Aircraft cockpit throttle console
da Silveira , et al. May 12, 2
U.S. patent number D592,126 [Application Number D/324,988] was granted by the patent office on 2009-05-12 for aircraft cockpit throttle console. This patent grant is currently assigned to Embraer - Empresa Brasileira de Aeronautica S.A.. Invention is credited to Eduardo Leandro da Silveira, Mozart Marques Louzada Junior.
| United States Patent | D592,126 |
| da Silveira , et al. | May 12, 2009 |
Aircraft cockpit throttle console
Claims
CLAIM The ornamental design for an "aircraft cockpit throttle console," as shown and described.
| Inventors: | da Silveira; Eduardo Leandro (Sao Jose dos Campos - SP, BR), Louzada Junior; Mozart Marques (Sao Jose dos Campos - SP, BR) |
|---|---|
| Assignee: | Embraer - Empresa Brasileira de
Aeronautica S.A. (Sao Jose Dos Campos - SP, BR) |
| Appl. No.: | D/324,988 |
| Filed: | September 24, 2008 |
| Current U.S. Class: | D12/415; D12/345 |
| Current International Class: | 1216 |
| Field of Search: | ;D12/192,415,179,345,421,423-425 ;180/190 ;280/750-752 ;296/190.01-190.09,70 ;224/401,212 ;D10/46,98,102-103 ;220/DIG.2 ;244/118.5,129.1 ;340/945,971,975,675 ;307/101,91 |
References Cited [Referenced By]
U.S. Patent Documents
| D273150 | March 1984 | Benson |
| D385847 | November 1997 | Ma et al. |
| D434365 | November 2000 | Herer et al. |
| D443246 | June 2001 | Smith |
| D553554 | October 2007 | Figueiredo |
| D556107 | November 2007 | Figueiredo |
| D563300 | March 2008 | Nishimura et al. |
| D575212 | August 2008 | Tsay et al. |
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. 29/324,987 entitled "Aircraft Control Panel" and filed even date herewith, which application is expressly incorporated hereinto by reference.
FIG. 1 is a top left side perspective view of an aircraft cockpit throttle console which embodies my new and original design therefore;
FIG. 2 is a front elevation view thereof, the rear elevation view being unornamented;
FIG. 3 is a top plan view thereof, the bottom plan view being unornamented, wherein the broken lines in FIG. 3 represent console components, such as switches, knobs, annunciators, handles and the like, which are in the environment of the claimed design, but which do not form part of the claimed design; and,
FIG. 4 is a right side elevation view thereof, the left side elevation view being essentially a mirror image thereof.
The aircraft cockpit throttle console is shown on an enlarged scale in FIGS. 2 4.
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