Patent
   D947748
Priority
Nov 25 2018
Filed
May 24 2019
Issued
Apr 05 2022
Expiry
Apr 05 2037
Assg.orig
Entity
unknown
14
12
n/a
The ornamental design for a vertical take-off and landing aircraft, as shown and described.

FIG. 1 is a front perspective view of a first embodiment for a new design for a vertical take-off and landing aircraft, with engines at vertical position;

FIG. 2 is a top view of the design seen in FIG. 1, with engines at vertical position;

FIG. 3 is a front view of the design seen in FIG. 1, with engines at vertical position;

FIG. 4 is a rear view of the design seen in FIG. 1, with engines at vertical position;

FIG. 5 is a right side view of the design seen in FIG. 1, with engines at vertical position;

FIG. 6 is a left side view of the design seen in FIG. 1, with engines at vertical position;

FIG. 7 is a bottom view of the design seen in FIG. 1, with engines at vertical position;

FIG. 8 is a bottom and rear perspective view of the design seen in FIG. 1, with engines at vertical position;

FIG. 9 is a bottom and rear perspective view of the design seen in FIG. 1, with engines at horizontal position;

FIG. 10 is a left and front perspective view of the design seen in FIG. 1, with engines at horizontal position;

FIG. 11 is a right and front perspective view of the design seen in FIG. 1, with engines at horizontal position;

FIG. 12 is a front perspective view of a second embodiment for a new design for a vertical take-off and landing aircraft with engines at vertical position;

FIG. 13 is a top view of the design seen in FIG. 12, with engines at vertical position;

FIG. 14 is a front view of the design seen in FIG. 12, with engines at vertical position;

FIG. 15 is a right side view of the design seen in FIG. 12, with engines at vertical position;

FIG. 16 is a rear view of the design seen in FIG. 12, with engines at vertical position;

FIG. 17 is a left side view of the design seen in FIG. 12, with engines at vertical position;

FIG. 18 is a top view of the design seen in FIG. 12, with engines at vertical position;

FIG. 19 is a bottom view of the design seen in FIG. 12, with engines at vertical position;

FIG. 20 is a bottom and rear perspective view of the design seen in FIG. 12, with engines at vertical position;

FIG. 21 is a bottom and left perspective view of the design seen in FIG. 12, with engines at horizontal position; and,

FIG. 22 is a top and rear perspective view of the design seen in FIG. 12, with engines at horizontal position.

The part of the photograph shown in a coarse dot pattern, along with the broken-line perimeter illustrates a portion of the vertical take-off and landing aircraft vehicle that forms no part of the claimed design.

Levy, Sharon, Bublitsky, Ron, Baharav, Ehud

Patent Priority Assignee Title
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Executed onAssignorAssigneeConveyanceFrameReelDoc
May 24 2019ISRAEL AEROSPACE INDUSTRIES LTD.(assignment on the face of the patent)
Aug 11 2019LEVY, SHARONISRAEL AEROSPACE INDUSTRIES LTDASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0500450298 pdf
Aug 11 2019BUBLITSKY, RONISRAEL AEROSPACE INDUSTRIES LTDASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0500450298 pdf
Aug 11 2019BAHARAV, EHUDISRAEL AEROSPACE INDUSTRIES LTDASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0500450298 pdf
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