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JP2010185760A |
To provide a stall detector for reducing the influence of disturbance and improving the estimation accuracy of stall sign points.A sensor M for detecting vibration of fluid abutting against the outer wall surface of a mobile unit 1 is pr...
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JP4523346B2 |
The system (10) has a touch sensitive screen (11) that is transparent over a significant portion of its area. A set of projectors project images of vehicle controls on a back of the screen. The projectors are operatively connected to a c...
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JP4422907B2 |
Aircraft probe assemblies integrally include a total airstream temperature sensor. Preferred embodiments include at least one pressure sensing port and a temperature sensing port which are in fluid communication with a pressure sensing c...
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JP4377332B2 |
The altitude and speed control assist for a helicopter (2) has a sensor circuit (22) to deliver signals dependent on the altitude and speed values and a stored value memory (26) for predetermined altitude and speed levels. A circuit (20)...
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JP4361329B2 |
A system for providing independent and dissimilar aircraft parameter estimations includes first and second dual-channel electronic multi-function probes (MFPs) positionable adjacent an aircraft skin. Each dual-channel electronic MFP has ...
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JP4345014B2 |
Device for measuring the movement and or position of an aircraft (1) comprises imaging optics (2) with which a sequential images of the environment (4) is obtained. The images are analyzed using an optoelectronic displacement sensor (3),...
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JP4331105B2 |
Total air temperature sensor comprises a fluid intake (1) mounted on a contoured body and a conduit within the body that guides air towards a temperature sensitive element arranged within the conduit. The fluid intake has a surface that ...
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JP4302629B2 |
A flat panel display for presenting graphical renderings of aircraft flight, operation and system status data to an aircraft pilot renders the data at various predetermined brightness levels depending on the category of data assigned to ...
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JP4293905B2 |
A block arrangement of optical elements is provided for use as a transmitter/receiver for a light detection and ranging (LIDAR) system. The block arrangement comprises: a plurality of glass modules aligned together as a block to form a p...
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JP4246155B2 |
A method and apparatus is disclosed for displaying a dynamic parameter of an aircraft, the apparatus comprises a display unit receiving a display signal and displaying a scale that changes dynamically and non-linearly in accordance with ...
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JP2009500235A |
One embodiment of the present invention includes an aircraft instrumentation system for a cockpit instrument panel having a first device associated with a first pilot of an aircraft and positioned on the instrument panel substantially in...
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JP4191387B2 |
Improved multifunction probe having circumferentially spaced pairs of sensing parts (22,24). An elongate, conically shaped probe element is rotatable about an axis. A central pressure port (20) picks up dynamic pressure. A pair of inner ...
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JP2008528372A |
A power situation indicator configured to provide power information in a rotorcraft is presented. The power situation indicator includes a detection unit configured to detect a current value of each of a plurality of control parameters, ...
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JP2008134257A |
To provide block optical element constitution used as a transceiver for a light detection and ranging (LIDAR) system.This block optical element constitution is provided with a plurality of glass modules aligned each other as a block to f...
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JP2007230367A |
To provide a monitor displaying system for unmanned helicopter base station which increases the reliability for a flight control by sufficiently grasping the flight condition and performing a proper environmental situation judgement, and...
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JP2007230368A |
To provide a base station constitution for unmanned helicopter which can control various kinds of arbitrary payload instruments from the base station without rewriting the program or the like of an airframe flight control device of the b...
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JP3917523B2 |
The altimeters (28, 30) which contain within it means for storing the Static Source Error Correction (SSEC) includes means for downloading the SSEC and for transferring it to a new altimeter (32) which may then be used in the place of on...
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JP3916455B2 |
To stabilize video and sound communication by restricting an abnormality after isochronous transfer recovery caused by the discrepancy of bus resources which occurs when the bus is reset in a digital interface device for controlling the ...
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JP3860264B2 |
To reduce or solve conventional problems by use of air flow measurement value to a main sustaining rotor capable of directly relating to airspeed and relative wind direction. This method and device for detecting the airspeed of helicopte...
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JP2006282037A |
To provide an elevating speed altimeter capable of easily recognizing flight altitude, a elevating speed in a vertical direction and a direction of an airframe at a glance.The flight altitude, the elevating speed in the vertical directio...
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JP2006282034A |
To provide a horizontal speed heading indicator capable of easily visually recognizing heading, horizontal direction and speed of a flight vehicle at a glance.The heading, the horizontal direction and speed of the flight vehicle is simul...
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JP3821781B2 |
Sensor structure of a flow body protruding into a current for carrying out measurements of flow states, containing a structural part ( 1 ) with at least two measuring orifices ( 5 ), to which transfer lines ( 7 ) are coupled, which guide...
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JP3749135B2 |
To provide a temperature measuring device capable of properly measuring the temperature even in the case of use under an ice condition, and preventing ice and snow from easily adhering thereto, protecting the temperature measuring device...
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JP2005522700A |
A differential pressure-induced airflow based approach is used to measure Angle-Of-Attack (AOA) or Angle-Of-Sideslip (AOS) for an aircraft. Ports on opposing sides of an aircraft fuselage are coupled by an airway incorporating a mass air...
