The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.
The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.
Patent No.:
Date of Patent:
Jun. 22, 2021
Filed:
Sep. 30, 2015
Applicant:
Sikorsky Aircraft Corporation, Stratford, CT (US);
Inventors:
Assignee:
SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/10 (2006.01); F16F 15/02 (2006.01); B64C 27/00 (2006.01); B64C 27/14 (2006.01); B64C 1/00 (2006.01); B64C 7/00 (2006.01); B64C 13/18 (2006.01); B64C 13/50 (2006.01); B64C 19/00 (2006.01); B64C 27/12 (2006.01); B64C 27/32 (2006.01); B64C 27/33 (2006.01); B64C 27/473 (2006.01); B64C 27/48 (2006.01); B64C 27/51 (2006.01); B64C 27/52 (2006.01); B64C 27/54 (2006.01); B64C 27/78 (2006.01); B64C 27/80 (2006.01); B64C 27/82 (2006.01); B64D 39/00 (2006.01); B64D 39/06 (2006.01); B64D 45/02 (2006.01); F16H 37/02 (2006.01); G05D 1/00 (2006.01); G05D 1/02 (2020.01); B64C 27/16 (2006.01); B64C 13/04 (2006.01); G05D 1/08 (2006.01); B64C 27/57 (2006.01); B64D 35/06 (2006.01); B64C 27/467 (2006.01); F02C 9/28 (2006.01); F16D 13/52 (2006.01); F16D 13/72 (2006.01); F16D 13/74 (2006.01); B64C 27/08 (2006.01);
U.S. Cl.
CPC ...
B64C 27/10 (2013.01); B64C 1/0009 (2013.01); B64C 7/00 (2013.01); B64C 13/04 (2013.01); B64C 13/18 (2013.01); B64C 13/50 (2013.01); B64C 13/503 (2013.01); B64C 19/00 (2013.01); B64C 27/001 (2013.01); B64C 27/006 (2013.01); B64C 27/008 (2013.01); B64C 27/12 (2013.01); B64C 27/14 (2013.01); B64C 27/16 (2013.01); B64C 27/32 (2013.01); B64C 27/322 (2013.01); B64C 27/33 (2013.01); B64C 27/467 (2013.01); B64C 27/473 (2013.01); B64C 27/48 (2013.01); B64C 27/51 (2013.01); B64C 27/52 (2013.01); B64C 27/54 (2013.01); B64C 27/57 (2013.01); B64C 27/78 (2013.01); B64C 27/80 (2013.01); B64C 27/82 (2013.01); B64D 35/06 (2013.01); B64D 39/00 (2013.01); B64D 39/06 (2013.01); B64D 45/02 (2013.01); F16F 15/02 (2013.01); F16H 37/02 (2013.01); G05D 1/0077 (2013.01); G05D 1/0202 (2013.01); G05D 1/0816 (2013.01); G05D 1/0858 (2013.01); B64C 27/08 (2013.01); B64C 2027/004 (2013.01); B64C 2027/8209 (2013.01); B64C 2027/8227 (2013.01); B64C 2027/8236 (2013.01); B64C 2027/8263 (2013.01); B64C 2027/8272 (2013.01); B64C 2027/8281 (2013.01); B64C 2201/024 (2013.01); F02C 9/28 (2013.01); F05D 2220/329 (2013.01); F05D 2270/021 (2013.01); F16D 13/52 (2013.01); F16D 13/72 (2013.01); F16D 13/74 (2013.01); G05D 1/0204 (2013.01); G05D 1/08 (2013.01);
Abstract
An aircraft is provided including an airframe, an extending tail, and a counter rotating, coaxial main rotor assembly including an upper rotor assembly and a lower rotor assembly. A translational thrust system positioned at the extending tail, the translational thrust system providing translational thrust to the airframe. A cockpit in the airframe, the cockpit including two seats and a single collective control input positioned between the two seats.