary drum digital indicator. Barometric pressure is converted into rectilinear motion to drive a mechanical-to-electrical transducer providing a signal to a servo amplifier having an output coupled to a servomotor. The servomotor drives both the rotating pointer and the rotary drum digital indicator. Also coupled to the mechanical-to-electrical transducer is a manually adjustable set input signal to correct for atmospheric pressure along a given flight path with respect to sea level. Temperature and altitude error corrections are also coupled to the transducer to correct the servomotor drive signal to give a true indicated altitude display. Also driven by the servomotor is a pressure altitude encoder for providing absolute altitude digital signals for transmission to a ground station. As a further extension, the servomotor drives a velocity generator that functions integrally with an altitude selector to provide vertical velocity control signals to the aircraft autopilot system.

27. Universal flight instrument

申请号: US32366240

申请日: 1940-03-13

公开（公告）号: US2300685A

公开（公告）日: 1942-11-03

发明人: WALTER MCKAY

28. Aerial flight instrument

申请号: US968935

申请日: 1935-03-06

公开（公告）号: US2280797A

公开（公告）日: 1942-04-28

发明人: CRANE CARL J

29. Combination flight instrument

申请号: US60510232

申请日: 1932-04-13

公开（公告）号: US2063764A

公开（公告）日: 1936-12-08

发明人: SMITH WESLEY L

30. Basic flight instrument

申请号: US816453

申请日: 1986-01-06

公开（公告）号: US4638660A

公开（公告）日: 1987-01-27

发明人: Richard D. Henry

A basic flight instrument to provide the pilot the means, by which, he can easily remain upright during instrument conditions. This flight instrument will be highly trustworthy, in that it will be absolutely tumble free due to its basic input derivatives. The instrument will be provided with two separate erection systems, whereby, the roll erection system will consist of a gimbal cage, spring tension erected and the pitch erection system will consist of a drum, the rotation of which will be properly erected by means of a gravitational weight and rotational reversing system. The pilot will be provided with simultaneous display of roll and pitch of reliable derivative. The roll rate of the gyro may be speed and altitude compensated if desired.

31. Aircraft flight instrument

申请号: US52853444

申请日: 1944-03-29

公开（公告）号: US2424511A

公开（公告）日: 1947-07-22

发明人: STANLEY ROBERT M; STRICKLER JR JOHN F

32. AIRCRAFT FLIGHT INSTRUMENT DISPLAYS

申请号: EP96910569.1

申请日: 1996-03-26

公开（公告）号: EP0817952B1

公开（公告）日: 2002-11-27

发明人: DURNFORD, Simon, J.; BRAITHWAITE, Malcolm, G.

An aircraft flight instrument display panel (10) has a combined speed and heading indicator in the form of a central square (11) surrounded by a scaled matrix (12). Displacement of an aircraft (100), in which the display is installed, from a desired speed and heading being indicated by displacement of an aircraft symbol (14) in the y and x directions from the central square. The aircraft (100) has an attitude sensor system (102) and the flight instrument display (108) has a flight instrument control system (104), the attitude sensor system and the flight instrument control system having an interconnection (106) with control laws such that, when the aircraft (100) is displaced from its desired speed and heading, pilot adjustment of pitch and roll, respectively, in a manner tending to return the aircraft (100) to the desired speed and heading, causes the aircraft symbol (14) to move towards the central symmetrical square (11). In a preferred embodiment, a linear slip meter (52) is included to indicate the necessary rudder input to maintain a coordinated turn. In a further embodiment, modes of operation (54) are indicated which, when selected, prompt the pilot to fly and climb or descend with standard rate turns.

33. AIRCRAFT FLIGHT INSTRUMENT DISPLAYS

申请号: EP96910569.0

申请日: 1996-03-26

公开（公告）号: EP0817952A1

公开（公告）日: 1998-01-14

发明人: DURNFORD, Simon, J.; BRAITHWAITE, Malcolm, G.

An aircraft flight instrument display panel (10) has a combined speed and heading indicator in the form of a central square (11) surrounded by a scaled matrix (12). Displacement of an aircraft (100), in which the display is installed, from a desired speed and heading being indicated by displacement of an aircraft symbol (14) in the y and x directions from the central square. The aircraft (100) has an attitude sensor system (102) and the flight instrument display (108) has a flight instrument control system (104), the attitude sensor system and the flight instrument control system having an interconnection (106) with control laws such that, when the aircraft (100) is displaced from its desired speed and heading, pilot adjustment of pitch and roll, respectively, in a manner tending to return the aircraft (100) to the desired speed and heading, causes the aircraft symbol (14) to move towards the central symmetrical square (11). In a preferred embodiment, a linear slip meter (52) is included to indicate the necessary rudder input to maintain a coordinated turn. In a further embodiment, modes of operation (54) are indicated which, when selected, prompt the pilot to fly and climb or descend with standard rate turns.

34. Flight instrument for aircraft

申请号: US60262645

申请日: 1945-06-30

公开（公告）号: US2569473A

公开（公告）日: 1951-10-02

发明人: HOOVER GEORGE W; EASTON ERVING E

35. Aerial flight instrument

申请号: US51624431

申请日: 1931-02-16

公开（公告）号: US1955488A

公开（公告）日: 1934-04-17

发明人: CRANE CARL J; OCKER WILLIAM C

36. 비행체를 이용한 원격 검침 시스템

申请号: KR1020140127565

申请日: 2014-09-24

公开（公告）号: KR101700634B1

公开（公告）日: 2017-01-31

发明人: 정용철; 신봉조; 조태원; 이재현

사용되는전기, 가스, 수도, 온도, 압력, 유량중 적어도하나이상의계량데이터를측정하는계량기가구비되고, 상기계량기로부터측정된계량데이터를저장하는제1저장부와, 외부로송, 수신하는제1단말장치; 복수개의설정된범위영역들중 선택된하나의특정영역의상공을비행하고, 제2단말장치가구비되는비행모듈; 상기제2단말장치는상기계량기에인접배치되는상기제1단말장치로부터계량데이터를수신하여, 저장하는제2저장부;를포함하며, 상기비행모듈을원격제어하거나또는상기제2단말장치로부터저장된계량데이터를제공받아과금을산출하는관재부를포함하는것을특징으로하는비행체를이용한원격검침시스템을제공한다.

37. 비행체를 이용한 원격 검침 시스템

申请号: KR1020140127565

申请日: 2014-09-24

公开（公告）号: KR1020160035797A

公开（公告）日: 2016-04-01

发明人: 정용철; 신봉조; 조태원; 이재현

사용되는전기, 가스, 수도, 온도, 압력, 유량중 적어도하나이상의계량데이터를측정하는계량기가구비되고, 상기계량기로부터측정된계량데이터를저장하는제1저장부와, 외부로송, 수신하는제1단말장치; 복수개의설정된범위영역들중 선택된하나의특정영역의상공을비행하고, 제2단말장치가구비되는비행모듈; 상기제2단말장치는상기계량기에인접배치되는상기제1단말장치로부터계량데이터를수신하여, 저장하는제2저장부;를포함하며, 상기비행모듈을원격제어하거나또는상기제2단말장치로부터저장된계량데이터를제공받아과금을산출하는관재부를포함하는것을특징으로하는비행체를이용한원격검침시스템을제공한다.

38. Electronic flight instrument displays

申请号: US10420602

申请日: 2003-04-22

公开（公告）号: US20030193411A1

公开（公告）日: 2003-10-16

发明人: Ricardo A. Price

The present invention is directed to novel primary flight displays, moving map displays and engine parameter displays for aircraft cockpits. These displays process data gathered from various aircraft sensors and, using an various electronic databases, generate intuitive symbols that aid the pilot. The present invention also uses various novel algorithms that use data gathered from inexpensive sensors to derive parameters normally requiring far more expensive sensors.