Emergency anti-torque control system and method for helicopters

Claim 2

An emergency anti-torque control system for a helicopter of the type having a tail rotor for counteracting main rotor torque, and with said control system comprising a housing adapted to be mounted to a rear end portion of the helicopter; a tethered drogue chute packed within said housing; means for deploying said drogue chute from said housing and to the rear of the helicopter in the event of tail rotor malfunction; and means for monitoring an operational performance characteristic of the tail rotor and for actuating said drogue chute deployment means in response to a detection of tail rotor malfunction.

Claim 3

The emergency anti-torque control system of claim 1 wherein said monitoring means comprises means for sensing tail rotor drive shaft vibrations.

Claim 4

The emergency anti-torque control system of claim 2 wherein said monitoring means further comprises means for sensing angular movement of the helicopter in a plane parallel to the path of travel of the main rotor.

Claim 5

An emergency anti-torque control system for a helicopter comprising a drogue chute adapted to be mounted to a rear end portion of the helicopter, means for monitoring tail rotor performance, and means for deploying said drogue chute in response to said monitoring means detecting the tail rotor to be malfunctioning.

Claim 6

An emergency anti-torque control system for a helicopter comprising a drogue chute adapted to be mounted to a rear end portion of the helicopter, means for monitoring tail rotor performance, and means for deploying said drogue chute in response to said monitoring means detecting the tail rotor to be malfunctioning.

Claim 7

The emergency anti-torque control system of claim 4 wherein said monitoring means comprises means for sensing levels of vibration of a tail rotor drive shaft.

Claim 8

The emergency anti-torque control system of claim 5 wherein said deployment means comprises a projectile tied to a drogue chute by a breakable line.

Claim 9

The emergency anti-torque control system of claim 6 further comprising microprocessor means for comparing levels of tail rotor drive shaft vibrations sensed by said monitoring means with respect to a preselected range of vibration levels and for generating a projectile fire signal in response to a sensed level being outside of said range.

Claim 10

The emergency anti-torque control system of claim 7 further comprising accelerometer means for sensing angular movement of the helicopter about the axis of a main rotor drive shaft, and wherein said microprocessor means is programmed to generate a projectile fire signal in response to a tail rotor drive shaft vibration level being detected outside of said preselected range and said accelerometer means sensing angular movement above a preselected speed.

Claim 13

An emergency anti-torque control system for a helicopter of the type having a tail rotor for counteracting main rotor torque, and with said control system comprising a housing adapted to be mounted to a rear end portion of the helicopter comprised of a movable, tubular section telescopically mounted to a stationary, tubular section; a projectile severably mounted to said movable housing section; a drogue chute packed within said housing and tethered by a moment cable; a pull line tethering said projectile to said drogue chute; and means for propelling said projectile from said housing to the rear of the helicopter, whereby upon the projectile being propelled it may telescopically extend the movable housing section beyond the tail rotor and deploy the drogue chute to the rear of the helicopter with the moment cable held clear of the tail rotor by the extended, movable housing section.

Claim 14

An emergency anti-torque control system for a helicopter of the type having a tail rotor for counteracting main rotor torque, and with said control system comprising a housing adapted to be mounted to a rear end portion of the helicopter comprised of a movable, tubular section telescopically mounted to a stationary, tubular section; a projectile severably mounted to said movable housing section; a drogue chute packed within said housing and tethered by a moment cable; a pull line tethering said projectile to said drogue chute; and means for propelling said projectile from said housing to the rear of the helicopter, whereby upon the projectile being propelled it may telescopically extend the movable housing section beyond the tail rotor and deploy the drogue chute to the rear of the helicopter with the moment cable held clear of the tail rotor by the extended, movable housing section.