Patent · US Active

Planetary rotary engine

US8356585B2 · kind B2 · utility

17Cited by
30References
26Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 16, 2009
Grant dateJan 22, 2013
Priority date
Expiry dateApr 2, 2031

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T10/12
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A planetary engine includes a charge compression system for compressing a charge of air and/or an air and fuel mixture that is precompressed by rotation of the rotors and supplied into a combustion chamber through a rotary valve that may be actively adjusted during operation of the engine to vary the intake valve opening size and/or timing. Exhaust valves may likewise be actively adjustable rotary valves for further engine control. A compression insert mounted between the end wall assemblies absorbs combustion forces and provides rigidity to the engine, as well as occupies all or nearly all of the volume between the rotors at the minimum volume of the combustion chamber to improve the compression ratio of the engine.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.