Dual mode frangible refueling nozzle
AssigneeNorthrop Grumman Systems Corporation
InventorJon F. Garruba
Life of this patent
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AssigneeNorthrop Grumman Systems Corporation
InventorJon F. Garruba
Estimating the term…
An in-flight refueling probe includes a first tubular member secured to an aircraft and a second tubular member having a releasable connection with the first tubular member such that the second tubular member detaches from the first tubular member in response to a predetermined force applied to the connection. A nozzle secured to the second tubular member can be coupled to a receptacle of a fuel dispensing aircraft. A tethering member is connected to the first tubular member and one of the second tubular member and the nozzle. The tethering member remains intact to connect the detached second tubular member to the first tubular member when a first tensile force is applied to the tethering member. The tethering member ruptures to disconnect the detached second tubular member from the first tubular member when a second tensile force greater than the first tensile force is applied to the tethering member.
An in-flight refueling probe for an aircraft to be refueled by a fuel dispensing aircraft having a receptacle for connecting to the refueling probe, the refueling probe comprising:
An in-flight refueling probe for an aircraft to be refueled by a fuel dispensing aircraft having a receptacle for connecting to the refueling probe, the refueling probe comprising:
An in-flight refueling probe for a fuel dispensing aircraft for refueling an aircraft having a receptacle for connecting to the refueling probe, the refueling probe comprising:
Dependencies are inferred from the claim text.