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:
Dec. 01, 2020

Filed:

Aug. 09, 2019
Applicant:

Enfield Engine Company, Llc, Enfield, NH (US);

Inventors:

Nicholas A. Sanders, Enfield, NH (US);

Ryan Thomas Kiley Sanders, Enfield, NH (US);

Assignee:

Enfield Engine Company, LLC, Enfield, NH (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F16H 19/02 (2006.01); F04B 9/04 (2006.01); F02B 75/20 (2006.01); F04B 53/16 (2006.01); F04B 53/14 (2006.01); F04B 35/01 (2006.01); F02B 75/04 (2006.01); F02B 75/40 (2006.01); F02B 75/32 (2006.01); F04B 9/02 (2006.01); F01B 9/04 (2006.01); F04B 19/22 (2006.01); F16C 3/06 (2006.01);
U.S. Cl.
CPC ...
F16H 19/02 (2013.01); F01B 9/04 (2013.01); F02B 75/042 (2013.01); F02B 75/20 (2013.01); F02B 75/32 (2013.01); F02B 75/40 (2013.01); F04B 9/02 (2013.01); F04B 9/045 (2013.01); F04B 19/22 (2013.01); F04B 35/01 (2013.01); F04B 53/14 (2013.01); F04B 53/16 (2013.01); F01B 9/047 (2013.01); F16C 3/06 (2013.01);
Abstract

In some aspects, reciprocating engines can include a first reciprocating mechanism that includes an axially translating y-axis component configured to reciprocate substantially along a y-axis with a reciprocating motion of a piston assembly relative to a base to which the y-axis component is slidingly attached. The first reciprocating mechanism can include an x-axis component slidingly coupled to and translating with the y-axis component along the y-axis, the x-axis component being: i) configured to reciprocate substantially perpendicularly to the y-axis relative to the y-axis component, ii) comprising an orbital output component, and iii) comprising an orbital linking component disposed substantially concentric with the orbital output component. The first reciprocating mechanism can include a stationary output component and a stationary linking component that are substantially concentric and disposed in a direction that is substantially perpendicular to the x-y plane.


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