Method and apparatus for accomplishing extended range TCAS

• US 5,805,111 A
• Filed: 12/01/1995
• Issued: 09/08/1998
• Est. Priority Date: 12/01/1995
• Status: Expired due to Term

• Current Assignee: L-3 Communications Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Smith, Mark Dean, Brettner, William Howard III
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US08/566,357
• Time in Patent Office: 1,012 Days
• Field of Search: 342/29, 342/455, 364/461, 343/705, 343/708
• US Class Current: 342/455
• CPC Class Codes: G01S 13/762 with special measures concerning the radiation pattern, e.g. S.L.S. aerials or aerial systems providing at least two radiation patterns, e.g. providing sum and difference patterns, H01Q25/00
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft

Abstract

A Traffic Alert and Collision Avoidance System(TCAS) antenna is mounted on a selected forward portion of an aircraft thereby extending the effective forward range of the TCAS. The antenna and ground plane are tilted relative to conventional TCAS antennas thereby aligning a peak of the antenna'"'"'s radiation pattern along the aircraft'"'"'s level line of flight. The resulting increased gain directed forward of the aircraft increases the forward range of the TCAS for both receiving and transmitting TCAS signals. The invention is also useful to extend the range of other aircraft systems including transponders. Alternate embodiments include tilting a conventional TCAS antenna mounted on a middle portion of the aircraft.

Claims

1. A Traffic Alert and Collision Avoidance System for an aircraft, said system comprising:

a) a TCAS computer unit; and

,

b) an antenna in communication with said computer unit, said antenna characterized by an elevation radiation pattern having a peak which substantially aligns with said aircraft'"'"'s level line of flight.

2. The Traffic Alert and Collision Avoidance System according to claim 1 wherein said antenna is tilted at an appropriate angle relative to said aircraft'"'"'s level line of flight such that said peak of said radiation pattern projects substantially forward of said aircraft.

3. The Traffic Alert and Collision Avoidance System according to claim 2 wherein said antenna is mounted on a selected forward portion of said aircraft.

4. The Traffic Alert and Collision Avoidance System according to claim 2 further comprising a shim positioned between said antenna and said aircraft for tilting said antenna.

5. The Traffic Alert and Collision Avoidance System according to claim 2 wherein said antenna is an approximately omnidirectional type antenna.

6. The Traffic Alert and Collision Avoidance System according to claim 2 wherein said antenna is a directional type antenna.

7. An extended range TCAS for aircraft, said TCAS comprising:

a) TCAS computer means for interpreting received TCAS signals; and

,

b) ERTCAS antenna means, in communication with said computer means, for receiving TCAS signals, said TCAS antenna means having a peak gain directed substantially in front of said aircraft and aligned along said aircraft'"'"'s level line of flight.

8. The extended range TCAS according to claim 7 wherein said ERTCAS antenna means is an antenna tilted at a suitable angle relative to normal of said aircraft'"'"'s level line of flight.

9. The extended range TCAS according to claim 8 wherein said ERTCAS antenna means is an antenna mounted on a suitably angled portion of said aircraft such that said peak gain is substantially aligned along said aircraft'"'"'s level line of flight.

10. The extended range TCAS according to claim 9 wherein said ERTCAS antenna means is an antenna mounted on the forward portion of said aircraft.

11. The extended range TCAS according to claim 7 wherein said TCAS computer means includes means for generating TCAS signals and said ERTCAS antenna means includes means for transmitting said generated TCAS signals.

12. The extended range TCAS according to claim 7 further comprising:

a) transponder means, in communication with said TCAS computer means, for transmitting and receiving transponder signals; and

,

b) extended range transponder antenna means, in communication with said transponder means, for receiving and transmitting transponder signals, said transponder antenna means having a peak gain substantially aligned along said aircraft'"'"'s level line of flight.

13. A method of extending the range of a Traffic Alert and Collision Avoidance System(TCAS) of an aircraft, said TCAS including a transmitter, said method comprising:

a) providing an antenna, said antenna in communication with said transmitter; and

,

b) mounting said antenna on said aircraft such that a peak gain of said antenna is directed in a desired elevation and azimuth relative to said aircraft such that the range of said TCAS is extended in the desired elevation and azimuth.

14. The method according to claim 13 wherein said desired elevation is between -10 degrees and +10 degrees relative to said aircraft'"'"'s level line of flight.

15. The method according to claim 14 wherein said desired elevation is approximately 0 degrees relative to said aircraft'"'"'s level line of flight and said desired azimuth is approximately 0 degrees relative to said aircraft'"'"'s level line of flight.

16. The method according to claim 13 wherein said mounting step includes tilting said antenna between 5 and 35 degrees from normal to the aircraft'"'"'s level line of flight.

17. The method according to claim 16 wherein said mounting step includes mounting said antenna on a suitably angled portion of the forward portion of said aircraft.

18. The method according to claim 13 wherein said antenna is an omnidirectional type antenna.

19. The method according to claim 13 wherein said antenna is a directional type antenna.

20. The method according to claim 13 wherein said TCAS includes a receiver and said antenna is in communication with said receiver.

21. An extended range transponder system for an aircraft, said transponder system comprising:

a) transponder means for receiving and processing transponder signals;

b) antenna means, in communication with said transponder means, for receiving said transponder signals and communication said transponder signals to said transponder means, said antenna means having a peak gain substantially aligned along said aircraft'"'"'s level line of flight.

22. The extended range transponder system according to claim 21 wherein said transponder means includes transmitter means for generating transponder signals and said antenna means includes means for radiating said generated transponder signals to free space.