Control panel for aircraft or the like

Weitz , et al. October 20, 1

Patent Grant D261387

U.S. patent number D261,387 [Application Number 06/031,805] was granted by the patent office on 1981-10-20 for control panel for aircraft or the like. This patent grant is currently assigned to Instrument Systems Corporation. Invention is credited to Diego M. Cacciatore, Harry Weitz.


United States Patent D261,387
Weitz ,   et al. October 20, 1981

Control panel for aircraft or the like

Claims

The ornamental design for a control panel for aircraft or the like, as shown and described.
Inventors: Weitz; Harry (New Hyde Park, NY), Cacciatore; Diego M. (Farmingdale, NY)
Assignee: Instrument Systems Corporation (Jericho, NY)
Appl. No.: 06/031,805
Filed: April 20, 1979

Current U.S. Class: D12/192; D13/164
Current International Class: D1216
Field of Search: ;D12/192,195 ;D13/12,32,40,41 ;200/5R,293 ;361/331,332,356,358,380,390

References Cited [Referenced By]

U.S. Patent Documents
D213144 January 1969 Kraus
D248980 August 1978 Friedman
D251727 May 1979 Erlacher et al.
Primary Examiner: Caun; Peter M.
Attorney, Agent or Firm: Blum, Kaplan, Friedman, Silberman & Beran

Description



FIG. 1 is a top plan view of the control panel for aircraft or the like showing our _new design;

FIG. 2 is a front elevational view of the control panel for aircraft or the like _of FIG. 1;

FIG. 3 is a right side elevational view of the control _panel for aircraft or the like of FIG. 1;

FIG. 4 is a rear elevational view of the control panel for aircraft or the like of FIG. 1;

FIG. 5 is a left side elevational view of the control panel for aircraft or the like _of FIG. 1;

FIG. 6 is a bottom plan view of the control panel for aircraft or the like of _FIG. 1;

FIG. 7 is a top plan view of a second embodiment of the _control panel for aircraft or the like showing our new design;

FIG. 8 is a front elevational view of the control panel for aircraft or the like _of FIG. 7, the side and rear elevational views of the embodiment _of FIG. 7 being identical to the embodiments of FIGS. 1-6;

FIG. 9 is a top plan view of a third embodiment of the _control panel for aircraft or the like showing our new design;

FIG. 10 is a front elevational view of the control panel for aircraft or the like _of FIG. 9;

FIG. 11 is a right side elevational view of the control _panel for aircraft or the like of FIG. 9;

FIG. 12 is a rear elevational view of the control panel for aircraft or the like _of FIG. 9; _

FIG. 13 is a left side elevational view of the control _panel for aircraft or the like of FIG. 9;

FIG. 14 is a bottom plan view of the control panel for aircraft or the like of _FIG. 9;

FIG. 15 is a fourth embodiment of the control panel for aircraft or the like showing _our new design;

FIG. 16 is a front elevational view of the control panel for aircraft or the like _of FIG. 15, the side, rear and bottom views thereof being _identical to the embodiment of FIGS. 9-14.

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