Inventor · disambiguated record
David Waldman
Also filed as: WALDMAN DAVID · WALDMAN DAVID R · WALDMAN DAVID ROSS
21 granted patents·2 pending applications·207 citations·filing 2002–2020
95Inventor score
Top patents by PatentIndex Score
23 records- 0197US9752835B2Unitary heat exchangers having integrally-formed compliant heat exchanger tubes and heat exchange systems including the sameHONEYWELL INT INC·Filed 2013·Granted Sep 5, 2017·19 cites·12 claims
- 0292US9951632B2Hybrid bonded turbine rotors and methods for manufacturing the sameHONEYWELL INT INC·Filed 2015·Granted Apr 24, 2018·10 cites·13 claims
- 0390US9410702B2Gas turbine engine combustors with effusion and impingement cooling and methods for manufacturing the same using additive manufacturing techniquesHONEYWELL INT INC·Filed 2014·Granted Aug 9, 2016·15 cites·13 claims
- 0489US11021965B2Engine components with cooling holes having tailored metering and diffuser portionsHONEYWELL INT INC·Filed 2016·Granted Jun 1, 2021·5 cites·14 claims
- 0589US7000306B2Spun metal form used to manufacture dual alloy turbine wheelHONEYWELL INT INC·Filed 2004·Granted Feb 21, 2006·37 cites·34 claims
- 0688US9764435B2Counter-flow heat exchange systemsHONEYWELL INT INC·Filed 2013·Granted Sep 19, 2017·18 cites·10 claims
- 0787US9879566B2Turbine engine couplings and methods for manufacturing turbine engine couplingsHONEYWELL INT INC·Filed 2015·Granted Jan 30, 2018·3 cites·13 claims
- 0885US10113433B2Gas turbine engine components with lateral and forward sweep film cooling holesHONEYWELL INT INC·Filed 2012·Granted Oct 30, 2018·9 cites·12 claims
- 0983US10711630B2Retention and control system for turbine shroud ringHONEYWELL INT INC·Filed 2018·Granted Jul 14, 2020·7 cites·20 claims
- 1082US9879544B2Turbine rotor blades with improved tip portion cooling holesHONEYWELL INT INC·Filed 2013·Granted Jan 30, 2018·7 cites·15 claims
- 1179US11333042B2Turbine blade with dust tolerant cooling systemHONEYWELL INT INC·Filed 2020·Granted May 17, 2022·1 cites·20 claims
- 1279US9816389B2Turbine rotor blades with tip portion parapet wall cavitiesHONEYWELL INT INC·Filed 2013·Granted Nov 14, 2017·6 cites·18 claims
- 1379US7097422B2Hoop stress relief mechanism for gas turbine enginesHONEYWELL INT INC·Filed 2004·Granted Aug 29, 2006·43 cites·28 claims
- 1469US10030542B2Compliant coupling systems and methods for shroudsHONEYWELL INT INC·Filed 2015·Granted Jul 24, 2018·2 cites·18 claims
- 1569US8070448B2Spacers and turbinesMORRIS MARK C·Filed 2008·Granted Dec 6, 2011·10 cites·20 claims
- 1667US7516526B2Spun metal form used to manufacture dual alloy turbine wheelHONEYWELL INT INC·Filed 2004·Granted Apr 14, 2009·10 cites·23 claims
- 1764US11286791B2Engine components with cooling holes having tailored metering and diffuser portionsHONEYWELL INT INC·Filed 2020·Granted Mar 29, 2022·0 cites·17 claims
- 1858US10787932B2Turbine blade with dust tolerant cooling systemHONEYWELL INT INC·Filed 2018·Granted Sep 29, 2020·0 cites·17 claims
- 1957US10900363B2Laser tip cladding to net-shape with shroudsHONEYWELL INT INC·Filed 2018·Granted Jan 26, 2021·0 cites·20 claims
- 2055US9506566B2Finger-foil seals and gas turbine engines employing the sameHONEYWELL INT INC·Filed 2013·Granted Nov 29, 2016·1 cites·20 claims
- 2142US6935006B2Spun metal form used to manufacture dual alloy turbine wheelHONEYWELL INT INC·Filed 2002·Granted Aug 30, 2005·4 cites·26 claims
- 2242US2010095679A1Dual wall structure for use in a combustor of a gas turbine engineHONEYWELL INT INC·Filed 2008·Application pending·0 cites
- 2340US2014161598A1Impeller backface rotating heat shieldHONEYWELL INT INC·Filed 2012·Application pending·0 cites
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