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WO/2010/149753A1 |
The invention, which relates to an arrangement and a method for monitoring moving parts in a motor vehicle, is based on the object of providing an arrangement and a method with which the manufacturing costs, consumption of energy and env...
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WO/2010/119298A1 |
A method of manufacturing a rotor blade (10) comprising the steps of; applying at least one optical fibre strain sensor (14) to the leading edge of the rotor blade body; and fitting an erosion shield (16) to the leading edge of the rotor...
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WO/2010/116004A1 |
The invention relates to a device for characterising the nature of an aerodynamic flow along a wall (2), the device including a plurality of temperature-sensitive optical nodes (6) such as a distributed Bragg reflector distributed along ...
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WO/2010/084252A1 |
The invention relates to an aircraft cockpit that includes an information display device (10) with a screen (11) having a display surface (11a) and a rear surface (11b) opposite said display surface (11a), and a cable harness (12) connec...
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WO/2010/055338A1 |
A flow sensor and fastener assembly (101, 102, 103, 104), comprising at least the following modules: a sensor housing (4, 54, 74) and a fastener element(6, 62); wherein : the sensor housing (4, 54, 74) is adapted to receive a flow-based ...
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WO/2010/039279A1 |
In accordance with the teachings of the present disclosure, systems and methods for aligning blind-mate connectors are provided. In one embodiment, a system comprises an avionics processing canister (62) that is coupled to a mounting blo...
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WO/2010/039278A1 |
According to one embodiment, a bracket (100) configured to hold a pressure transducer (200) comprises a body (120), a face plate (170), and one or more pressure fitting connectors. The body has a rear portion (130) and a front portion (1...
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WO/2010/039281A1 |
According to one embodiment, a housing for a pedestal canister includes a first side plate and a fan. The first side plate includes a plurality of fins disposed on an exterior portion of the first side plate. The fan is coupled to the ex...
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WO/2010/039280A1 |
According to one embodiment, a pedestal canister includes a housing, one or more processing modules, and one or more aircraft interfaces. The housing is configured to be disposed within a pedestal aperture of a pedestal mounting block. T...
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WO/2010/036254A1 |
A method and module for displaying a munition release envelope.
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WO/2010/031179A1 |
A method for determining a hard-landing occurrence for an aircraft has sensors at selected positions of the aircraft. A model defining critical points throughout the aircraft is obtained. Data is received from the sensors when the aircra...
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WO/2010/004114A2 |
This aircraft control cabin comprises an avionics display device with multiple fixed screens (10a-10d) and at least one screen (15, 16) as an accessory, designed to be a replacement screen or extra screen for the avionics display system....
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WO/2009/106430A2 |
The invention relates to a device holder (2) for mounting devices (40) in a vehicle. Said device holder (2) comprises at least one external rack (4) and at least one internal rack (6). The at least one external rack (4) can be mounted on...
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WO/2009/102373A2 |
A system and method for conducting flight procedures training in a rotary-wing aircraft with a multi-engine powerplant includes determining a variable bias relative an available power margin to simulate a reduced power available flight c...
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WO/2005/086580A9 |
A method for providing on-demand audio information to a pilot of a first aircraft during aerial combat engagement with a hostile aircraft. The method includes receiving a pilot-initiated request for information, identifying the pilot-ini...
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WO/2009/050393A2 |
The invention relates to a crossed monitoring device for a head-up display (500-1) that can be used for displaying the representation of at least one first datum. The device includes means (505-1) for generating at least one image from s...
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WO/2009/047306A1 |
The invention relates to a flat screen device (L2) that comprises a multiple-path graphic generation (UGGL2) and a video data switch (50). The invention also relates to a method for managing a data network for improving the reliability o...
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WO/2009/044257A2 |
The system of the invention comprises: a first sensor (8) operating in a first spectral band and a second sensor (12) operating in a second complementary spectral band, respectively providing first and second signals corresponding to the...
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WO/2009/042309A2 |
A flight control system includes a fly by wire system operable to provide predictive termination point symbology overlaid on a synthetic imagery displayed by a display system in response to a control system and a sensor system. A method ...
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WO/2009/030856A2 |
The invention relates to a device for motorized aircraft comprising at least one avionic component (300) positioned in the said aircraft, at least one engine interface (310) positioned in the said aircraft and at least one engine control...
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WO/2009/010650A2 |
The invention relates to a method and device for determining a reliable position of an aircraft. The device (1) includes means (3, 10) for determining different aircraft position values and means (8, 16, 18) for deducing a reliable posit...
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WO/2009/007591A2 |
The invention relates to a method of managing an electrical power supply outage on board an aircraft, comprising the following operations: - detection of an electrical power supply outage, - measurement of a duration of the power supply ...
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WO/2008/145590A2 |
The general field of the invention is, in the context of ground collision prevention systems for aircraft, the presentation in the head-up display of a simplified symbology suited to these critical situations. It mainly comprises two ide...
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WO/2008/142240A2 |
The invention relates to an aircraft communication system including an aircraft terminal connected to at least one input/output unit. The invention is characterised in that the system includes a portable resource connected to the aircraf...
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WO/2008/122129A1 |
There is described a method and a system for providing a sighting reticle oriented to aim at a target from a vehicle within an environment of the target. The method improves the situational awareness of the operator regardless of the ori...
