Device to reduce the lateral force generated by aerial...

Aeronautics and astronautics – Aircraft structure – Fuel supply

Reexamination Certificate

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Reexamination Certificate

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07726608

ABSTRACT:
Device to reduce the lateral force generated by an aerial refueling boom (11) of an aircraft characterized in that it has at least one plate (31), the plate (31) has two cantilevered wings (32, 33), the wings (32, 33) have perforations (34), so that the wake produced in the boom (11) has a lower dynamic pressure than that of the free stream.

REFERENCES:
patent: 1613348 (1927-01-01), Falkenthal
patent: 4231536 (1980-11-01), Ishimitsu et al.
patent: 6394397 (2002-05-01), Ngo et al.
patent: 7097139 (2006-08-01), Schroeder
patent: 7404530 (2008-07-01), Saggio et al.
patent: 2005/0236520 (2005-10-01), Wukowitz
patent: 2006/0075694 (2006-04-01), Lin
patent: 2007/0084968 (2007-04-01), Thal et al.

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