Fluid loading system

Aeronautics and astronautics – Aircraft structure – Material discharging and diffusing

Reexamination Certificate

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C169S053000, C239S171000

Reexamination Certificate

active

06874734

ABSTRACT:
A pump system for loading fluid into a tank onboard a translating aircraft includes a substantially rigid tube member having a diving device on the distal end of the tube member. A strut structure may also be provided on a front face of the tube member. In use, the tube member is directed rearward relative to the translating aircraft so that splashing of fluid onto the underside of the aircraft is substantially avoided.

REFERENCES:
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patent: 3714987 (1973-02-01), Mattson
patent: 3759330 (1973-09-01), Rainey et al.
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patent: 4474350 (1984-10-01), Hawkshaw
patent: 5451016 (1995-09-01), Foy et al.
patent: 5967462 (1999-10-01), Foster et al.
patent: 6209593 (2001-04-01), Nichols, Sr.
patent: 2512775 (1981-09-01), None

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