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. 07, 2022

Filed:

Dec. 28, 2020
Applicant:

Rotary Research Group Llc, Joplin, MO (US);

Inventors:

P. Tyson Garvin, Joplin, MO (US);

Timothy C. Stamps, Carl Junction, MO (US);

Assignee:

Rotary Research Group LLC, Joplin, MO (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02B 3/00 (2006.01); F02B 3/08 (2006.01); F02B 53/02 (2006.01); F02B 55/02 (2006.01); F02B 55/08 (2006.01); F02B 53/00 (2006.01);
U.S. Cl.
CPC ...
F02B 3/08 (2013.01); F02B 53/02 (2013.01); F02B 55/02 (2013.01); F02B 55/08 (2013.01); F02B 2053/005 (2013.01);
Abstract

A rotary engine that starts and operates on compression-ignition of a heavy fuel without a secondary ignition source. The rotary engine includes a rotor housing that forms an epitrochoidal-shaped chamber having linear side portions extending between rounded end portions. A three-flanked rotor is disposed in the chamber to rotate and operate in a manner similar to that of a common Wankel-style rotary engine. The rotor and chamber are configured to provide a compression ratio sufficient to produce compression-ignition of a heavy fuel. The rotor includes apex seal and side seal mounting blocks formed from hardened materials and that are simply removable from the rotor for replacing apex and side seals. The apex seals may include multiple non-parallel seal members at each apex and the apex seals and the side seals may overlap or intersect a corner seal to increase sealing under high compression loads produced by the rotor/chamber configuration.


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