Sinusoidal circular wing and spokes for a closed wing aircraft

Fenny , et al. September 5, 2

Patent Grant D796414

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]

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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


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