Power line detection system

• US 5,351,032 A
• Filed: 02/19/1993
• Issued: 09/27/1994
• Est. Priority Date: 02/19/1993
• Status: Expired due to Fees

• Current Assignee: United States Department of Energy
• Original Assignee: Regents of the University of California (University of California)
• Inventors: Latorre, Victor R., Watwood, Donald B.
• Primary Examiner(s): Peng, John K.
• Assistant Examiner(s): TONG, NINA C
• Application Number:
  US08/019,696
• Time in Patent Office: 585 Days
• Field of Search: 340/310 R, 340/310 A, 340/870.31, 340/870.07, 340/538, 340/657, 324/127, 324/133, 364/483, 364/492
• US Class Current: 340/983
• CPC Class Codes: G01S 1/68 Marker, boundary, call-sign, or like beacons transmitting signals not carrying directional information

Abstract

A short-range, radio frequency (RF) transmitting-receiving system that provides both visual and audio warnings to the pilot of a helicopter or light aircraft of an up-coming power transmission line complex. Small, milliwatt-level narrowband transmitters, powered by the transmission line itself, are installed on top of selected transmission line support towers or within existing warning balls, and provide a continuous RF signal to approaching aircraft. The on-board receiver can be either a separate unit or a portion of the existing avionics, and can also share an existing antenna with another airborne system. Upon receipt of a warning signal, the receiver will trigger a visual and an audio alarm to alert the pilot to the potential power line hazard.

Claims

1. A power line detection system for air borne vehicles, said system including at least one transmission line, said system comprising:

at least one radio-frequency (RF) transmitter mounted on said at least one transmission line;

a RF receiver located on board an aircraft wherein said receiver is tuned to receive a transmission from said at least one RF transmitter, wherein said RF receiver comprises;

a RF antenna;

a first receiver channel to receive a first frequency from said RF antenna;

a second receiver channel to receive a second frequency from said RF antenna; and

a first comparator to compare signals from said first receiver channel and said second receiver channel wherein said first comparator sends a signal that is the stronger receiver channel signal of the compare signals to a display and alarm system;

the display and alarm system located on-board the aircraft, said display and alarm system receiving the stronger receiver channel signal from said first comparator, said display and alarm system comprising;

a first display to indicate a power line altitude signal and identification number of said at least one transmitter;

a barometric pressure corrected altimeter producing an aircraft altitude signal;

a second display to indicate said aircraft altitude signal;

a second comparator to compare said aircraft altitude signal with said power line altitude signal;

a third display to indicate the difference between said aircraft altitude signal and said power line altitude signal plus a margin of error; and

an audio and visual alarm that receives signals from said second comparator, wherein said audio and visual alarm is triggered when said aircraft altitude is less than said power line altitude plus said margin of error.

2. The system of claim 1, wherein said RF transmitter is mounted within a warning ball mounted onto said at least one transmission line.

3. The system of claim 2, wherein said RF transmitter comprises:

a power transducer to derive power from said at least one transmission line;

a loop antenna powered by said power transducer;

a common sensor to sense when said at least one transmission line is not powered; and

a back-up battery to power said at least one RF transmitter when said common sensor senses that said at least one transmission line is not powered.

4. The system of claim 3, wherein said power transducer has spacing, coil diameter, and number of turns that are determined by the actual power used by said at least one RF transmitter.

5. The system of claim 1, wherein said at least one RF transmitter is mounted on at least one of a plurality of towers of a transmission line complex, said at least one RF transmitter having a vertical antenna.

6. The system of claim 1, wherein said at least one RF transmitter transmits the altitude and position information of said at least one transmission line.

7. The system of claim 1, wherein said at least one RF transmitter has a frequency that has been selected to be different from that of an adjacent RF transmitter.

8. In an existing transmission line complex including at least one tower and at least one transmission line, the improvement comprising a detection system, said detection system including:

at least one radio-frequency (RF) transmitter mounted on said at least one transmission line;

a RF receiver located on board an aircraft wherein said RF receiver is tuned to receive a transmission from said at least one RF transmitter; and

wherein said RF receiver comprising;

a RF antenna;

a first receiver channel to receive a first frequency from said RF antenna;

a second receiver channel to receive a second frequency from said RF antenna; and

a first comparator to compare signals from said first receiver channel and said second receiver channel wherein said first comparator sends a signal to a display and alarm system after comparing the signals from the first and second receiver channels

the display and alarm system located on-board said aircraft wherein said display and alarm system is triggered by said RF receiver when said RF receiver receives a transmission from said at least one RF transmitter, said display and alarm system comprising;

a first display to indicate a Dower line altitude signal and identification number of said at least one RF transmitter;

a barometric pressure corrected altimeter producing an aircraft altitude signal;

a second display to indicate said aircraft altitude signal;

a comparator to compare said aircraft altitude signal with said power line altitude signal;

a third display to indicate the difference between said aircraft altitude signal and said power line altitude signal plus a margin of error; and

an audio and visual alarm that receives signals from said comparator, wherein said audio and visual alarm is triggered when said aircraft altitude is less than said power line altitude plus said margin of error.