Flight refuelling system

• US 5,499,784 A
• Filed: 05/11/1994
• Issued: 03/19/1996
• Est. Priority Date: 05/12/1993
• Status: Expired due to Term

• Current Assignee: Airbus Operations SAS (Airbus SE)
• Original Assignee: Aerospatiale Societe Nationale Industrielle
• Inventors: Maury, Julien, Mitonneau, Gilbert, Crabere, Henri
• Primary Examiner(s): Cuchlinski, Jr., William A.
• Assistant Examiner(s): MARQUIS, LISSI MOJICA
• Application Number:
  US08/241,018
• Time in Patent Office: 678 Days
• Field of Search: 244/135 R, 244/135 A, 244/1 R, 340/945, 345/115, 345/118, 345/119
• US Class Current: 244/135.00A
• CPC Class Codes: B64D 39/00 Refuelling during flight filling or emptying fuel tanks B64D37/14
• CPC Class Codes: B64D 43/00 Arrangements or adaptations of instruments arrangements of cameras B64D47/08; aeronautical measuring instruments per se G01C

Abstract

The invention relates to a system for the flight refueling of at least one first aircraft provided with an intermediate fuel intake means connected to at least one fuel tank, by a second aircraft equipped with an intermediate fuel supply means connected to at least one fuel supply tank and which can be connected to the intermediate fuel intake means so as to permit, with the aid of at least one fuel pump, the transfer of fuel contained in the tank(s) of the second aircraft to the tank(s) of the first aircraft. This system includes at least one camera positioned below the aircraft, at least one multimode display to display at least one image from a camera and symbology information such as fuel data information used during the refueling operation. The system further includes multifunction equipment incorporating a screen for monitoring the refueling operation and a control keyboard to control several operations, in a single work station within the second aircraft for checking the flight refueling of the first aircraft.

Claims

1. System for the flight refueling of at least one first aircraft, equipped with an intermediate fuel intake means connected to at least one fuel tank, by a second aircraft, equipped with an intermediate fuel supply means including refueling means connected to at least one fuel supply tank and connectable to the intermediate fuel intake means so as to permit, with the aid of at least one fuel pump, the transfer of the fuel contained in the supply tank(s) of the second aircraft to the fuel tank(s) of said first aircraft, at least one camera being located below the fuselage of the second aircraft, at least one means for providing symbology information comprising a diagrammatic representation of the relative position of said supply means and fuel intake means and/or fuel data information including the location of fuel quantities for the first aircraft, at least one multimode display being installed in a working station within the second aircraft for displaying an image from the camera and for displaying an image of said symbology information either simultaneously or sequentially and at least one multifunction equipment comprising a screen and means for monitoring on said screen the refueling operation by day or night from said working station and a control keyboard for controlling several operations including the operation of said telescopic tube as well as for providing an operator with refueling information to monitor and assist in the refueling procedure throughout the refueling phase from the working station.

2. System according to claim 1, wherein the working station is located in the cockpit area.

3. System according to claim 1, wherein the intermediate fuel intake means is a probe installed at the front of the first aircraft and the intermediate fuel supply means is a refuelling pod installed beneath the wing or a winch mounted beneath the fuselage of the second aircraft.

4. System according to claim 1, wherein the intermediate fuel intake means is a receptacle located on the front, upper part of the first aircraft and the intermediate fuel supply means is a telescopic tube located below the fuselage of the second aircraft.

5. System according to claim 4, wherein a camera is located on the telescopic tube.

6. System according to claim 1, wherein a symbology of each multimode screen is associated with navigational data.

7. System according to claim 1, wherein each multifunction equipment functions in the form of successive menu pages.

8. System according to claim 6, wherein said multifunction equipment further comprises a loader (magnetic or optical reader) for updating said navigation data.