U.S. patent number D796,414 [Application Number D/564,597] was granted by the patent office on 2017-09-05 for sinusoidal circular wing and spokes for a closed wing aircraft.
This patent grant is currently assigned to BELL HELICOPTER TEXTRON INC.. The grantee listed for this patent is Bell Helicopter Textron Inc.. Invention is credited to Carlos Alexander Fenny, Rohn Lee Olson, Andrew James Zahasky.
United States Patent |
D796,414 |
Fenny , et al. |
September 5, 2017 |
Sinusoidal circular wing and spokes for a closed wing aircraft
Claims
CLAIM The ornamental design for a sinusoidal circular wing and
spokes for a closed wing aircraft, as shown and described.
Inventors: |
Fenny; Carlos Alexander (Fort
Worth, TX), Olson; Rohn Lee (Hurst, TX), Zahasky; Andrew
James (North Richland Hills, TX) |
Applicant: |
Name |
City |
State |
Country |
Type |
Bell Helicopter Textron Inc. |
Fort Worth |
TX |
US |
|
|
Assignee: |
BELL HELICOPTER TEXTRON INC.
(Fort Worth, TX)
|
Appl.
No.: |
D/564,597 |
Filed: |
May 13, 2016 |
Current U.S.
Class: |
D12/328; D12/345;
D21/441 |
Current International
Class: |
1207 |
Field of
Search: |
;D12/16.1,319-324,326-345
;D21/436,441,443,444,446,447,448,449,450,451,452,453 |
References Cited
[Referenced By]
U.S. Patent Documents
Other References
Volocopter, Misc. Website images, VC400
http://www.volocopter.com/index.php, 13 pp. Oct. 29, 2014. cited by
applicant.
|
Primary Examiner: Spear; Robert M
Assistant Examiner: Cash; Marissa J
Attorney, Agent or Firm: Chalker; Daniel J. Flores; Edwin S.
Chalker Flores, LLP
Description
FIG. 1 is a perspective view of a sinusoidal circular wing and
spokes for a closed wing aircraft in which all the rotors are
deployed;
FIG. 2 is a front elevation view thereof;
FIG. 3 is a rear elevation view thereof;
FIG. 4 is a right side elevation view thereof;
FIG. 5 is a left side elevation view thereof;
FIG. 6 is a top plan view thereof;
FIG. 7 is a bottom plan view thereof;
FIG. 8 is a perspective view of a sinusoidal circular wing for a
closed wing aircraft in which the rotors on the spokes are deployed
and the rotors on the ring wing are folded forward;
FIG. 9 is a front elevation view thereof;
FIG. 10 is a rear elevation view thereof;
FIG. 11 is a right side elevation view thereof;
FIG. 12 is a left side elevation view thereof;
FIG. 13 is a top plan view thereof; and,
FIG. 14 is a bottom plan view thereof.
The fuselage, rotors and landing gear depicted by broken lines in
the drawings have been shown for the purpose of illustrating
environment that forms no part of the claimed design.
* * * * *
References