Parking guidance system for aircraft

• US 4,184,655 A
• Filed: 09/19/1977
• Issued: 01/22/1980
• Est. Priority Date: 09/29/1976
• Status: Expired due to Term

• Current Assignee: Safegate AB A Swedish Joint-Stock Company
• Original Assignee: Nils-Eric Anderberg
• Inventors: Anderberg, Nils-Eric
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US05/834,613
• Time in Patent Office: 855 Days
• Field of Search: 244/114 R, 116/50, 116/29, 116/124 R, 340/23, 340/31 R, 340/26, 340/37, 340/51, 340/25, 340/24, 340/38 L, 340/38 R, 340/38 P, 246/77, 246/122 R, 246/167 R, 246/182 B, 246/187 R, 200/86 A, 73/178 T, 180/1 AP
• US Class Current: 340/958
• CPC Class Codes: B64F 1/002 Taxiing aids

Abstract

A guidance system for use by a pilot in parking an aircraft on a parking place at an air terminal building and in stopping the aircraft at an exactly predetermined stopping point in the parking place. The system includes a transmitter unit having a plurality of transmitter elements disposed on the ground in the region of the parking place and successively following upon each other in the direction of travel of the aircraft. When the nose wheel of the aircraft successively passes over the transmitter elements these elements activate an information unit preferably mounted on the air terminal building within the pilot'"'"'s field of vision. The information unit includes indicator elements which continuously inform the pilot of the length of the distance up to the stopping point and when this stopping point is reached.

Claims

1. A system for guiding a pilot taxiing an aircraft, having a plurality of wheels, on the ground in such a way that the pilot is enabled to stop the aircraft with satisfactory accuracy at a predetermined stopping point in a parking place, said system comprising a transmitter unit disposed in the region of the parking place and having a plurality of transmitter elements disposed on the surface of the ground successively following each other in a line at spaced locations in the direction of travel of the aircraft as the aircraft approaches the stopping point to cause a selected one of the plurality of wheels to roll successively over the transmitter elements as the aircraft approaches the stopping point;

and an information unit operatively connected to the transmitter unit to provide, in response to the passage of said one wheel over successive ones of the transmitter elements toward the stopping point, a continuous quantitative indication of the remaining distance between the one of said spaced locations over which said one wheel is rolling and the stopping point.

2. A system as claimed in claim 1 further comprising means for selectively dividing said transmitter elements into groups and activating a group of the transmitter elements selected in accordance with the type of aircraft to be parked.

3. A system as claimed in claim 2, wherein the means for selectively dividing and activating comprises a push-button unit in the traffic control tower.

4. A system as claimed in claim 2, wherein the means for selectively dividing and activating comprises a push-button unit in a control panel for a passenger loading device at which the aircraft is to be parked.

5. A system as claimed in claim 2, wherein at least the transmitter elements of each group are spaced equal distances apart in the direction of travel of the aircraft.

6. A system as claimed in claim 1, wherein the transmitter elements are formed by elongated contactors directed transversely of the direction of travel of the aircraft.

7. A system as claimed in claim 6, wherein the contactors operate on the pressure wave principle.

8. A system as claimed in claim 6, wherein the contactors operate on the resistance strain principle.

9. A system as claimed in claim 1, wherein the information unit is in the form of an indicator instrument having a number of indicator elements corresponding to the number of transmitter elements in each group, said indicator elements indicating the length of the remaining distance and telling the pilot when to stop.

10. A system as claimed in claim 9, wherein the indicator instrument also has an indicator element which indicates the group of transmitter elements connected and thus the type of aircraft to be guided.

11. A system as claimed in claim 10, wherein the indicator elements emit light signals when activated by the transmitter elements.

12. A system as claimed in claim 11, wherein the indicator instrument is disposed in the aircraft cockpit.

13. A system as claimed in claim 1, wherein the information unit is in the form of a sound tape which can be set in motion from the one of the transmitter elements in the connected group which is first passed and which informs the pilot of the length of the remaining distance and tells him when to stop.

14. A system as claimed in claim 13, wherein the sound tape is connected to a radio transmitter located outside the aircraft and sending the information to the pilot.

15. A system as claimed in claim 13, wherein the sound tape is contained in a tape recorder installed in the aircraft.

16. A system as claimed in claim 10, wherein the indicator elements emit sound signals when activated by the transmitter elements.

17. A system as claimed in claim 10, wherein the indicator elements emit light and sound signals when activated by the transmitter elements.

18. A system as claimed in claim 10, wherein the indicator instrument is disposed on the ground in front of the aircraft when the aircraft is stopped at the predetermined stopping point.

19. A system as claimed in claim 10, wherein the indicator instrument is disposed at an air terminal building in front of the aircraft when the aircraft is stopped at the predetermined stopping place.