Aircraft refueling system and method of refueling an aircraft
AssigneeThe Boeing Company
InventorKevin Julian Chang
Life of this patent
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Abstract
An aircraft refueling system for use with a supplying aircraft is provided. The refueling system includes at least two strips of material coupled to a lower portion of the supplying aircraft. The at least two strips are separated by a distance and comprise a material that facilitates the at least two strips becoming progressively visible to a pilot of a receiving aircraft as the receiving aircraft approaches the supplying aircraft.
Claims20
An aircraft refueling system for use with a supplying aircraft, said refueling system comprising:
- at least two strips of material coupled to a lower portion of the supplying aircraft, said at least two strips are separated by a distance and comprise a material that facilitates said at least two strips becoming progressively visible to a pilot of a receiving aircraft as the receiving aircraft approaches the supplying aircraft;
- wherein said at least two strips comprising a first strip and a second strip, wherein only said first strip is visible to the receiving aircraft pilot when the receiving aircraft is in a first position relative to the supplying aircraft, and wherein said first strip and said second strip are visible to the receiving aircraft pilot when the receiving aircraft is in a second position relative to the supplying aircraft.
An aircraft refueling system comprising:
- a hose extending downward from a lower portion of a supplying aircraft, wherein a free end of said hose is configured to mate with a fuel receptacle extending from a receiving aircraft;
- and
- a ranging system coupled to the lower portion of the supplying aircraft, said ranging system comprising self-illuminating material configured to indicate, to a pilot of the receiving aircraft, positioning of the receiving aircraft relative to the supplying aircraft during low-light conditions, wherein only a first portion of said ranging system is visible to the receiving aircraft pilot when the receiving aircraft is a first distance from the supplying aircraft, and wherein said first portion and a second portion of said ranging system are visible to the receiving aircraft pilot when the receiving aircraft is a second distance from the supplying aircraft, the second distance being shorter than the first distance.
A method of refueling an aircraft, said method comprising:
- coupling a ranging system to a lower portion of a supplying aircraft, wherein the ranging system includes at least two strips of material separated by a distance, wherein the at least two strips include a first strip and a second strip, only the first strip being visible to the receiving aircraft pilot when the receiving aircraft is in a first position relative to the supplying aircraft, and wherein the first strip and the second strip are visible to the receiving aircraft pilot when the receiving aircraft is in a second position relative to the supplying aircraft;
- and
- positioning, with the ranging system, the receiving aircraft in a refueling position relative to the supplying aircraft, wherein the at least two strips become progressively visible to a pilot of the receiving aircraft as the receiving aircraft approaches the supplying aircraft.
Dependencies are inferred from the claim text.