Inventor · disambiguated record
Ashok K. Jain
Also filed as: JAIN ASHOK · JAIN ASHOK K · JAIN ASHOK KUMAR
24 granted patents·5 pending applications·283 citations·filing 2006–2025
96Inventor score
Top patents by PatentIndex Score
29 records- 0197US8282037B2Nacelle flow assemblyJAIN ASHOK K·Filed 2010·Granted Oct 9, 2012·38 cites·8 claims
- 0295US8209953B2Gas turbine engine system providing simulated boundary layer thickness increaseWINTER MICHAEL·Filed 2010·Granted Jul 3, 2012·18 cites·8 claims
- 0394US8402739B2Variable shape inlet section for a nacelle assembly of a gas turbine engineJAIN ASHOK K·Filed 2007·Granted Mar 26, 2013·28 cites·10 claims
- 0494US7870721B2Gas turbine engine providing simulated boundary layer thickness increaseUNITED TECHNOLOGIES CORP·Filed 2006·Granted Jan 18, 2011·46 cites·10 claims
- 0593US8596573B2Nacelle flow assemblyJAIN ASHOK K·Filed 2012·Granted Dec 3, 2013·17 cites·15 claims
- 0689US8408491B2Nacelle assembly having inlet airfoil for a gas turbine engineJAIN ASHOK K·Filed 2007·Granted Apr 2, 2013·26 cites·23 claims
- 0786US8205430B2Variable geometry nacelle assembly for a gas turbine engineJAIN ASHOK K·Filed 2007·Granted Jun 26, 2012·21 cites·17 claims
- 0883US10309315B2Variable area nozzle assisted gas turbine engine restartingUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jun 4, 2019·3 cites·18 claims
- 0981US11309994B2Highly parallel and scalable cyclic redundancy checkINFINERA CORP·Filed 2016·Granted Apr 19, 2022·4 cites·20 claims
- 1079US9228534B2Variable contour nacelle assembly for a gas turbine engineJAIN ASHOK K·Filed 2007·Granted Jan 5, 2016·10 cites·16 claims
- 1176US9004399B2Nacelle flow assemblyJAIN ASHOK K·Filed 2007·Granted Apr 14, 2015·6 cites·20 claims
- 1275US8727267B2Variable contraction ratio nacelle assembly for a gas turbine engineJAIN ASHOK K·Filed 2007·Granted May 20, 2014·11 cites·10 claims
- 1375US8657567B2Nacelle compartment plenum for bleed air flow delivery systemCLOFT THOMAS G·Filed 2007·Granted Feb 25, 2014·16 cites·16 claims
- 1467US8720182B2Integrated variable area nozzle and thrust reversing mechanismJAIN ASHOK K·Filed 2006·Granted May 13, 2014·8 cites·9 claims
- 1564US9479849B2OTU4 one level de-multiplexing spatial framer for G.709 optical transport networksINFINERA CORP·Filed 2015·Granted Oct 25, 2016·2 cites·20 claims
- 1663US9328666B2Variable area nozzle assisted gas turbine engine restartingJAIN ASHOK K·Filed 2006·Granted May 3, 2016·5 cites·4 claims
- 1762US8650854B2Bifurcation and aft vent used to vary fan nozzle exit areaMIGLIARO JR EDWARD F·Filed 2006·Granted Feb 18, 2014·7 cites·13 claims
- 1858US8137060B2Actuation of a turbofan engine bifurcation to change an effective nozzle exit areaWINTER MICHAEL·Filed 2006·Granted Mar 20, 2012·6 cites·10 claims
- 1957US8240979B2Gas turbine engine systems involving integrated fluid conduitsJAIN ASHOK K·Filed 2007·Granted Aug 14, 2012·4 cites·17 claims
- 2057US2025278918A1System and method for generating media presentation with zoom-in effectSAMSUNG ELECTRONICS CO LTD·Filed 2025·Application pending·0 cites
- 2155US8935073B2Reduced take-off field length using variable nozzleHURWITZ WAYNE·Filed 2006·Granted Jan 13, 2015·4 cites·20 claims
- 2255US2013170950A1Variable shape inlet section for a nacelle assembly of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2013·Application pending·0 cites
- 2354US9611758B2Gas turbine engine systems involving integrated fluid conduitsJAIN ASHOK K·Filed 2012·Granted Apr 4, 2017·0 cites·20 claims
- 2450US8209950B2Detecting ice buildup on an aircraft engine and actuating the turbofan exit nozzle to break the iceJAIN ASHOK K·Filed 2006·Granted Jul 3, 2012·3 cites·16 claims
- 2543US2014355441A1Method and apparatus of delivering assured services over unreliable internet infrastructure by using virtual overlay network architecture over a public cloud backboneJAIN ASHOK KUMAR·Filed 2013·Application pending·0 cites
- 2641US9729245B2Using artificial justifications to apply noise shaping to actual justifications associated with mapping client dataINFINERA CORP·Filed 2015·Granted Aug 8, 2017·0 cites·19 claims
- 2739US2008310956A1Variable geometry gas turbine engine nacelle assembly with nanoelectromechanical systemJAIN ASHOK K·Filed 2007·Application pending·0 cites
- 2836US10331601B2Systems, apparatus, and methods for efficient space to time conversion of OTU multiplexed signalINFINERA CORP·Filed 2016·Granted Jun 25, 2019·0 cites·20 claims
- 2927US2017317640A1Arrangement for angularly displacing solar panelsMAHINDRA SUSTEN PVT LTD·Filed 2017·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →