Aircraft guidance subpanel
Ozay , et al. March 1, 2
U.S. patent number D750,545 [Application Number D/503,113] was granted by the patent office on 2016-03-01 for aircraft guidance subpanel. This patent grant is currently assigned to EMBRAER S.A.. The grantee listed for this patent is EMBRAER S.A.. Invention is credited to Fabiano Cypel, Rogerio Tadao Ozay, Guilherme Maximiliano Verhalen.
| United States Patent | D750,545 |
| Ozay , et al. | March 1, 2016 |
Aircraft guidance subpanel
Claims
CLAIM The ornamental design for an "aircraft guidance subpanel," as shown and described.
| Inventors: | Ozay; Rogerio Tadao (Sao Jose dos Campos-SP, BR), Cypel; Fabiano (Sao Jose dos Campos-SP, BR), Verhalen; Guilherme Maximiliano (Sao Jose dos Campos-SP, BR) | ||||||||||
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| Applicant: |
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| Assignee: | EMBRAER S.A. (Sao Jose dos
Campos--SP, BR) |
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| Appl. No.: | D/503,113 | ||||||||||
| Filed: | September 23, 2014 |
| Current U.S. Class: | D12/345 |
| Current International Class: | 1207 |
| Field of Search: | ;D6/336,384,653,654,665,657,663,672,573 ;D7/602,603,614 ;D12/319,323,325,336,345,192,423,415,416,179,180,182 ;D21/436,447,448,449,453 ;D14/125-134,307,336,371 |
References Cited [Referenced By]
U.S. Patent Documents
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| D202262 | September 1965 | Brunger |
| D276039 | October 1984 | Tanaka |
| D284751 | July 1986 | Soederberg |
| D384015 | September 1997 | Stenger |
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| D424002 | May 2000 | Leschke |
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| D457851 | May 2002 | Krongold |
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| D493397 | July 2004 | Tuzar |
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| 7928863 | April 2011 | Firra |
| 2003/0127557 | July 2003 | Anderson |
| 2010/0076628 | March 2010 | Boorman |
Assistant Examiner: Cash; Marissa J
Attorney, Agent or Firm: Nixon & Vanderhye P.C.
Description
This application may be deemed related to commonly owned copending U.S. Design patent application Ser. No. 29/503,111 entitled "Aircraft Control Panel" filed on Sep. 23, 2014, which copending application is expressly incorporated hereinto by reference.
FIG. 1 is a front environmental plan view of an aircraft guidance subpanel which embodies my new and original design therefore;
FIG. 2 is an enlarged front plan view of thereof; and,
FIG. 3 is a top left side perspective view thereof, the rear elevation view, left and right side elevation views, and top and bottom plan views being unornamented.
The broken lines in FIGS. 1-3 represent aircraft panel components in the environment of the claimed design, but which do not form part of the claimed design.
The chain line in FIGS. 1-3 represents an environmental boundary within which the claimed design is present.
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