Aircraft Collision Avoidance System

• US 20140340245A1
• Filed: 08/11/2014
• Published: 11/20/2014
• Est. Priority Date: 03/02/2009
• Status: Abandoned Application

• Current Assignee: Wingguard, LLC
• Original Assignee: Wingguard, LLC
• Inventors: Griffith, Gregory M.
• Application Number:
  US14/457,040
• Publication Number:
  US 20140340245A1
• Time in Patent Office: Days
• US Class Current: 340/961
• CPC Class Codes: B64F 1/228 remotely controlled; operating autonomously
• CPC Class Codes: G01S 13/86 Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
• CPC Class Codes: G01S 13/931 of land vehicles
• CPC Class Codes: G01S 13/934 on airport surfaces, e.g. while taxiing
• CPC Class Codes: G01S 2013/9316 combined with communication equipment with other vehicles or with base stations
• CPC Class Codes: G08B 3/10 using electric transmission; using electromagnetic transmission
• CPC Class Codes: G08G 5/04 Anti-collision systems
• CPC Class Codes: G08G 5/045 Navigation or guidance aids, e.g. determination of anti-collision manoeuvers radar or analogous systems specially adapted for anti-collision between aircraft G01S13/933
• CPC Class Codes: G08G 5/065 Navigation or guidance aids, e.g. for taxiing or rolling

Abstract

An aircraft collision avoidance system comprising (a) at least one separation monitoring device connectable to at least a portion of an aircraft, the separation monitoring device comprising (1) at least one transmitter and (2) at least one receiver and (b) a master unit.

Claims

1. An aircraft collision avoidance system, comprising:

at least one separation monitoring device connectable to at least a portion of an aircraft, the separation monitoring device comprising;

at least one transmitter capable of selectively transmitting signals which are reflected off of an object and received by at least one receiver, the reflected signals defining a separation distance between the at least one receiver and the object and wherein the at least one transmitter outputs a separation distance signal representative of the separation distance; and

a master unit for receiving and analyzing the separation distance signals output by the at least one transmitter and outputting a warning signal to a warning device when the at least one separation monitoring device is within a predetermined distance from the object.

3. The aircraft collision avoidance system according to claim 1, wherein a separation monitoring device is disposed on at least one of a wing and a horizontal stabilizer of an aircraft and the master unit communicates with the separation monitoring device to monitor the position of at least one of the wing and the horizontal stabilizer of the aircraft relative to an object.

4. The aircraft collision avoidance system according to claim 1, wherein the at least one separation monitoring device is connected to at least a portion of at least one of a wing and a horizontal stabilizer of an aircraft, wherein the at least one separation monitoring device transmits signals in an arcuate pattern both horizontally and substantially co-planar to at least one of the wing and the horizontal stabilizer and receives signals reflected off of an object and outputs a separation distance signal representing the separation distance between the object and the at least one separation monitoring device.

5. The aircraft collision avoidance system according to claim 1, wherein the at least one separation monitoring device is connected to at least a portion of at least one of a wing and a horizontal stabilizer of an aircraft, wherein the at least one separation monitoring device transmits and receives signals both vertically and substantially perpendicularly to at least one of the wing and the horizontal stabilizer and outputs a separation distance signal.

6. The aircraft collision avoidance system according to claim 1, wherein each wing, each horizontal stabilizer and at least a portion of a fuselage of an aircraft comprise at least one separation monitoring device.

7. The aircraft collision avoidance system according to claim 6, wherein when at least one of the wings of the aircraft are within a predetermined distance away from an object, the master unit communicates a warning to an individual so as to prevent collisions between at least one of the wings of the aircraft and an object.

8. The aircraft collision avoidance system according to claim 1, wherein the warning device comprises a speaker capable of communicating an audible warning when the warning device receives warning signals from the master unit.

9. The aircraft collision avoidance system according to claim 8, wherein when the separation distance between the separation monitoring device and the object decreases the audible warning increases in decibel level.

10. The aircraft collision avoidance system according to claim 1, wherein the warning device of the master unit comprises a visual display communicating a visible warning.

11. The aircraft collision avoidance system according to claim 10, wherein the visual display comprises a plurality of light emitting diodes which are illuminated when the master unit communicates a warning signal to the warning device.

12. The aircraft collision avoidance system according to claim 1, wherein the master unit is in electrical communication with a vehicle utilized to translate the aircraft.

13. The aircraft collision avoidance system according to claim 12, wherein when the at least one separation monitoring device is within a collision distance the master unit automatically stops the vehicle.

14. The aircraft collision avoidance system according to claim 1, wherein the master unit comprises a communicator device selected from the group consisting of:

a personal digital assistant, a cellular telephone, a laptop, or a global positioning device.

15. The aircraft collision avoidance system according to claim 1, wherein the at least one separation monitoring device and the master unit communicate wirelessly via at least one wireless communication protocol, wherein the at least one communication protocol is selected from the group consisting of:

Infrared, Bluetooth, Radio Frequencies or Wi-Fi.

20. The aircraft collision avoidance system according to claim 1, wherein the master unit is electrical communication with a vehicle utilized to translate the aircraft.

21. The aircraft collision avoidance system according to claim 20, wherein when the at least one transceiver is within a collision distance the master unit automatically stops the vehicle.

2. An aircraft collision avoidance system, comprising:

at least one wireless transceiver capable of selectively transmitting signals and receiving signals which are reflected back to the wireless transceiver off of an object in order to define a separation distance between the wireless transceiver and the object and wherein the wireless transceiver outputs a separation distance signal representative of the separation distance; and

a master unit for receiving and analyzing the separation distance signals output by the wireless transceiver, the master unit outputting a warning signal to a warning device when the wireless transceiver is within a predetermined distance from an object.

16. An aircraft collision avoidance system for monitoring the position of at least a portion of an aircraft relative to an object, the system comprising:

at least one separation monitoring device connected to at least a portion the aircraft, the separation monitoring device comprising;

at least one transceiver, the transceiver capable of transmitting signals and receiving signals which are reflected back to the transceiver off of at least a portion of the object to define a separation distance and wherein the at least one transceiver wirelessly outputs a separation distance signal; and

a master unit for receiving and analyzing the separation distance signals output by the at least one transceiver and outputting a warning signal to a warning device when the at least one transceiver is within a predetermined distance from the object.

17. An aircraft collision avoidance system according to claim 16, wherein the object is a door of a hangar.

18. An aircraft collision avoidance system according to claim 16, wherein the object is another aircraft.

19. The aircraft collision avoidance system according to claim 16, wherein each wing and each horizontal stabilizer and at least a portion of a fuselage of an aircraft comprise at least one separation monitoring device.