Deck landing system for aircrafts

Abstract

A deck landing system for aircrafts, in particular rotating wing aircrafts, apt to implement a hook between the aircraft and the deck of a ship or of a floating platform, the deck being equipped with a target grid plate, it does not require the use of hydraulic systems and it comprises: a telescopic actuator (1) with a harpoon (3) having, at its own distal end, hooking grippers (7); and a control unit (9) which actuates said telescopic actuator (1), wherein the telescopic actuator (1) comprises a linear electromechanical actuator (8) having: a main battery (13) fed through a unit (12) for converting and conditioning the energy and connected to said telescopic actuator (1); and a device (10) for recovering and releasing the kinetic energy generated by the waves with the aircraft locked on said deck, is of the type acting with super-capacitors, which feeds said main battery (13).

Claims

1. A deck landing system for aircrafts, adapted to implement a hook between the aircraft and a deck of a ship or of a floating platform, the deck being equipped with a target grid plate, which comprises: a telescopic actuator (1) with a harpoon (3) having, at a distal end thereof, hooking grippers (7); and a control unit (9) which actuates said telescopic actuator (1), wherein the telescopic actuator (1) comprises a linear electromechanical actuator (8) having: a main battery (13), fed through an energy conversion and conditioning unit (12), and connected to said telescopic actuator (1); and a supercapacitor device (10), which recovers and releases kinetic energy generated by waves with the aircraft locked on said deck, and which feeds said main battery (13).

2. The deck landing system according to claim 1, further comprising an electric motor supplied by an auxiliary battery (15) of the aircraft, providing power to the grippers (7) of the telescopic actuator (1) to unlock the grippers from a closed position thereof.

3. The deck landing system according to claim 2, wherein said electric motor is a brushless electric motor.

4. The deck landing system according to claim 1, wherein the control unit (9) comprises sensors (14) which include accelerometers.

5. The deck landing system according to claim 1, wherein a tracking system is provided capable of hooking the grid plate.

6. The deck landing system according to claim 5, wherein the tracking system is a laser-guiding type, which directs a laser beam to the center of the grid plate on the ship.

Description

(1) The present invention will be described hereinafter according to a preferred embodiment example thereof, provided by way of example and not for limitative purposes with reference to the enclosed drawings wherein:

(2) FIG. 1 shows a scheme illustrating a deck landing system according to the prior art;

(3) FIG. 2 shows a scheme illustrating a deck landing system according to the present invention;

(4) FIG. 3 shows a section of an electro-mechanical linear actuation device used in the deck landing system according to the present invention;

(5) FIG. 4 shows a functional scheme of the deck landing system according to the present invention; and

(6) FIG. 5 shows an additional scheme of an accessory system connected to the deck landing system according to the present invention.

(7) With reference to figures, the herein described deck landing system, intended to be assembled on a rotating wing aircraft, comprises an extension and retraction telescopic actuator 1 which drives a rod 2 of a harpoon 3 having, at the proximal end thereof, hooking grippers 7.

(8) The telescopic actuator 1 comprises a linear electromechanical actuator 8 which actuates said rod 2 and which is driven and controlled by an electronic control unit 9.

(9) The electro-mechanical actuator 8 is of the linear type and it can be adapted from the electric point of view with motor power adjustment and even from the point of view of the outer mechanical interface towards the helicopter, by modifying some geometrical parameters, so as to have a highly versatile equipment.

(10) FIG. 3 represents a section of a typical linear actuator suitable to the purpose, equipped. The electric motor therewith it is equipped is of three-phase brushless type.

(11) This actuator normally is actuated by the control electronic unit 9 providing for extending and checking the locking of the grippers 7, apart from the unlocking of the same and to the management of a device for recovering and releasing the kinetic energy 10 (KERS), preferably of the type acting with super-capacitors.

(12) The control electronic unit 9 then has the purpose of driving said brushless motor by means of a driver installed inside thereof which can be easily modified to adapt it to the different needs of helicopters thereon it should have to be installed, being able to act on the electric parameters of the control ring of the motor itself.

(13) The control electronic unit 9 is interfaced with the device for recovering and releasing the kinetic energy 10 according to the principle scheme shown in FIGS. 2 and 4.

