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Collision avoidance and warning system

  • US 9,196,168 B2
  • Filed: 05/20/2009
  • Issued: 11/24/2015
  • Est. Priority Date: 05/20/2009
  • Status: Active Grant
First Claim
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1. A collision avoidance and warning system for an aircraft, comprising:

  • a transceiver having a transmitter for transmitting radio waves and a receiver for receiving reflected radio waves from the radio waves transmitted by the transmitter, the transceiver being located on the aircraft;

    a ground-personnel warning signal system comprising;

    a speaker located near a region outside a pilot'"'"'s field of view for audibly alerting ground personnel; and

    a light located near the region outside the pilot'"'"'s field of view for visually alerting ground personnel;

    wherein the ground-personnel warning system is located on the aircraft for selectively issuing a ground-personnel warning signal to ground personnel from equipment worn by a detected person when the aircraft is on the ground;

    a flight-ground detection system located on the aircraft for determining whether the helicopter is on the ground or in flight; and

    a data processor located on the aircraft and configured to process data received from the transceiver and data received from the flight-ground detection system while the aircraft is in flight and on the ground, the data processor configured to selectively initiate an alert from the ground-personnel warning signal system to issue a ground-personnel warning signal based upon the flight-ground detection system determination of flight status;

    wherein the transmitter of the transceiver is configured for transmitting radio waves towards the region outside the pilot'"'"'s field of view; and

    wherein the flight-ground detection system comprises;

    a weight-on-gear switch;

    a collective pitch position sensor; and

    a radar altimeter.

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