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JP3671216B2 |
To rapidly estimate an angle of elevation and an angle of sideslip with high accuracy even in case of the large angle of elevation in a system for detecting the angle of elevation and the angle of sideslip of an aircraft. The arrangement...
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JP3653047B2 |
A composite for use in the aircraft construction industry includes an optical transmission device, such as an optical fiber, embedded within a carrier. The optical transmission device is provided with a high-quality optical interface sur...
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JP3653046B2 |
A method of and an apparatus for coupling a first optical transmission means (10, 42), such as an optical fibre, embedded within an aircraft composite (12, 40) to a second optical transmission means (14), such as an optical fibre, extern...
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JP2005514258A |
An air data sensor for an aircraft has a flush mounted plate at the outside surface of the aircraft and a housing for the sensor within the aircraft below the plate. A plurality of holes in the plate provide air flow to a pressure sensor...
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JP2005502056A |
A wide field scanning laser obstacle awareness system (LOAS) for use on-board an aircraft is provided. The LOAS serves for alerting an operator of obstacles posing a risk of collision with said aircraft. The system comprising: a light so...
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JP3584325B2 |
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JP3574814B2 |
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JP3557444B2 |
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JP3522550B2 |
To provide a gyrocompas capable of automatic selection of correction mode suitable for operation condition of a ship by providing a means to automatically correct errors with a means to automatically select a correction mode suitable for...
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JP2004122857A |
To provide an airborne electronic apparatus casing expanding the cruising range of an aircraft.This airborne electronic apparatus casing is provided with a thermoelectric transducer 23 absorbing heat from an electronic apparatus 21 by be...
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JP2003344526A |
To provide a flying object measuring instrument that can measure a flying object with high reliability and can be manufactured at a low cost. This flying object measuring instrument 1 is provided with a plurality of antenna sections 2-1 ...
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JP3467836B2 |
PURPOSE: To obtain a navigating apparatus which can accurately detect an aircraft's own position. CONSTITUTION: An altitude calculator 7 periodically inputs the pilot's own aircraft's absolute position and terrain clearance obtained by a...
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JP3465944B2 |
PURPOSE: To precisely detect the failure of printing action by imparting markers to the unprinted portions of a web, detecting the presence of the markers on a web feed path, measuring the elapsed time of each marker between predetermine...
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JP2003294776A |
To provide a method of measuring moving speed and a device for measuring moving speed by imaging a target on the ground surface with an imaging sensor and measuring the moving speed of the target independent of the presence of a ground r...
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JP2003111075A |
To provide an obstacle detector capable of simply detecting presence of an obstacle around a mobile body with high accuracy.The obstacle detector comprises; a binary signal conversion section 22 for converting two image data A, B into bi...
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JP2002544499A |
The invention concerns a mass flow meter comprising at least a resistive wire (1 or 2) placed in the path of a fluid whereof the flow rate is to be measured, means (30) for applying to the wire current pulses, measuring means for determi...
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JP3354353B2 |
PURPOSE: To obtain a settlement computing method in which a settlement is performed with high accuracy and in a short time by a method wherein an attitude angle from an attitude indicator loaded on a moving body, an azimuth angle from an...
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JP2002280801A |
To provide an antenna system that is mounted on a mobile body such as an aircraft, makes microwave communication with a communication satellite or the like, mechanically contactlessly transmits a signal between a moving part and a statio...
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JP2002277245A |
To expand the mounting space of the gimbal carriage, compared with the conventional one, by mounting only an inertial detector of an inertial apparatus on an innermost rotary shaft of a gimbal mechanism of a space stabilizer and placing ...
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JP2002267489A |
To provide an altimeter and a speed indicator by which the correlation of a plurality of displayed values can be judged instantaneously and the work load of a pilot be also reduced.A symbol SA comprised of a long pointer and a short poin...
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JP2002055162A |
To prevent a collision accident in a small aircraft or helicopter, using a rotary type radar in which image display and voice display are included.Training or ordinary flight is carried out mainly at a height of about 1,500 feets where t...
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JP3238235B2 |
PURPOSE: To prevent agricultural chemicals from adhering to a light transmission member and at the same time reduce the number of maintenances of a sensor by providing a member forming a closed space which is located at the lower part wh...
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JP2001334999A |
To provide a warning generation system on the trend performance analysis.In this warning generation system (26) on the trend performance analysis, and this method therefor, a multivariate abnormal state detector (28) normalizes the data ...
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JP3232385B2 |
PURPOSE: To lessen errors in speed detection in the right and left directions, and concurrently let the detecting device hardly interfere with an obstacle by providing a speed detecting wave emitting section and a reflecting wave receivi...
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JP2001269417A |
To provide a safety device by which a pilot makes an airplane safely land under an emergent situation. This emergent flight safety device is used for a crew (3) of an airplane under an emergent situation, and includes a full-face mask (1...
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JP2001265476A |
To efficiently operate plural functions by a simple key operation without moving any view point.The menu of each function to be operated is obtained in a hierarchical structure, and the menu of each function is displayed at a menu displa...
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