Aircraft proximity warning indicator

• US 4,139,848 A
• Filed: 06/17/1976
• Issued: 02/13/1979
• Est. Priority Date: 06/17/1976
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Corporation
• Original Assignee: Westinghouse Electric Company LLC (Brookfield Asset Management Incorporated)
• Inventors: Maxwell, Richard F. Jr.
• Primary Examiner(s): Wilbur, Maynard R.
• Assistant Examiner(s): Goodwin, Lawrence
• Application Number:
  US05/697,100
• Time in Patent Office: 971 Days
• Field of Search: 343/6 DF, 343/6 ND, 343/6 TV, 343/6 R, 343/6.5 R, 343/6.5 SS, 343/6.8 R, 343/5 PD, 343/112 CA, 343/113 R, 356/4, 356/5, 356/
• US Class Current: 342/30
• CPC Class Codes: G01S 13/867 Combination of radar systems with cameras
• CPC Class Codes: G01S 17/87 Combinations of systems using electromagnetic waves other than radio waves

Abstract

An aircraft proximity warning indicator incorporating an RF receiver, optical sensor, and display is described which may receive an RF signal followed by an optical radiation pulse from another aircraft where the received RF signal is used to control the optical sensor and display so that it senses and displays the optical radiation pulse.

Claims

1. A method for a first aircraft to provide proximity warning to a second aircraft comprising the steps of:

generating and transmitting by said first aircraft a radio frequency signal indicative that an optical radiation pulse is about to occur;

generating an optical radiation pulse later in time by a predetermined amount than said radio frequency signal by said first aircraft;

receiving said radio frequency signal by said second aircraft;

sensing said optical radiation pulse during a predetermined amount of time after receiving said radio frequency signal by said second aircraft;

displaying said sensed optical radiation pulse by said second aircraft;

generating and transmitting a second signal by said second aircraft;

receiving said second signal by said first aircraft;

transmitting a third signal by said first aircraft;

receiving said third signal by said second aircraft;

measuring the elapsed time from the transmission of said second signal to the reception of said third signal; and

converting said elapsed time into an indication of range between said first aircraft and second aircraft.

2. Apparatus for a first and second aircraft to provide proximity warning to said second aircraft comprising:

means for generating and transmitting a radio frequency signal by said first aircraft;

means for generating an optical radiation pulse later in time by a predetermined amount than said radio frequency signal by said first aircraft;

means for receiving said radio frequency signal by said second aircraft;

means for sensing said optical radiation pulse during a predetermined amount of time after receiving said radio frequency signal by said second aircraft;

means for displaying said sensed optical radiation pulse by said second aircraft;

means for generating and transmitting a second signal by said second aircraft;

receiving said second signal by said first aircraft;

transmitting a third signal by said first aircraft;

receiving said third signal by said second aircraft;

measuring the elapsed time from the transmission of said second signal to the reception of said third signal; and

means for converting said elapsed time into an indication of range between said first aircraft and second aircraft.