U.S. patent number D803,724 [Application Number D/578,694] was granted by the patent office on 2017-11-28 for amphibious unmanned vertical takeoff and landing aircraft.
The grantee listed for this patent is Dylan T X Zhou. Invention is credited to Dylan T X Zhou.
United States Patent |
D803,724 |
Zhou |
November 28, 2017 |
Amphibious unmanned vertical takeoff and landing aircraft
Claims
CLAIM We claim the ornamental design for an amphibious unmanned
vertical takeoff and landing aircraft, as shown and described.
Inventors: |
Zhou; Dylan T X (Tiburon,
CA) |
Applicant: |
Name |
City |
State |
Country |
Type |
Zhou; Dylan T X |
Tiburon |
CA |
US |
|
|
Appl.
No.: |
D/578,694 |
Filed: |
September 23, 2016 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
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29572722 |
Jul 29, 2016 |
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29567712 |
Jun 10, 2016 |
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14940379 |
Nov 13, 2015 |
9493235 |
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14034509 |
Sep 23, 2013 |
9510277 |
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Current U.S.
Class: |
D12/16.1;
D12/324; D12/326 |
Current International
Class: |
1207 |
Field of
Search: |
;D12/16.1,319,323-345,82,88,90,91,3,4,2
;D21/436,438,439,440,441,447,448,449,450,452,453,454,455,424,533,833 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Spear; Robert M.
Assistant Examiner: Cash; Marissa J
Attorney, Agent or Firm: Nielsen; Steven A.
www.NielsenPatents.com
Description
FIG. 1 is a top perspective view of an amphibious unmanned vertical
takeoff and landing aircraft with wings folded upward;
FIG. 2 is a top perspective view thereof, shown in an alternate
configuration of use, with wings folded down;
FIG. 3 is a top perspective view thereof, with wings extended;
FIG. 4 is a top perspective view thereof, with extended wings
folded upward;
FIG. 5 is a right side view thereof;
FIG. 6 is a left side view thereof,
FIG. 7 is a front view thereof;
FIG. 8 is a back view thereof;
FIG. 9 is a top view thereof;
FIG. 10 is a bottom view thereof;
FIG. 11 is a perspective view of an amphibious unmanned vertical
takeoff and landing aircraft in FIG. 3, shown in an alternate
configuration of use, with onboard parachutes deployed;
FIG. 12 is a top perspective view of the amphibious unmanned
vertical takeoff and landing aircraft in FIG. 2, shown in an
alternate configuration of use, with rotor blades folded;
FIG. 13 is a top perspective view thereof, shown in an alternate
configuration of use, with rotor blades and wings folded;
FIG. 14 is a top perspective view, shown in an alternate
configuration of use, with engines tilted partially upward;
and,
FIG. 15 is a top perspective view thereof, with engines tilted
fully vertical.
The broken lines of FIG. 12 illustrate environmental factors only
and form no part of the claimed design.
* * * * *
References