Sextant Avionique

Roger Parus

Philippe Coirier

Xavier Denoize

Francedillaois Faivre

Alain Goujon

Francois Faivre

Bruno Aymeric

Catherine Boiteau

Vehicle course steering aid device

Device for assisting with the extinguishing of fires by water-bombing

This device relates to assistance in the piloting of an aircraft or helicopter in conditions of poor visibility, at the landing stage, during the final approach before touchdown. In case of poor visibility, the landing operations are facilitated by ILS radioelectrical installations that enable an automatic approach to the runway threshold. All that remains to be done is to perform a flare-out for touchdown which has to be done in a certain zone at the start of the runway. It happens, in the event of poor visibility, that this touchdown zone is difficult to assess. This causes risks of overshooting. The disclosed device is aimed at putting out an alarm in the event of overshooting of the nominal touchdown zone. It has means for the integration of the ground speed, means to detect the crossing of a lower value of a threshold of height with respect to the ground activating said integration means and means to detect a crossing of an upper value of a distance threshold acting on the signal delivered by the integration means and generating an alarm when there is no detection, by the load sensor, of an alighting of wheels.

Device for assistance in the piloting of an aircraft at the landing stage

A device for the substitution of an artificial image shown to an aircraft pilot by the corresponding real image includes a device for the simulation of human vision; criteria for the exploitation of the simulated image; compare to a device for comparing to compare the simulated image with the criteria of exploitation; a device for attenuating the artificial image, the artificial image being attenuated when the simulated image meets a given number of exploitation criteria.

Device for substituting an artificial image shown to an aircraft pilot

This optoelectronic device is designed to provide assistance in the piloting of an aircraft under conditions of poor visibility, at the final approach stage, during taxiing and at take-off from a runway equipped with an ILS. The device consists of a collimator displaying a reticule symbolizing a runway centerline that is shown to the pilot during flight as well as on the ground, without any break between the in-flight final approach stage and the ground stage of taxiing on the runway. The device takes account of the pilot's off-centered position in the aircraft cockpit.

Device for assistance in the piloting of an aircraft

A device to improve the field of vision in aircraft that lack sufficient transparent surface area. The device includes at least one collimator connected to an imaging sensor of the space outside the aircraft. The collimator projects an image in the pilot's field of vision. The image covers both the transparent window surface and the instrument panel of the cockpit. The image coincides with the real image in the field of direct vision produced by the transparent surface. A further image may also be viewed by the pilot through a periscope arrangement.

Device for improving the field of vision of aircraft that do not have a

The disclosure relates to systems for piloting aircraft. Equations of the movements of the aircraft are used for computing, in a computer, of the first and second derivatives parameters V.sub.p, .PHI..sub.v, .sigma..sub.a, .beta..sub.v, .alpha., .PHI..sub.v, .sigma..sub.a, .beta..sub.v, of the parameters V.sub.p, .PHI..sub.v, .sigma..sub.a, .beta..sub.v, .alpha. of the movement of the aircraft, and the values thus computed are compared with those computed by means of the values of said parameters V.sub.p, .PHI..sub.v, .sigma..sub.a, .beta..sub.v, .alpha. at the instants t, (t+dt) and (t+2dt). An alarm signal (circuit 23) is generated if equality is not verified to a given precision.

Growing community of inventors

Merignac, France

Roger Parus