System and method for identifying a receiving aircraft during airborne fueling

• US 9,090,354 B2
• Filed: 03/02/2006
• Issued: 07/28/2015
• Est. Priority Date: 03/02/2006
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Oman, Eric P., Iverson, Donald G. Jr., Yeoman, Paul D.
• Primary Examiner(s): Xavier, Valentina
• Application Number:
  US11/366,858
• Publication Number:
  US 20070205328A1
• Time in Patent Office: 3,435 Days
• Field of Search: 244/135.R, 244/135.A, 244/136
• US Class Current: 1/1
• CPC Class Codes: B64D 39/00 Refuelling during flight filling or emptying fuel tanks B64D37/14
• CPC Class Codes: B64D 39/06 Connecting hose to aircraft; Disconnecting hose therefrom
• CPC Class Codes: B67D 7/04 for transferring fuels, lubricants or mixed fuels and lubricants
• CPC Class Codes: B67D 7/14 responsive to input of recorded programmed information, e.g. on punched cards
• CPC Class Codes: B67D 7/3245 relating to the transfer method

Abstract

A system for effecting automatic identifying of a receiving aircraft receiving fuel from a fuel delivery apparatus in a delivering aircraft during an airborne fueling operation includes: (a) a first unit coupled with the receiving aircraft; (b) a second unit coupled with the delivering aircraft; and (c) a processing unit coupled with at least one of the first unit and the second unit. The first and second units cooperate to effect communicative coupling for conveying identifying information between the receiving aircraft and the delivering aircraft. The processing unit cooperates with at least one of the first unit and the second unit for employing the identifying information to effect the identifying.

Claims

1. A system for accounting for fueling of a receiving aircraft during airborne fueling of said receiving aircraft by a delivering aircraft;

the system comprising;

(a) at least one identifying indicia affixed with said receiving aircraft;

said at least one identifying indicia uniquely indicating individual identity of said receiving aircraft;

(b) at least one identity recognizing unit associated with said delivering aircraft;

said at least one identity recognizing unit automatically recognizing data provided by said at least one identifying indicia within a predetermined distance;

(c) a processing unit associated with at least one of said delivering aircraft and said receiving aircraft;

said processing unit cooperating with said at least one recognizing unit to ascertain said individual identity during said airborne fueling;

(d) a fueling apparatus coupled with said processing unit;

said fueling apparatus providing information to said processing unit indicating an amount of fuel provided to said receiving aircraft during said airborne refueling;

said fueling apparatus and said processing unit cooperating to accumulate information in a predetermined form to automatically record said amount of fuel in association with and said individual identity; and

(e) a fuel receiving structure via which said receiving aircraft is coupled with said fueling apparatus while receiving fuel, said fuel receiving structure is repositionable so as to present a more aerodynamic profile when not engaged in a fueling operation;

said identifying indicia being affixed proximate said fuel receiving structure so as to be exposed for interrogation by said identity recognizing unit during the fueling operation and to be disposed in a protected environment when not engaged in the fueling operation.

2. A system for accounting for fueling of a receiving aircraft during airborne fueling of said receiving aircraft by a delivering aircraft as recited in claim 1 wherein said fuel receiving structure is closed when said receiving aircraft is not engaged in a fueling operation;

said identifying indicia being affixed inside said fuel receiving structure when said fuel receiving structure is closed.

3. A system for accounting for fueling of a receiving aircraft during airborne fueling of said receiving aircraft by a delivering aircraft as recited in claim 1 wherein said processing unit includes a data port configured for downloading information related to said fueling.

4. A system for accounting for fueling of a receiving aircraft during airborne fueling of said receiving aircraft by a delivering aircraft as recited in claim 1 wherein said processing unit is situated in said receiving aircraft;

said processing unit being coupled with said at least one recognizing unit and with said fueling apparatus during said airborne refueling operation.

5. A system for accounting for fueling of a receiving aircraft during airborne fueling of said receiving aircraft by a delivering aircraft as recited in claim 1 wherein said processing unit is situated in said delivery aircraft.

6. A system for accounting for fueling of a receiving aircraft during airborne fueling of said receiving aircraft by a delivering aircraft as recited in claim 1 wherein said processing unit includes a data port configured for downloading information related to said fueling.

7. A system for accounting for fueling of a receiving aircraft during airborne fueling of said receiving aircraft by a delivering aircraft as recited in claim 1 wherein said processing unit is situated in said receiving aircraft;

said processing unit being coupled with said at least one recognizing unit and with said fueling apparatus during said airborne refueling operation.

8. A system for accounting for fueling of a receiving aircraft during airborne fueling of said receiving aircraft by a delivering aircraft as recited in claim 1 wherein said processing unit is situated in said delivery aircraft.

9. A system for accounting for fueling of a receiving aircraft during airborne fueling of said receiving aircraft by a delivering aircraft as recited in claim 6 wherein said processing unit is situated in said delivery aircraft.

10. A system for accounting for fueling of a receiving aircraft during airborne fueling of said receiving aircraft by a delivering aircraft as recited in claim 1 wherein the fuel receiving structure comprises a fuel receiving probe configured to close or be retracted within the receiving aircraft when not engaged in the fueling operation.

11. A system for accounting for fueling of a receiving aircraft during airborne fueling of said receiving aircraft by a delivering aircraft as recited in claim 10 wherein the identifying indicia is located on the fuel receiving probe.

12. A system for accounting for fueling of a receiving aircraft during airborne fueling of said receiving aircraft by a delivering aircraft as recited in claim 10 wherein the identifying indicia is located within the fuel receiving probe.

13. A system for accounting for fueling of a receiving aircraft during airborne fueling of said receiving aircraft by a delivering aircraft as recited in claim 1 wherein the fuel receiving structure is configured to withdraw into a cavity defined by the receiving aperture when not engaged in the fueling operation, and wherein the identifying indicia is located within the cavity defined by the receiving aperture during the fueling operation.