Rotary engine with exhaust gas supplemental compounding
View Patent ↗A rotary engine which provides a supplemental phase of compression between a first phase of compression and a second phase of compression.
1. A method of supplemental compression for a rotary engine comprising:
communicating exhaust gases from a second stage rotor volume radially into a first stage rotor volume through a second transfer duct therebetween; and
forcing compressed air within a first transfer duct between said first stage rotor volume and said second stage rotor volume radially into said second stage rotor volume with said exhaust gases; and
communicating said exhaust gases from said second stage rotor volume through a port and forcing said compressed air between said first stage rotor volume and said second stage rotor volume through same port.
2. A method as recited in claim 1 , further comprising:
locating said port at a first stage rotor top-dead-center (TDC) position.
3. A method as recited in claim 1 , further comprising:
offsetting said port from a first stage rotor top-dead-center (TDC) position.
4. A method as recited in claim 1 , further comprising:
recirculating at least a portion of said exhaust gases from said second stage rotor volume within said second stage rotor volume.
5. A method as recited in claim 1 , further comprising:
delivering fuel to said second stage rotor volume along a passageway outside said first and second transfer ducts.
6. A rotary engine comprising:
a first rotor section which provides a first phase of compression;
a second rotor section in communication with said first rotor section, said second rotor section provides a second phase of compression, a combustion phase and a first phase of expansion, said second rotor section in communication with said first rotor section such that said first rotor section provides a second phase of expansion, an exhaust gas from said first phase of expansion provides a supplemental phase of compression between said first phase of compression and said second phase of compression; and
a first transfer duct which communicates compressed air from said first rotor section through a first rotor volume outlet port to said second rotor section and a second transfer duct which communicates exhaust gases from said second rotor section to said first rotor section through a first rotor volume inlet port, said first rotor volume outlet port and said first rotor volume inlet port are located to one side of a first stage rotor top-dead-center (TDC) position, wherein said first rotor volume outlet port and said first rotor volume inlet port form one port in communication with said second rotor section.
7. A rotary engine comprising:
a first rotor section which provides a first phase of compression;
a second rotor section in communication with said first rotor section, said second rotor section provides a second phase of compression, a combustion phase and a first phase of expansion, said second rotor section in communication with said first rotor section such that said first rotor section provides a second phase of expansion, an exhaust gas from said first phase of expansion provides a supplemental phase of compression between said first phase of compression and said second phase of compression; and
a first transfer duct to communicate compressed air between said first rotor section and said second rotor section, said first transfer duct includes a portion that extends radially outside a radial perimeter of said first rotor section;
a second transfer duct to communicate exhaust gases between said second rotor section and said first rotor section;
wherein said first transfer duct being in fluid communication with said second transfer duct via a port positioned on a periphery of said first rotor section.
8. The rotary engine as recited in claim 7 , wherein said supplemental phase of compression includes communication of the exhaust gas from said first phase of expansion to charge said first phase of compression.
9. The rotary engine as recited in claim 8 , wherein the exhaust gas from said first phase of expansion is not recirculated to said first phase of expansion.
10. The rotary engine as recited in claim 8 , wherein the exhaust gas from said first phase of expansion increases airflow in said second phase of compression.
11. The rotary engine as recited in claim 10 , wherein the exhaust gas from said first phase of expansion adds heat to said second phase of compression.
12. The rotary engine as recited in claim 10 , wherein the exhaust gas from said first phase of expansion is at least partially recirculated.
13. The rotary engine as recited in claim 7 , wherein said second transfer duct communicates exhaust gases from said second rotor section to said first rotor section through said port.
14. The rotary engine as recited in claim 7 , wherein said port is located to one side of a first stage rotor top-dead-center (TDC) position.
15. The rotary engine as recited in claim 14 , wherein said port is located on a rotationally downstream side of a first stage rotor top-dead-center (TDC) position.
16. The rotary engine as recited in claim 7 , wherein said first transfer duct communicates radially into said second rotor section.
17. The rotary engine as recited in claim 7 , including a fuel injector to deliver fuel, wherein said fuel injector is separate from said transfer duct.