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WO/2008/119955A1 |
One aspect of the present invention relates to an aircraft cockpit display arrangement including a primary instrument display region (401) for positioning in front of at least one pilot, the primary instrument display region including a ...
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WO/2008/118633A2 |
A system (12) for measuring parameters at a plurality of loci associated with an aircraft includes: (a) a central unit (14); (b) a plurality of communicating nodes (16n) coupled with the central unit; and (c) a respective plurality of se...
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WO/2008/115273A2 |
A tandem inlet apparatus (10) for use with a high speed mobile platform, for example a commercial or military aircraft. The tandem inlet apparatus includes a Pitot inlet (102) for feeding air to a cabin air compressor (CAC) of an air con...
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WO/2008/101167A2 |
A system to monitor aircraft equipment, having a chassis, defining an interior compartment, an arrangement configured to accept input data of at least one aircraft parameter, the arrangement configured to be placed within an aircraft, cr...
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WO/2008/097319A2 |
The present invention is directed to a control system for use on a fly-by-wire (FBW) aircraft. The system includes a controller coupled to the FBW aircraft. The controller is configured to generate a plurality of simulated pilot control ...
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WO/2008/088575A1 |
An electronic display instrument configured to secure in a desired position over multiple pre-existing instrument holes in a dashboard of an aircraft in place of multiple conventional display instruments, each conventional instrument hav...
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WO/2008/064191A2 |
A visual display system includes a monitor for displaying a visual display; a memory having a user application definition file containing information related to the visual display; and a processor coupled to the monitor and the memory, t...
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WO/2008/042162A2 |
An augmented kinesthetic control system for use with a lift platform (100), the lift platform comprising first and second longitudinally-spaced thrust generating means (201/202), is provided. The first and second lift planes (701/703) de...
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WO/2008/034795A1 |
The present invention relates to a backup instrument fitted to the instrument panel of an aircraft to detect overload. The backup instrument comprises means for calculating and displaying flight information on the basis of data supplied ...
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WO/2008/036063A2 |
An avionics system having a pilot user interface, and method of interfacing with a pilot, includes providing a display screen and a video processor driving the display screen. A plurality of context dependent input devices is provided. O...
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WO/2008/025931A2 |
Device (100), particularly for positioning a moving vehicle (101) in a fluid, characterized in that it comprises: - a set of at least two probes (1), each one having a different measuring point, and each equipped with a sensor (3) of dif...
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WO/2007/149114A2 |
Military systems in particular face two specific problems: field casualties typically increase as unit visibility decreases and it is often difficult for ground stations and/or headquarters to maintain control and visibility of geographi...
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WO/2007/096501A1 |
Method and device for detecting a lateral dissymmetry of an aircraft. The detection device (1) comprises a means (7) for detecting a lateral dissymmetry, as a function of the current value of a control parameter which is representative o...
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WO/2007/074175A1 |
The invention concerns a method of and an apparatus for recording digital messages which are exchanged with data link devices between a pilot of an aircraft and staff on the ground, comprising an accident-protected speech recorder and a ...
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WO/2007/060167A1 |
The invention relates to a method for managing a convoy flight of at least two aeroplanes (1, 2), wherein a first aeroplane (1) is provided with means for transmitting the position, speed and the flight plan thereof, said flight plan com...
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WO/2007/030936A1 |
A system for maneuvering an aircraft for operations in connection with a sea-going vessel, the vessel having a designated area for landings and sling-load operations. Each of the aircraft has a navigation unit (INU) comprising a GPS rece...
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WO/2007/028675A1 |
The invention concerns a method for homogenizing measurement units used for displaying communication messages containing encrypted data, in particular messages exchanged by an aircraft with an air traffic control authority. The method in...
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WO2006093520A9 |
An air data system and method for a rotary aircraft is described. The air data system includes a plurality of flush ports (202) connected via tubing (304) to a plurality of air flow sensors (302) that can measure air flow speeds as low a...
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WO/2007/006310A2 |
Information allowing a pilot to safer and faster determine the status of an airplane, especially at take-off and landing. The information graphically illustrates to the pilot a relation between the length of a runway and a distance requi...
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WO/2006/130984A1 |
This invention allows for the precise determination of an aircraft's landing conditions and whether an aircraft has experienced a hard landing that exceeds the allowable design loads of the aircraft's landing gear. The system comprises a...
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WO/2006/117347A1 |
The invention relates to a combined instrument (10) for a helicopter (21), a method of determining the speed of a helicopter (21) and a method of adjusting a combined instrument (10) for a helicopter (21). Numerous helicopters are alread...
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WO/2006/106730A1 |
A fuselage information display panel (71) for a flying body, displaying vertically and horizontally arranged display sections (71a) provided by different information items. The display sections changes their colors depending on informati...
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WO/2006/104158A1 |
An unmanned helicopter has GPS devices (GPS receivers (37-39), GPS antennas (23-25)) for detecting the position of a fuselage (4), an autonomous control section (autonomous control box (17)) including a data communication unit (35) for c...
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WO/2006/101417A1 |
The invention relates to navigation equipment and the arrangement thereof in aircraft cockpits. The inventive aircraft cockpit comprises a first and second navigation situation displays, wherein said first display is cantilever fitted ab...
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WO/2006/098469A1 |
A flight control system has a flying body (1) and a ground station (40) that can communicate with each other. A fuselage of the flying body and a payload device are controlled from the ground station. The flying body (1) transmits data o...
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