Inventor · disambiguated record
Kattalaicheri Srinivasan Venkataramani
Also filed as: VENKATARAMANI KATTALAICHERI S · VENKATARAMANI KATTALAICHERI SR · VENKATARAMANI KATTALAICHERI SRINIVASAN
22 granted patents·4 pending applications·574 citations·filing 1988–2007
96Inventor score
Top patents by PatentIndex Score
26 records- 0196US6990797B2Methods and apparatus for operating gas turbine enginesGEN ELECTRIC·Filed 2003·Granted Jan 31, 2006·85 cites·18 claims
- 0295US5257500AAircraft engine ignition systemGEN ELECTRIC·Filed 1992·Granted Nov 2, 1993·49 cites·10 claims
- 0394US8015788B2Heat transfer system for turbine engine using heat pipesGEN ELECTRIC·Filed 2006·Granted Sep 13, 2011·45 cites·19 claims
- 0493US7900438B2Heat transfer system and method for turbine engine using heat pipesGEN ELECTRIC·Filed 2006·Granted Mar 8, 2011·47 cites·30 claims
- 0589US7823374B2Heat transfer system and method for turbine engine using heat pipesGEN ELECTRIC·Filed 2006·Granted Nov 2, 2010·33 cites·13 claims
- 0689US5367871AAircraft engine ignition systemGEN ELECTRIC·Filed 1993·Granted Nov 29, 1994·29 cites·5 claims
- 0788US7900437B2Heat transfer system and method for turbine engine using heat pipesGEN ELECTRIC·Filed 2006·Granted Mar 8, 2011·30 cites·24 claims
- 0884US4903480AHypersonic scramjet engine fuel injectorGEN ELECTRIC·Filed 1988·Granted Feb 27, 1990·38 cites·6 claims
- 0982US7845159B2Heat pipe-based cooling apparatus and method for turbine engineGEN ELECTRIC·Filed 2006·Granted Dec 7, 2010·21 cites·20 claims
- 1075US7096674B2High thrust gas turbine engine with improved core systemGEN ELECTRIC·Filed 2004·Granted Aug 29, 2006·33 cites·28 claims
- 1174US6928804B2Pulse detonation system for a gas turbine engineGEN ELECTRIC·Filed 2003·Granted Aug 16, 2005·23 cites·30 claims
- 1273US7739873B2Gas turbine engine combustor hot streak controlGEN ELECTRIC·Filed 2005·Granted Jun 22, 2010·7 cites·13 claims
- 1368US6931858B2Rotating pulse detonation system for a gas turbine engineGEN ELECTRIC·Filed 2003·Granted Aug 23, 2005·24 cites·35 claims
- 1468US6904750B2Integral pulse detonation system for a gas turbine engineGEN ELECTRIC·Filed 2003·Granted Jun 14, 2005·18 cites·43 claims
- 1564US4986068AHypersonic scramjet engine fuel injectorGEN ELECTRIC·Filed 1989·Granted Jan 22, 1991·22 cites·5 claims
- 1659US7328570B2Pulse detonation system for a gas turbine engine having multiple spoolsGEN ELECTRIC·Filed 2004·Granted Feb 12, 2008·14 cites·21 claims
- 1758US7124573B2Rotary pulse detonation system with aerodynamic detonation passages for use in a gas turbine engineGEN ELECTRIC·Filed 2004·Granted Oct 24, 2006·12 cites·31 claims
- 1855US6889505B2Pulse detonation system for a gas turbine engineGEN ELECTRIC·Filed 2003·Granted May 10, 2005·18 cites·46 claims
- 1948US2006216476A1Articles having a surface with low wettability and method of makingGEN ELECTRIC·Filed 2005·Application pending·0 cites
- 2045US7093446B2Gas turbine engine having improved core systemGEN ELECTRIC·Filed 2004·Granted Aug 22, 2006·7 cites·27 claims
- 2144US7200538B2Methods and apparatus for modeling gas turbine enginesGEN ELECTRIC·Filed 2003·Granted Apr 3, 2007·7 cites·18 claims
- 2244US2008229751A1Cooling system for gas turbine engine having improved core systemGEN ELECTRIC·Filed 2007·Application pending·0 cites
- 2342US4951463AHypersonic scramjet engine fuel injectorGEN ELECTRIC·Filed 1989·Granted Aug 28, 1990·9 cites·4 claims
- 2438US2006053801A1Cooling system for gas turbine engine having improved core systemORLANDO ROBERT J·Filed 2004·Application pending·0 cites
- 2538US2007214795A1Continuous real time EGT margin controlCOOKER PAUL·Filed 2006·Application pending·0 cites
- 2631US4969327AHypersonic scramjet engine fuel injectorGEN ELECTRIC·Filed 1989·Granted Nov 13, 1990·3 cites·6 claims
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