USD510312S1 - Aircraft rinse pad panel - Google Patents
Aircraft rinse pad panel Download PDFInfo
- Publication number
- USD510312S1 USD510312S1 US29/218,566 US21856604F USD510312S US D510312 S1 USD510312 S1 US D510312S1 US 21856604 F US21856604 F US 21856604F US D510312 S USD510312 S US D510312S
- Authority
- US
- United States
- Prior art keywords
- pad panel
- rinse pad
- aircraft rinse
- aircraft
- panel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
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 (1)
- The ornamental design for a aircraft rinse pad panel, as shown and described.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US29/218,566 USD510312S1 (en) | 2004-12-03 | 2004-12-03 | Aircraft rinse pad panel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US29/218,566 USD510312S1 (en) | 2004-12-03 | 2004-12-03 | Aircraft rinse pad panel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| USD510312S1 true USD510312S1 (en) | 2005-10-04 |
Family
ID=35005386
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US29/218,566 Expired - Lifetime USD510312S1 (en) | 2004-12-03 | 2004-12-03 | Aircraft rinse pad panel |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | USD510312S1 (en) |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USD341122S (en) * | 1991-11-04 | 1993-11-09 | Texstar, Inc. | Pressure seal for aircraft canopy |
| USD455705S1 (en) * | 2000-06-02 | 2002-04-16 | Fairchild Dorier Gmbh | Surface configuration of a ceiling panel for an airplane |
-
2004
- 2004-12-03 US US29/218,566 patent/USD510312S1/en not_active Expired - Lifetime
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USD341122S (en) * | 1991-11-04 | 1993-11-09 | Texstar, Inc. | Pressure seal for aircraft canopy |
| USD455705S1 (en) * | 2000-06-02 | 2002-04-16 | Fairchild Dorier Gmbh | Surface configuration of a ceiling panel for an airplane |
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