Aircraft rinse pad panel
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FIG. 1 is a perspective view of the aircraft rinse pad panel of the present invention;
FIG. 2 is a top elevation view of the aircraft rinse pad panel of the present invention;
FIG. 3 is a front elevation view of the aircraft rinse pad panel of the present invention;
FIG. 4 is a rear elevation view of the aircraft rinse pad panel of the present invention;
FIG. 5 is a bottom plan view of the aircraft rinse pad panel of the present invention; and,
FIG. 6 is a right side elevation view of the aircraft rinse pad panel of the present invention, with the left side elevation view a mirror image of the right side elevation view.
The broken line enclosure on the bottom of the panel in FIG. 5 and the corresponding broken line shown in FIGS. 1, 3, 4, and 6 show the limits of the claimed novel features on the bottom of the aircraft rinse pad panel, as Applicants do not claim to any feature on the bottom of the aircraft rinse pad panel within the bounds of such broken line enclosures.
Claims
The ornamental design for a aircraft rinse pad panel, as shown and described.
Type: Grant
Filed: Dec 3, 2004
Date of Patent: Oct 4, 2005
Assignee: LJC Technologies, LLC (Tyler, TX)
Inventors: Garrett Wade Jones (Lindale, TX), Robert Wayne Jones (Lindale, TX), Kazuto Otsuba (Longview, TX), Christopher Michael Vasiliotis (Lindale, TX)
Primary Examiner: Marcus A. Jackson
Attorney: Carstens & Cahoon, LLP
Application Number: 29/218,566
