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Device and method for monitoring the obstructions in the close environment of an aircraft

a technology for aircraft and close environment, applied in the field of aircraft navigation aids, can solve the problems of not being able to detect mobile obstacles such as terrestrial vehicles or other aircraft, reducing sensitivity so much, and reducing the surprise effect, so as to reduce the stress of the crew and reduce the surprise effect.

Active Publication Date: 2012-08-23
THALES SA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The invention is a device that helps improve safety for helicopters operating in close proximity to fixed or mobile obstacles. It detects and identifies potential hazards in real-time, and alerts the pilot with a combination of visual and auditory signals. This allows the pilot to react to the situation and take appropriate action to prevent accidents. The device can detect both terrain and human constructions, and calculates the criticality of each obstacle based on its size, speed of displacement, and distance from the helicopter. Overall, the invention helps reduce stress on the pilot and increases safety during flights.

Problems solved by technology

Cases of collision between the craft and an arbitrary obstruction usually occur during the takeoff or landing phases—phases during which the TAWS alert functions are disabled, or in the best of cases, with a sensitivity that is reduced so much that the alert will be delivered too late to save the craft and more particularly the anti-torque device situated on the tail of the helicopter.
Systems of TAWS type, through their use of a digital terrain model, are not capable of detecting mobile obstacles, such as terrestrial vehicles or other aircraft.
It does not make it possible to calculate or to picture the discrepancy with respect to this threshold.
The systems of “HELLAS” type are complex and expensive.
These systems do not generally make it possible to protect the lateral parts and the tailplane of the craft.
The systems of flight control type are also complex and expensive and rely on the possibility offered to them of acting on the control surfaces of the craft.
Not all helicopters may be so equipped.
Moreover these systems, through their corrective action, do not allow the crew to anticipate the situation.
They likewise do not make it possible to protect the lateral parts or the front of the craft and they offer reliable protection only in relation to the ground or obstacles situated under the craft.
They do not protect the craft in relation to mobile obstacles.

Method used

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  • Device and method for monitoring the obstructions in the close environment of an aircraft
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  • Device and method for monitoring the obstructions in the close environment of an aircraft

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Embodiment Construction

[0021]The aim of the present invention is to make the systems cited hereinbelow collaborate, so as to present to the crew the obstacles and the terrain zones that are potentially dangerous for the craft in general. The monitoring device is arranged in such a way that it recovers the data originating from an active system for detecting obstacles and the relief based on short-range radar technology, of WTAS type for example, the data of a system of TAWS type making it possible to raise ad-hoc alerts should the craft approach dangerously near to a relief zone and / or obstacles, and that it transmits, to a display device in the cockpit, the information formulated by the system so as to present the said information to the crew.

[0022]The invention also relates to the method for monitoring obstructions for an aircraft, characterized in that detection means measure parameters for locating and identifying obstacles in the close environment of the aircraft, in that identification means calcula...

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Abstract

The invention relates to a device for monitoring obstructions for an aircraft including data storage, an anticollision device and viewing devices, wherein the monitoring device comprises a detector to detect in real-time obstructions, of terrain type and of human constructions type, in a close environment of the aircraft in a flight situation, a sensor to identify the obstructions at risk calculating identification parameters, a circuit to calculate criticality of the obstructions, a display to display both the obstructions with the identification and criticality parameters of the obstructions, and a generator of alerts to describe the situation according to a combination of the identification and criticality parameters. One or more embodiments of the invention is a monitoring system adapted for zones close to the aircraft and in the flight zones not visible to the crew. One or more embodiments of the invention applies particularly to helicopters executing low-altitude flights. It relates more particularly to military carriers such as rescue carriers.

Description

CROSS-REFERENCE TO RELATED APPLICATION[0001]The present application claims the benefit of French Patent application No. 08 / 03215, filed Jun. 10, 2008, which is hereby incorporated by reference in its entirety.FIELD OF THE INVENTION[0002]The invention relates to the field of aerial navigation aids for the prevention of accidents in which an aircraft which is still manoeuvrable collides with an obstacle. Hereinafter, the term “obstacle” designates any non-natural obstruction present in the environment of the aircraft, and one then speaks notably of human constructions such as buildings or bridges. Moreover, the term “relief” or “terrain” designates obstructions relating to the natural environment such as mountainous zones and more generally the ground.[0003]Through the type of missions carried out, landing and takeoff in zones that are difficult to access, sometimes unprepared, or low-altitude flight, the helicopter, for example, is a craft that is very highly exposed to the risk of c...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): G08G5/04G01S13/935
CPCG01S7/22G01S7/24G01S13/94G01S13/87G01S7/41G01S13/935
Inventor FLOTTE, LAURENTMARTY, NICOLASGAYRAUD, PASCAL
Owner THALES SA
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