Distributed and Cable reduced TCAS

• US 7,583,223 B2
• Filed: 05/15/2007
• Issued: 09/01/2009
• Est. Priority Date: 09/18/2006
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Jones, James B., Brandao, Ruy C.
• Primary Examiner(s): Tarcza; Thomas H
• Assistant Examiner(s): GALT, CASSI J
• Application Number:
  US11/748,848
• Publication Number:
  US 20080068250A1
• Time in Patent Office: 840 Days
• Field of Search: 342 29- 32, 342 42- 49, 342/63, 343/705, 343/708, 340945-983, 701/120
• US Class Current: 342/30
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 3/46 using antennas spaced apart and measuring phase or time difference between signals therefrom, i.e. path-difference systems
• CPC Class Codes: G08G 5/0008 with other aircraft
• CPC Class Codes: G08G 5/0078 for monitoring traffic from the aircraft radar or analogous systems specially adapted for traffic control G01S13/91

Abstract

A direction finding antenna system for determining the relative bearing of a second aircraft from a first aircraft in conjunction with a Traffic Alert Collision Avoidance System (TCAS). The system includes a first antenna and a second antenna located on a top surface of the first aircraft, spaced apart along a first axis, as well as a third antenna and a fourth antenna located on a bottom surface of the first aircraft, spaced apart along a second axis orthogonal to the first axis. The system further includes a transmitting, receiving, and processing system coupled to the first, second, third, and fourth antennas, wherein the transmitting, receiving, and processing system is configured to transmit TCAS interrogations, receive TCAS replies, and process the TCAS replies to determine the relative bearing of the second aircraft from the first aircraft.

Claims

1. A direction finding antenna system located on a first aircraft for determining the relative bearing of a second aircraft from the first aircraft in conjunction with a Traffic Alert Collision Avoidance System (TCAS), the second aircraft being equipped to transmit signals received by the antenna system, the system comprising:

a first antenna and a second antenna located on a top surface of the first aircraft, spaced apart along a first axis;

a third antenna and a fourth antenna located on a bottom surface of the first aircraft, spaced apart along a second axis orthogonal to the first axis; and

a transmitting, receiving, and processing system coupled to the first, second, third, and fourth antennas,

wherein the transmitting, receiving, and processing system is configured to transmit TCAS interrogations, receive TCAS replies, and process the TCAS replies to determine the relative bearing of the second aircraft from the first aircraft, wherein the transmitting, receiving, and processing system includes a transmitter selectively coupled to at least one of the first, second, third, and fourth antennas, the transmitter configured to transmit TCAS interrogations omnidirectionally, and wherein each of the first antenna, the second antenna, the third antenna, and the fourth antenna have only a single element.

2. The system of claim 1, wherein the transmitting, receiving, and processing system is further configured to transmit transponder signals.

3. The system of claim 1, wherein the first, second, third, and fourth antennas are L-band blade antennas.

4. The system of claim 1, wherein the transmitter is further configured to transmit TCAS interrogations by generating a directional beam using at least two of the first, second, third, and fourth antennas.

5. The system of claim 1, wherein the transmitting, receiving, and processing system includes a line replaceable unit (LRU), the LRU including a receiver selectively coupled to the first, second, third, and fourth antennas.

6. The system of claim 5, wherein the receiver includes a first detector for detecting an aspect of signals received from the first antenna, a second detector for detecting an aspect of signals received from the second antenna, a third detector for detecting an aspect of signals received from the third antenna, and a fourth detector for detecting an aspect of signals received from the fourth antenna.

7. The system of claim 6, wherein the first, second, third, and fourth detectors each include a phase detector for detecting the phase of signals received from the first, second, third, and fourth antennas respectively.

8. The system of claim 7, wherein the first, second, third, and fourth detectors each include an amplitude detector for detecting the amplitude of signals received from the first, second, third, and fourth antennas respectively.

9. The system of claim 1, wherein the transmitting, receiving, and processing system comprises:

a first line replaceable unit (LRU); and

a second LRU in signal communication with the first LRU

wherein the first and second LRUs are configured to process bearing information in a distributed manner.

10. The system of claim 9, wherein the first LRU includes a first receiver selectively coupled to the first antenna and the third antenna and the second LRU includes a second receiver selectively coupled to the second antenna and the fourth antenna.

11. The system of claim 10, wherein the first receiver includes a first phase detector for detecting the phase of signals received from the first antenna and a second phase detector for detecting the phase of signals received from the third antenna.

12. A direction finding antenna system located on a first aircraft for determining the relative bearing of a second aircraft from the first aircraft in conjunction with a Traffic Alert Collision Avoidance System (TCAS), the second aircraft being equipped to transmit signals received by the antenna system, the system comprising:

a first two-element antenna located on a top surface of the first aircraft, having only a first element and a second element spaced apart along a first axis;

a second two-element antenna located on a bottom surface of the first aircraft, having only a first element and a second element spaced apart along a second axis orthogonal to the first axis; and

a transmitting, receiving, and processing system coupled to the first and second antennas,

wherein the transmitting, receiving, and processing system is configured to transmit TCAS interrogations, receive TCAS replies, and process the TCAS replies to determine the relative bearing of the second aircraft from the first aircraft and wherein the transmitting, receiving, and processing system includes a transmitter selectively coupled to at least one of the first, second, third, and fourth antennas, the transmitter configured to transmit TCAS interrogations omnidirectionally.

13. The system of claim 12, wherein the transmitting, receiving, and processing system is further configured to transmit transponder signals.