Method and apparatus for alerting pilot to transponder antenna failure in a traffic alert and collision avoidance system

• US 5,629,692 A
• Filed: 07/20/1995
• Issued: 05/13/1997
• Est. Priority Date: 07/20/1995
• Status: Expired due to Term

• Current Assignee: L-3 Communications Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Stayton, Gregory T., Zinder, David A., Stelling, Desi D.
• Primary Examiner(s): Hofsass, Jeffery
• Assistant Examiner(s): Lee, Benjamin C.
• Application Number:
  US08/504,977
• Time in Patent Office: 663 Days
• Field of Search: 340/945, 340/961, 340/963, 340/635, 340/650, 340/652, 340/653, 342/165, 342/173, 342/174, 342/42, 455/115, 455/226.1, 364/461, 371/68.1
• US Class Current: 340/961
• CPC Class Codes: G01S 13/765 with exchange of information between interrogator and responder
• CPC Class Codes: G01S 13/767 Responders; Transponders teaching or practice apparatus for gun-aiming or gun-laying using reflecting targets or active targets F41G3/26
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 7/4004 of parts of a radar system
• CPC Class Codes: G08G 5/0008 with other aircraft
• CPC Class Codes: G08G 5/0095 Aspects of air-traffic control not provided for in the other subgroups of this main group

Abstract

A system for use with aircraft having a collision avoidance system which employs i) two transponder systems each including two antennas and a selected one of two transponders and ii) a failure warning when a transponder system failure occurs, to permit the aircraft to take off when the failure warning is the result of only one antenna failure.

Claims

1. In an aircraft warning system that uses first and second transponder systems with each transponder system including first and second antennas and a selected one of first and second transponders either of which are connected to the first and second antennas by a transponder switch, the warning system further including a selector switch when in a first position is operable to provide a first warning when intruder aircraft are about to enter a first zone which is within no less than a first time period in advance of possible collision and a second warning when intruder aircraft are about to enter a closer zone which is within no less than a second time period in advance of a possible collision, and the selector switch in a second position is operable to provide the first warning only, the warning system also including a failure warning when there is a transponder system failure using the first transponder, the method of extinguishing the failure warning whenever the failure warning is due to only a single antenna failure comprising the steps of:

A. upon receiving the failure warning, selecting the second transponder and if the failure warning is not then extinguished,

B positioning the selector switch in the second position, in which case the failure warning will thereby be extinguished if only a single antenna failed.

2. The method of claim 1 wherein the warning system transponder switch is operable in a first position to connect the first transponder to the two antennas and in a second position to connect the second transponder to the two antennas and wherein step A includes selecting the second transponder by positioning the transponder switch in the second position.

3. The method of claim 1 wherein the selector switch has a third position in which the transponders may operate without the first and second warnings and wherein step B includes positioning the selector switch in the second or third position to extinguish the failure warning if only a single antenna failed.

4. The method of claim 2 wherein the warning system transponder switch is operable in a first position to connect the first transponder to the two antennas and in a second position to connect the second transponder to the two antennas and wherein step A includes selecting the second transponder by positioning the transponder switch in the second position.