Vertical take-off and landing aircraft

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Description

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.

Claims

The ornamental design for a vertical take-off and landing aircraft, as shown and described.

Referenced Cited
U.S. Patent Documents
9120560 September 1, 2015 Armer
10081436 September 25, 2018 Tian
D832154 October 30, 2018 Tian
D843306 March 19, 2019 Tzarnotzky
D850357 June 4, 2019 Cummings
10322814 June 18, 2019 Tian
D864084 October 22, 2019 Clark
D868668 December 3, 2019 Parvizian
D872681 January 14, 2020 Tzarnotzky
D875022 February 11, 2020 Cummings
20160236774 August 18, 2016 Niedzballa
20170300066 October 19, 2017 Douglas
Patent History
Patent number: D947748
Type: Grant
Filed: May 24, 2019
Date of Patent: Apr 5, 2022
Assignee: ISRAEL AEROSPACE INDUSTRIES LTD. (Lod)
Inventors: Sharon Levy (Bat-Hefer), Ron Bublitsky (Haifa), Ehud Baharav (Ramat Gan)
Primary Examiner: John A Voytek
Application Number: 29/692,400
Classifications
Current U.S. Class: Vertical Takeoff Type (D12/326)