U.S. patent number D951,137 [Application Number D/684,687] was granted by the patent office on 2022-05-10 for hybrid vertical takeoff and landing flying automobile.
The grantee listed for this patent is Andrew H B Zhou, Dylan T X Zhou, Tiger T G Zhou. Invention is credited to Andrew H B Zhou, Dylan T X Zhou, Tiger T G Zhou.
United States Patent |
D951,137 |
Zhou , et al. |
May 10, 2022 |
Hybrid vertical takeoff and landing flying automobile
Claims
CLAIM The ornamental design for a hybrid vertical takeoff and
landing flying automobile, as shown and described.
Inventors: |
Zhou; Dylan T X (Tiburon,
CA), Zhou; Andrew H B (San Gabriel, CA), Zhou; Tiger T
G (Tiburon, CA) |
Applicant: |
Name |
City |
State |
Country |
Type |
Zhou; Dylan T X
Zhou; Andrew H B
Zhou; Tiger T G |
Tiburon
San Gabriel
Tiburon |
CA
CA
CA |
US
US
US |
|
|
Appl.
No.: |
D/684,687 |
Filed: |
March 22, 2019 |
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Application
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Issue Date |
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15484177 |
Apr 11, 2017 |
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15061982 |
Apr 11, 2017 |
9619794 |
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14815988 |
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Current U.S.
Class: |
D12/4 |
Current International
Class: |
1213 |
Field of
Search: |
;D12/1-4,7-9,12,14-16.1,18,36,37,40,82,84-104,218,319-322,324,326-342,344
;D21/433,436,441,422,447,450,533,539,550,552,563,564,579-583 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Robinson; Cary M
Assistant Examiner: Mager; Adam C
Attorney, Agent or Firm: Khayet; Georgiy L.
Description
FIG. 1 is a top perspective view of a hybrid vertical takeoff and
landing flying automobile showing our new design;
FIG. 2 is a top perspective view of the hybrid vertical takeoff and
landing flying automobile with wings extended;
FIG. 3 is a top perspective view of the hybrid vertical takeoff and
landing flying automobile with four wheels on the ground and wings
extended;
FIG. 4 is a top perspective view of the hybrid vertical takeoff and
landing flying automobile with wings vertical;
FIG. 5 is a top perspective view of the hybrid vertical takeoff and
landing flying automobile with four wheels on the ground and wings
vertical;
FIG. 6 is a top perspective view of the hybrid vertical takeoff and
landing flying automobile with wings extended and parachute
launched;
FIG. 7 is a left side view of hybrid vertical takeoff and landing
flying automobile shown in FIG. 1;
FIG. 8 is a right side view thereof;
FIG. 9 is a top view thereof;
FIG. 10 is a bottom view thereof;
FIG. 11 is a back view thereof; and,
FIG. 12 is a front view thereof.
The broken lines shown in the drawings illustrate portions of the
hybrid vertical takeoff and landing flying automobile and forms no
part of the claimed design.
* * * * *