In-flight refueling system, damping device and method for...

Details In-flight refueling system, damping device and method for... In-flight refueling system, damping device and method for...

2006-08-29

2006-08-29

Dinh, Tien (Department: 3644)

Aeronautics and astronautics

Aircraft structure

Fuel supply

Reexamination Certificate

active

07097139

ABSTRACT:
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.

REFERENCES:
patent: 2793828 (1957-05-01), Rohtert
patent: 2949265 (1960-08-01), Person
patent: 3011737 (1961-12-01), Morrow
patent: 4129270 (1978-12-01), Robinson et al.
patent: 5427333 (1995-06-01), Kirkland
patent: 6604711 (2003-08-01), Stevens et al.

Affiliated with

Also associated with

Rating

In-flight refueling system, damping device and method for... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with In-flight refueling system, damping device and method for..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and In-flight refueling system, damping device and method for... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-3633979