Aircraft rinse pad panel

Information

  • Patent Grant
  • D510312
  • Patent Number
    D510,312
  • Date Filed
    Friday, December 3, 2004
    21 years ago
  • Date Issued
    Tuesday, October 4, 2005
    20 years ago
  • US Classifications
    Field of Search
    • US
    • D12 319-345
    • 244 121000
    • 244 129400
  • International Classifications
    • 1207
    • Term of Grant
      14Years
Abstract
Description

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.
US Referenced Citations (2)
Number Name Date Kind
D341122 Webb Nov 1993 S
D455705 Granzeier et al. Apr 2002 S