Systems and methods for collision avoidance

• US 7,541,944 B2
• Filed: 07/12/2004
• Issued: 06/02/2009
• Est. Priority Date: 07/12/2004
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Brouwer, Todd B., Konya, Kazuhide
• Primary Examiner(s): Lee; Benjamin C
• Assistant Examiner(s): Fan; Hongmin
• Application Number:
  US10/889,200
• Publication Number:
  US 20060007021A1
• Time in Patent Office: 1,786 Days
• Field of Search: 340/435, 340/933, 340/958, 340/961, 340/995.26, 340/945, 340/936, 701/301, 342 70- 72, 342/36, 342/63
• US Class Current: 340/945
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0078 for monitoring traffic from the aircraft radar or analogous systems specially adapted for traffic control G01S13/91
• CPC Class Codes: G08G 5/065 Navigation or guidance aids, e.g. for taxiing or rolling

Abstract

Systems and methods for collision avoidance are disclosed. In one embodiment, a method includes providing a proximity warning system operatively coupled to the aircraft and adapted to monitor a scanning area proximate a selected portion of the aircraft. The scanning area is monitored using the proximity warning system. A ground-based device within the scanning area is detected using the proximity warning system, and a distance between the ground-based device and the selected portion on the aircraft is determined using the proximity warning system. If the distance between the ground-based device and the selected portion does not exceed a selected minimum distance, then a warning signal is provided. In alternate embodiments, the proximity warning system provides a second warning signal distinguishable from the warning signal.

Claims

1. A method comprising performing ground-based service operations on an aircraft having a fuselage, nacelle and wings, the method including using a plurality of proximity warning devices on the aircraft to scan respective areas in front of selected portions of the nacelle, fuselage and wings of the aircraft while at least one ground-based service vehicle performs ground service operations on the aircraft;

and warning a vehicle operator whose vehicle enters a scanned area and approaches a safety clearance of the aircraft.

2. The method of claim 1, wherein the proximity devices include laser rangefinders for scanning the respective areas and also for determining distances of the at least one of those ground-bases service vehicles within the scanned areas from the selected portions.

3. The method of claim 1, wherein determining the distance of a ground-based vehicle from a selected portion includes:

determining a first distance, and wherein providing the warning comprises providing a first warning signal, wherein the first warning signal includes either an intermittent warning signal or a constant warning signal;

determining a second distance between the ground-based vehicle and the selected portion using the proximity warning devices; and

if the second distance does not exceed a second selected minimum distance, providing a second warning signal distinguishable from the first warning signal, wherein the second warning signal includes the other of the intermittent warning signal or the constant warning signal.

4. The method of claim 3, wherein the first and second warning signals are audible.

5. An aircraft, comprising:

a structural assembly including a fuselage, nacelles and wings; and

a plurality of proximity warning devices operatively coupled to the aircraft for scanning respective areas in front of selected portions of the fuselage, nacelles and wings while ground-based service equipment is performing ground service operations on the aircraft, the selected portions susceptible to damage by the ground-based equipment during the ground service operations, each proximity warning device configured to determine;

a first monitored distance between an object positioned in the corresponding scanning area and the selected portion, and to provide a first warning signal when the first monitored distance does not exceed a selected minimum distance; and

a second monitored distance between the object and the selected portion; and

if the second monitored distance does not exceed a second selected minimum distance, to provide a second warning signal distinguishable from the first warning signal.

6. The aircraft of claim 5, wherein the proximity warning devices include a laser scanning system having a rotating lens element.

7. The aircraft of claim 6, wherein the laser scanning system includes:

a controller operatively coupled to a laser rangefinder adapted to emit a laser beam; and

a scanning assembly adapted to receive the laser beam and to at least one of transmit, reflect, and refract the laser beam over the scanning area.

8. The aircraft of claim 5, wherein the monitored distance comprises a first monitored distance, and the warning signal comprises a first warning signal, and wherein the proximity warning device is further adapted to

determine a second monitored distance between the ground-based device and the selected portion;

and

if the second monitored distance does not exceed a second selected minimum distance, to provide a second warning signal distinguishable from the first warning signal.