Warning device for helicopters

Claim 2

A warning device, for a helicopter with a tail rotor and a tail rotor mechanical protection device, which device produces a warning signal when the tail is in such a position as to be in danger of making contact with an obstruction or the ground and comprises a height-measuring device with transmitting and receiving means for a high frequency electromagnetic wave beam used in the height measurement, the transmitting and receiving means being positioned at the tail of the helicopter such that the electromagnetic wave beam is directed backwards and obliquely downwards, and computing means for determining from the height measurements of the height measuring device, the speed of approach to the ground or obstruction in the path of the beam and for initiating a warning signal if the speed of approach relative to the instantaneous height corresponds to a predetermined value.

Claim 3

A warning device according to claim 1 wherein the direction of said electromagnetic wave beam is substantially along or adjacent and parallel to the axis of a tail rotor mechanical protection device.

Claim 4

A warning device according to claim 1 wherein the transmitting and receiving means are mounted on a tail rotor support device.

Claim 5

A warning device according to claim 2 wherein the transmitting and receiving means are mounted on a tail rotor support device.

Claim 6

A warning device, for a helicopeter with a tail rotor, said device producing a warning signal when the tail is in such a position as to be in danger of making contact with an obstruction or the ground, said device comprising a height-measuring means with transmitting and receiving means for a high frequency electromagnetic wave beam used in the height measurement, the transmitting and receiving means being positioned at the tail of the helicopter such that the electromagnetic wave beam is directed backwardly and obliquely downwardly, computing means responsive to said height measurement means for determining the speed of approach to the ground or obstruction in the path of the beam and for initiating a warning signal if the speed of approach relative to the instantaneous height corresponds to a predetermined value, wherein the computing means and height measuring means are contained in a housing together with an aircraft frequency radio tarnsmitter means and an independent power supply for the measuring means, the computing means and the radio transmitter means, and releasable mounting means on the housing to enable its releasable mounting onto a helicopter, and means for passing said warning signals indicated by the computing means to and transmitting them by the radio transmitter means to be received over the standard helicopter radio receiver.

Claim 7

A warning device, for a helicopeter with a tail rotor, said device producing a warning signal when the tail is in such a position as to be in danger of making contact with an obstruction or the ground, said device comprising a height-measuring means with transmitting and receiving means for a high frequency electromagnetic wave beam used in the height measurement, the transmitting and receiving means being positioned at the tail of the helicopter such that the electromagnetic wave beam is directed backwardly and obliquely downwardly, computing means responsive to said height measurement means for determining the speed of approach to the ground or obstruction in the path of the beam and for initiating a warning signal if the speed of approach relative to the instantaneous height corresponds to a predetermined value, wherein the computing means and height measuring means are contained in a housing together with an aircraft frequency radio tarnsmitter means and an independent power supply for the measuring means, the computing means and the radio transmitter means, and releasable mounting means on the housing to enable its releasable mounting onto a helicopter, and means for passing said warning signals indicated by the computing means to and transmitting them by the radio transmitter means to be received over the standard helicopter radio receiver.

Claim 8

The warning device according to claim 5 wherein the direction of said electromagnetic wave beam is substantially along or adjacent and parallel to the axis of a tail rotor mechanical protection device.

Claim 9

The warning device according to claim 5 wherein the height measuring transmitting and receiving means are mounted on a tail rotor support.

Claim 10

A warning device for a helicopter with at least a tail rotor, said device producing a warning signal during at least a flare in an auto-rotation landing when the tail rotor is in a position which is in danger of making contact with an obstruction, the warning being given in time for the pilot to level the helicopter before such contact, the warning device comprising a height measuring means having transmitting and receiving means mounted on the tail rotor support for a transmitting and receiving energy wave beam used in the height measurement, the transmitting and receiving means being positioned at the tail of the helicopter such that the wave beam is directed backwardly and obliquely downwardly, computing means responsive to height measurement means for detecting the speed of approach to the ground or obstruction in the path of the beam and for initiating a warning signal if the speed of approach relative to the instantaneous height corresponds to a predetermined value.

Claim 11

A warning device for a helicopter with at least a tail rotor, said device producing a warning signal during at least a flare in an auto-rotation landing when the tail rotor is in a position which is in danger of making contact with an obstruction, the warning being given in time for the pilot to level the helicopter before such contact, the warning device comprising a height measuring means having transmitting and receiving means mounted on the tail rotor support for a transmitting and receiving energy wave beam used in the height measurement, the transmitting and receiving means being positioned at the tail of the helicopter such that the wave beam is directed backwardly and obliquely downwardly, computing means responsive to height measurement means for detecting the speed of approach to the ground or obstruction in the path of the beam and for initiating a warning signal if the speed of approach relative to the instantaneous height corresponds to a predetermined value.