(14) The device for recovering and releasing the kinetic energy 10, provided with super-condensers, accumulates and converts energy at high specific powers by providing it to the electro-mechanical actuator 8 for extending and retracting the deck landing system with the hooking grippers 7 connected to the grid plates of the ship, by guaranteeing that the helicopter is held to the deck under all conditions provided according to specification and of heavy sea in particular.

(15) The capability of the super-condensers of being able to be loaded or discharged almost instantaneously with respect to the chemical accumulators guarantees a very high specific power necessary in the function of adjusting the actuator stroke to the conditions of «ship motion» of the ship and to the respective consequences on the helicopter when locked on the ship dock.

(16) The device KERS (Kinetic Energy Recovery System) is used herein for recovering and returning the inertial energy deriving from the originated longitudinal motion of the boat generated by the wave motion (pitch) under the form of electric energy.

(17) It is meant however that the linear actuator 8 is also connected to the supply system of the aircraft, which can actuate it under normal conditions.

(18) Moreover, a battery 11 can be provided which can provide energy to a manual unlocking device 15, of electrical type too.

(19) According to the scheme of FIG. 4, the device for recovering and releasing the kinetic energy 10 feeds a main battery 13 through a unit 12 for converting and conditioning the energy, and the battery 13, in turn, is connected to the actuator of the deck landing system.

(20) The control unit 9 at last is equipped with sensors 14 which includes, for example, accelerometers.

(21) With reference to FIG. 5, an accessory system of the deck landing system is described hereinafter, allowing a manoeuvre of hooking a helicopter to the deck of a ship, or of a floating platform, equipped with suitable grid plates in compliance with standards of usual use in the field (STANAG 1276).

(22) Such manoeuvre often results to be very difficult due to the particularly heavy conditions of the sea and poor visibility or night hours. The pilot often is obliged to several manoeuvres for approaching the ship and the grid place in particular before being able to reach the right place therefrom it is possible to actuate the deck landing system and secure the helicopter on the ship.

(23) On this regard, the deck landing system comprises a tracking system capable of hooking the trajectory of the moving grid plate, expecting the motion thereof, guiding the helicopter and allowing the hooking of the helicopter itself to the grid plate in the easiest way through a system supporting the deck landing procedure under the conditions of poor visibility, night hours, and conditions of unfavourable sea based upon a tracking system of the grid plate which transforms the same in a precise “target-point” to be reached with the maximum precision.

(24) The tracking system is of the laser-guiding type and it directs the laser beam to the centre of the locking grid plate on the ship.

(25) When the helicopter is in proximity of the grid plate, at a sufficient distance to be able to receive the laser reflected energy, a laser sensor detects the direction and the distance of the moving points of the “target” and transmits the data to the system for processing the trajectory of the grid plate.

(26) The system for processing the trajectory is constituted by the sensors receiving the information from the laser and a software having the task of processing the received data, by detecting the current trajectory of the grid plate in real time, estimating with great precision, thanks to dedicated algorithms, the dynamics of the grid plate and by calculating the trajectory which the helicopter will have to follow to hook to the ship deck with precision and without risks.

(27) The electronic system for processing the trajectory then will provide the calculated data to the helicopter which could use them as input to an advanced navigation system supporting the automatic drive of the helicopter in the single manoeuvre of hooking to the grid plate of the ship even under unfavourable visibility and atmospheric conditions.

(28) More in details, the data received from the electronic system for processing the trajectory are transformed by the same to make them available to the helicopter which will use them by means of an advanced navigation system supporting the automatic guide of the same, in the manoeuvres of deck landing to the ship.

(29) The flight automatic system then has the task of guiding the helicopter through a defined path and to stabilize it, by controlling the asset and the speed even thanks to a GPS module which determines the reference orientation to pursue the wished path by performing the flight control manoeuvres of the helicopter by means of a Fly-By-Wire system to position it at the wished height, speed and position.

(30) To what described above a person skilled in the art, with the purpose of satisfying additional and contingent needs, could introduce additional modifications and variants, all however within the protective scope of the present invention, as defined by the enclosed claims.