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.

Date of Patent:
Jun. 16, 2020

Filed:

Mar. 06, 2018
Applicant:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Inventors:

Levi Bilbrey, Fort Worth, TX (US);

Jeremy Robert Chavez, Colleyville, TX (US);

Joshua Edler, Colleyville, TX (US);

James R. Williamson, Southlake, TX (US);

Joseph Scott Drennan, Dallas, TX (US);

Doug Fidler, Keller, TX (US);

Rares Halmagean, McKinney, TX (US);

Assignee:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64D 43/00 (2006.01); A42B 3/30 (2006.01); G06F 3/01 (2006.01); G01C 23/00 (2006.01); G08G 5/00 (2006.01); B64C 13/18 (2006.01); B64C 13/22 (2006.01); A42B 3/04 (2006.01); A42B 3/22 (2006.01); G06T 19/00 (2011.01); G02B 27/01 (2006.01); B64D 11/06 (2006.01); B64C 13/04 (2006.01); B64C 1/06 (2006.01); B64C 1/18 (2006.01); B64C 1/40 (2006.01); B64C 13/10 (2006.01); B64D 11/00 (2006.01); G06F 3/044 (2006.01);
U.S. Cl.
CPC ...
B64D 43/00 (2013.01); A42B 3/042 (2013.01); A42B 3/0433 (2013.01); A42B 3/228 (2013.01); A42B 3/30 (2013.01); B64C 1/066 (2013.01); B64C 1/18 (2013.01); B64C 1/40 (2013.01); B64C 13/042 (2018.01); B64C 13/044 (2018.01); B64C 13/18 (2013.01); B64C 13/22 (2013.01); B64D 11/0626 (2014.12); B64D 11/0647 (2014.12); B64D 11/0689 (2013.01); G01C 23/00 (2013.01); G01C 23/005 (2013.01); G02B 27/017 (2013.01); G06F 3/012 (2013.01); G06F 3/017 (2013.01); G06T 19/006 (2013.01); G08G 5/0004 (2013.01); G08G 5/0017 (2013.01); G08G 5/0021 (2013.01); G08G 5/0039 (2013.01); G08G 5/0047 (2013.01); G08G 5/0091 (2013.01); B64C 13/10 (2013.01); B64D 11/0015 (2013.01); B64D 11/0641 (2014.12); B64D 11/0646 (2014.12); B64D 2011/0046 (2013.01); G06F 3/044 (2013.01);
Abstract

The present invention achieves technical advantages as a pilot and passenger seating. An aircraft employs a pilot seat, comprising a contoured structure having ergonomically formed and padded surfaces, with left and right arm supports that include an articulated control knob, movable in three rectangular axes and rotatable about a vertical axis to provide one or more aircraft steering functions for an aircraft, and a touch-sensitive control surface for controlling one or more power system components. A passenger seat, having a contoured structure, having ergonomically formed and padded surfaces, a headrest, a seat, a left support member, and a right support member are adapted to cradle a portion of a passenger's body to support the passenger during travel.


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