Inventor · disambiguated record
Donald W. Peters
Also filed as: PETERS DONALD · PETERS DONALD W · PETERS DONALD WILLIAM
34 granted patents·3 pending applications·171 citations·filing 2004–2022
96Inventor score
Top patents by PatentIndex Score
37 records- 0191US9945295B2Composite piston ring seal for axially and circumferentially translating ductsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 17, 2018·6 cites·16 claims
- 0291US7581301B2Method for attaching a non-metal component to a metal componentUNITED TECHNOLOGIES CORP·Filed 2006·Granted Sep 1, 2009·22 cites·14 claims
- 0390US9835043B2Guided binding-resistant actuation apparatus and methodUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 5, 2017·14 cites·20 claims
- 0486US10087884B2Stepped fairing modulated exhaust coolingUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 2, 2018·4 cites·9 claims
- 0586US9551456B2Belleville washer nut plateUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jan 24, 2017·9 cites·15 claims
- 0683US10280791B2Tuned mass damper for tubesUNITED TECHNOLOGIES CORP·Filed 2016·Granted May 7, 2019·4 cites·20 claims
- 0783US9034465B2Thermally insulative attachmentPETERS DONALD W·Filed 2012·Granted May 19, 2015·8 cites·10 claims
- 0878US7624567B2Convergent divergent nozzle with interlocking divergent flapsUNITED TECHNOLOGIES CORP·Filed 2005·Granted Dec 1, 2009·13 cites·8 claims
- 0978US7261489B2Fastener assembly for attaching a non-metal component to a metal componentUNITED TECHNOLOGIES CORP·Filed 2004·Granted Aug 28, 2007·21 cites·12 claims
- 1075US10012104B2Gas turbine engine convergent/divergent nozzle with unitary synchronization ring for roller track nozzleUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 3, 2018·2 cites·13 claims
- 1175US7624579B2Convergent divergent nozzle with supported divergent sealsUNITED TECHNOLOGIES CORP·Filed 2006·Granted Dec 1, 2009·11 cites·9 claims
- 1273US7096661B2Axial divergent section slot nozzleUNITED TECHNOLOGIES CORP·Filed 2004·Granted Aug 29, 2006·25 cites·21 claims
- 1371US10551066B2Combustor liner panel and rail with diffused interface passage for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Feb 4, 2020·1 cites·23 claims
- 1471US9803557B2Gas turbine engine and blocker door assemblyUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 31, 2017·2 cites·9 claims
- 1570US11939924B2Synchronized air modulating systemRAYTHEON TECH CORP·Filed 2022·Granted Mar 26, 2024·0 cites·7 claims
- 1669US10823412B2Panel surface pockets for coating retentionUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 3, 2020·1 cites·13 claims
- 1764US10371089B2System for actuating an exhaust cowlUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 6, 2019·1 cites·16 claims
- 1864US9157394B2Adjustable cable for exhaust duct liner hangerPETERS DONALD W·Filed 2012·Granted Oct 13, 2015·3 cites·7 claims
- 1963US11156359B2Combustor liner panel end rail with diffused interface passage for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 26, 2021·0 cites·13 claims
- 2063US7007483B2Turbine engine nozzleUNITED TECHNOLOGIES CORP·Filed 2004·Granted Mar 7, 2006·12 cites·20 claims
- 2162US9732632B2Multi-component fastener and method of producing the sameUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 15, 2017·1 cites·17 claims
- 2261US11492977B2Synchronized air modulating systemUNITED TECHNOLOGIES CORP·Filed 2019·Granted Nov 8, 2022·0 cites·9 claims
- 2360US10760500B2Composite piston ring seal for axially and circumferentially translating ductsUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 1, 2020·0 cites·19 claims
- 2458US9309834B2Liner hanger cablePETERS DONALD W·Filed 2012·Granted Apr 12, 2016·2 cites·18 claims
- 2557US10760529B2Composite wear pad for exhaust nozzleUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 1, 2020·0 cites·7 claims
- 2655US7721550B2Aircraft engine exhaust flap curved strut slotUNITED TECHNOLOGIES CORP·Filed 2005·Granted May 25, 2010·3 cites·22 claims
- 2754US10352248B2Synchronized air modulating systemUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 16, 2019·0 cites·10 claims
- 2854US10180105B2Adjustable cable for exhaust duct liner hangerUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jan 15, 2019·0 cites·19 claims
- 2953US9938930B2Composite wear pad for exhaust nozzleUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 10, 2018·0 cites·13 claims
- 3050US10041444B2Variable orifice jet for a turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 7, 2018·0 cites·20 claims
- 3148US9464655B2Push-lock pinUNITED TECHNOLOGIES CORP·Filed 2012·Granted Oct 11, 2016·0 cites·14 claims
- 3248US7546738B2Turbine engine nozzleUNITED TECHNOLOGIES CORP·Filed 2004·Granted Jun 16, 2009·6 cites·13 claims
- 3347US10605200B2Serpentine baffle for a gas turbine engine exhaust ductUNITED TECHNOLOGIES CORP·Filed 2013·Granted Mar 31, 2020·0 cites·21 claims
- 3443US2014238027A1Thermally compliant dual wall liner for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 3542US2018283695A1Combustion panel grommetUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 3640US2016169261A1Ceramic bolt for exhaust panelUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 3738US9856956B2Rod-and-bracket connector system for securing a pivoting member to a guide anchor moveably secured within a guide trackUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jan 2, 2018·0 cites·15 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →