Inventor · disambiguated record
Allan R. Penda
Also filed as: PENDA ALLAN R
19 granted patents·1 pending application·274 citations·filing 1994–2015
95Inventor score
Top patents by PatentIndex Score
20 records- 0192US9797311B2Integrated thermal system for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 24, 2017·7 cites·10 claims
- 0292US8966875B2Constant speed transmission for gas turbine engineSUCIU GABRIEL L·Filed 2011·Granted Mar 3, 2015·16 cites·17 claims
- 0391US9714610B2Low profile compressor bleed air-oil coolersUNITED TECHNOLOGIES CORP·Filed 2012·Granted Jul 25, 2017·14 cites·20 claims
- 0489US9038367B2Fan case thrust reverserSUCIU GABRIEL L·Filed 2011·Granted May 26, 2015·11 cites·20 claims
- 0586US7596954B2Blade clearance controlUNITED TECHNOLOGIES CORP·Filed 2004·Granted Oct 6, 2009·36 cites·28 claims
- 0684US9080511B2Integrated thermal system for a gas turbine engineSUCIU GABRIEL L·Filed 2011·Granted Jul 14, 2015·7 cites·7 claims
- 0783US9109462B2Energy-absorbing fan case for a gas turbine engineSUCIU GABRIEL L·Filed 2011·Granted Aug 18, 2015·8 cites·20 claims
- 0882US10144524B2Assembly for mounting a turbine engine to a pylonROHR INC·Filed 2013·Granted Dec 4, 2018·9 cites·13 claims
- 0979US5482429AFan blade containment assemblyUNITED TECHNOLOGIES CORP·Filed 1994·Granted Jan 9, 1996·62 cites·4 claims
- 1078US8978351B2Integrated thermal management system and environmental control system for a gas turbine engineSUCIU GABRIEL L·Filed 2011·Granted Mar 17, 2015·8 cites·16 claims
- 1178US5485723AVariable thickness isogrid caseUNITED TECHNOLOGIES CORP·Filed 1994·Granted Jan 23, 1996·44 cites·3 claims
- 1270US10087886B2Turbofan thrust reverser systemUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 2, 2018·3 cites·7 claims
- 1369US9297272B2Grounding for fan blades on an underblade spacerUNITED TECHNOLOGIES CORP·Filed 2012·Granted Mar 29, 2016·2 cites·22 claims
- 1464US9909445B2Monitoring a dynamic parameter such as torque in a rotational systemUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 6, 2018·2 cites·20 claims
- 1563US8672260B2Single plane mount system for gas turbine enginePENDA ALLAN R·Filed 2009·Granted Mar 18, 2014·8 cites·17 claims
- 1660US10179377B2Process for manufacturing a gamma titanium aluminide turbine componentUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jan 15, 2019·0 cites·5 claims
- 1759US10563592B2Turbo compressor for bleed airUNITED TECHNOLOGIES CORP·Filed 2012·Granted Feb 18, 2020·1 cites·13 claims
- 1857US6048174AImpact resistant hollow airfoilsUNITED TECHNOLOGIES CORP·Filed 1997·Granted Apr 11, 2000·36 cites·8 claims
- 1948US2016146104A1Angled Core EngineUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 2033US8573940B2Interlocking knife edge sealsPICKENS JOHN T·Filed 2006·Granted Nov 5, 2013·0 cites·12 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →