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JPH01101292U |
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JPH0189300U |
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JPH01122799A |
PURPOSE: To reduce a load for an indicator by arranging an eyes direction detection sensor detecting the direction of the eyes of a pilot, displaying detailed information in an indicator on the eyes according to the detected result, and ...
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JPH01109197A |
PURPOSE: To make multipoint measurements of steering angle in the span direction of the rudder of the aileron, etc., of an aircraft by photographing the outside diameter of the rudder with a camera, and processing the taken images for me...
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JPS6460499A |
PURPOSE: To improve steering performance by providing an aircraft-shaped steering cue which moves vertically in accordance with required pitch change and rolls in accordance with a required bank angle in a device having a display surface...
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JPS6430446U |
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JPS63185800U |
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JPS63178891U |
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JPS63279999A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS63177395U |
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JPS63503093A |
An aircraft performance instrument which provides a first indicator which represents the line of level flight of the aircraft and a second indicator representative of the maximum permissible angle of attack of the aircraft.
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JPS63168200U |
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JPS63502933A |
An integrated head-up and panel display system for aircraft cockpits and the like. The system utilizes a wavelength-sensitive fold mirror (25) to separate the HUD image and the panel images. The system includes a monochromatic HUD image ...
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JPS6398300U |
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JPS6391567A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS6316713B2 |
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JPS634666B2 |
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JPS632798A |
A method for developing desired air data for use in flight control systems is disclosed including determining angle of attack and sideslip angle relative to inertial space and also determining said angles by solving appropriate aerodynam...
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JPS62285017A |
1. Arrangement in aircraft for generating triple redundant information for an assessment by majority decision for at least two horizontal axes in space with two strap-down gyroscope devices which are arranged to be rigidly fixed in space...
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JPS6218666U |
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JPS621880B2 |
In order to provide a more accurate representation of aircraft pitch attitude for use in aircraft head up display devices, a circuit for generating a computed pitch signal responds to a longitudinal accelerometer and a vertical gyroscope...
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JPS626899A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS61503024A |
A mounting and mounting method for a sensor positioned within a tubular axle of an aircraft undercarriage which will provide an output voltage proportional to the angular deflection of an axle for computation of aircraft gross weight. Th...
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JPS6156952B2 |
An improved variometer comprises a needle indicating on a graduation the instantaneous speed hx` of the aerodyne, and a speed representative of the potential speed h`u. The instantaneous vertical speed hx` is obtained by means of a circu...
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JPS61244698A |
In one form of the present invention, boundary layer air is diverted from a probe in an aircraft and freestream air is induced to impinge upon the probe.
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JPS61501944A |
An enclosure for an aircraft inertial unit (IRU) includes a dip-brazed chassis (10) having an inertial sensor assembly (ISA) compartment (40) and an electronics module compartment (36). The ISA compartment (40) is rigid with the ISA (42)...
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JPS61103300U |
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JPS61500841A |
A hot air leak sensor (12) for sensing jet engine bleed air leaks in an aircraft. Infrared detectors (10) are combined with thermal re-radiating elements (30) which are installed in air passages adjacent to the bleed air ducts (70) and d...
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JPS6058829B2 |
PCT No. PCT/FR79/00040 Sec. 371 Date Jan. 7, 1980 Sec. 102(e) Date Jan. 7, 1980 PCT Filed May 7, 1979 PCT Pub. No. WO79/01039 PCT Pub. Date Nov. 29, 1979.The invention concerns a process for the rapid detection of a wind gradient. This p...
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JPS6055018B2 |
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JPS60123721A |
PURPOSE: To improve the performance of a magnetic compass, by providing loop coils in the attaching frame of the magnetic compass, forming a constant magnetic field by the loop coils, thereby reducing errors. CONSTITUTION: In right and l...
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JPS6020559Y2 |
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JPS6020240B2 |
An airborne arrangement for displaying a moving map and aerial-navigation data such as symbols and characters on an electronic display screen is disclosed. It comprises a video map generator for converting the map to be displayed, carrie...
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JPS6015884B2 |
In a helicopter, torque display for a main rotor mast is mounted and connected to be driven from a power source at its base and connected to a main rotor at its tip. A reference member secured inside the main mast at the tip thereof depe...
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JPS603602B2 |
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JPS608193A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS5942244B2 |
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JPS59501706A |
Pressure tappings for rigid sails are described, the tappings (10-11-12-15-16) being located to either provide a stall warning or to enable tuning of the sailset to the desired operating angles. A particular flow-state sensitive stall wa...
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JPS59141014A |
This invention is a means for providing a pilot of an aircraft with a projective bar of light (42) which illustrates by its angle to the horizontal the bank angle of the aircraft, and by vertical position the pitch angle of the aircraft ...
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JPS59109798A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS5918397Y2 |
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JPS5921837B2 |
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JPS5978000A |
In order to provide timely aircraft performance data from an aircraft flight data recorder in a useful format, a flight data display system is provided: with a data storage unit; an interface circuit for reformatting flight data from the...
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JPS5934997A |
In order to provide timely aircraft performance data from an aircraft flight data recorder in a useful format, a flight data display system is provided: with a data storage unit (34); an interface circuit (12) for reformatting flight dat...
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JPS5918095A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS58190712A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS5863599A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS5863600A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS5830898A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS5758080Y2 |
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