U.S. patent number D843,304 [Application Number 35/503,550] was granted by the patent office on 2019-03-19 for tail section of flying car.
This patent grant is currently assigned to AEROMOBIL R&D, S. R. O.. The grantee listed for this patent is AEROMOBIL R&D, S. R. O.. Invention is credited to Adam Danko, Kenneth Douglas Alexander MacAndrew, Alan Roach, William Simon Rooms, Tomas Urik.
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United States Patent |
D843,304 |
MacAndrew , et al. |
March 19, 2019 |
Tail section of flying car
Claims
CLAIM The ornamental design for a tail section of flying car, as
shown and described.
Inventors: |
MacAndrew; Kenneth Douglas
Alexander (Bystrica, SK), Rooms; William Simon
(Bratislava, SK), Urik; Tomas (Sastin-Straze,
SK), Danko; Adam (Stupava, SK), Roach;
Alan (Oslo, NO) |
Applicant: |
Name |
City |
State |
Country |
Type |
AEROMOBIL R&D, S. R. O. |
Mestska Cast Podunajske Biskupice |
N/A |
SK |
|
|
Assignee: |
AEROMOBIL R&D, S. R. O.
(Mestska cast Podunajske Biskupice, SK)
|
Appl.
No.: |
35/503,550 |
Filed: |
April 25, 2017 |
International Registration
Int'l Reg. No. |
Int'l Reg. Date |
Int'l Reg.
Publication Date |
Hague Int'l
Filing Date |
DM/097344 |
Apr 25, 2017 |
Aug 25, 2017 |
Apr 25, 2017 |
Foreign Application Priority Data
|
|
|
|
|
Oct 25, 2016 [EM] |
|
|
003434125 |
|
Current U.S.
Class: |
D12/319 |
Current International
Class: |
1207 |
Field of
Search: |
;D12/16.1,319-322,324-327,330,333-345
;D21/430,436,437,441-449,451 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Ly; Darlington
Attorney, Agent or Firm: Finnegan, Henderson, Farabow,
Garrett & Dunner LLP
Description
1.1 is a top, rear, and left side perspective view of a tail
section of a flying car showing our new design;
1.2 is a bottom plan view thereof;
1.3 is a left side elevation view thereof;
1.4 is a top, rear, and left side perspective view thereof wherein
the propeller blades are in a folded configuration;
1.5 is a bottom plan view thereof wherein the propeller blades are
in a folded configuration; and
1.6 is a left side elevation view thereof wherein the propeller
blades are in a folded configuration.
* * * * *