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REFUELING
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Technical Examples
- Refueling booms with multiple couplings, and associated methods and systems, are disclosed. A system in accordance with one embodiment of the invention includes a deployable boom carrying a refueling passage. A first coupler carried by the boom can be operatively coupleable to the refueling passage. The first coupler can be configured to be releasably connected to a receiver aircraft during refueling. A second coupler can be carried by the boom and can be operatively coupleable to the refueling passage, with the second coupler being configured to be releasably connected to a receiver aircraft during refueling. In particular embodiments, the first and second couplers can have different configurations so as to be compatible with aircraft having different refueling arrangements.
- An in-flight refueling system and method are provided to extend and retract an in-flight refueling device between a stowed position and an extended position relative to a tanker aircraft. The system and method of the present invention provide an induction device configured to extend and retract the in-flight refueling device such that the in-flight refueling system requires less maintenance and may be packaged in a compact, low-profile arrangement so that the in-flight refueling system may be carried by a variety of tanker aircraft in a variety of different configurations.
- The invention pertains to a head piece (01) with a refueling coupler (02) for being connected to a tank, wherein several rigid pipe sections (03, 04, 05, 06, 07, 08) are provided for conveying the fuel, wherein the pipe sections (03, 04, 05, 06, 07, 08) are connected by means of several swivel joints (09, 10, 11, 12, 13, 14) in order to realize an adjustable spatial arrangement of the refueling coupler (02), and wherein at least a first swivel joint (09) and a second swivel joint (10) can be respectively swiveled about a horizontal swiveling axis (25, 26) in order to adjust the height of the refueling coupler (02). A parallel lever drive (15) is provided on the head piece (01) in order to hold a first pipe section (03) in a certain angular position during the height adjustment of the refueling coupler (02).
- A fueling and associated vapor recovery system maintains the same, or lower, vacuum level in the vapor hose during ORVR vehicle refueling as that seen during a non-ORVR refueling. A valve assembly is made as either a part of the end of the vapor recovery hose assembly, a separate unit that is placed between the hose assembly and the nozzle, or incorporated directly into the nozzle. The valve assembly is biased to one position by a spring to which is attached a sliding valve member. The force of the spring is sufficient to keep the valve member in the original position when refueling non-ORVR vehicles so that the vapor hose is unobstructed and an air bleed hole is closed. When refueling an ORVR vehicle, the elevated vacuum level moves the valve member to a second position which blocks off the vapor hose from the vacuum pump and opens up the vapor hose to the air bleed hole.
- An in-flight refueling system, damping device and method are provided for substantially reversing a change in the disposition of an elongate hose extending from a first aircraft during an in-flight refueling operation. The various embodiments of the present invention provide a compact, lightweight, and easily installed damping device that may act to minimize the occurrence of oscillations within the elongate hose that may act to produce a change in the disposition of the elongate hose. In addition, the embodiments of the present invention facilitate the detuning of the elongate hose and, for instance, an attached drogue that may oscillate uncontrollably at a resonant frequency in response to aerodynamic forces exerted on the hose and drogue during an in-flight refueling operation.
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