Inventor · disambiguated record
Peter Holemans
Also filed as: HOLEMANS PETER
13 granted patents·209 citations·filing 1990–2019
91Inventor score
Top patents by PatentIndex Score
13 records- 0194US5082721AFabrics for protective garment or coverSMITH NOVIS W JR·Filed 1990·Granted Jan 21, 1992·81 cites·14 claims
- 0289US10207788B2Structure having joined unitary structuresBOEING CO·Filed 2016·Granted Feb 19, 2019·3 cites·18 claims
- 0381US6918839B2Damage tolerant shaftBOEING CO·Filed 2002·Granted Jul 19, 2005·15 cites·12 claims
- 0478US9216821B1Methods and systems for helicopter rotor blade balancingBOEING CO·Filed 2013·Granted Dec 22, 2015·8 cites·11 claims
- 0576US10053203B2Composite stiffener with integral conductive elementBOEING CO·Filed 2015·Granted Aug 21, 2018·3 cites·9 claims
- 0674US9981446B2Structural inserts for honeycomb structuresBOEING CO·Filed 2013·Granted May 29, 2018·6 cites·20 claims
- 0766US6780488B2Liquid molded hollow cell core composite articlesBOEING CO·Filed 2001·Granted Aug 24, 2004·12 cites·24 claims
- 0864US6974555B2Method of fabricating a damage tolerant shaftBOEING CO·Filed 2003·Granted Dec 13, 2005·4 cites·14 claims
- 0957US10773821B2Energy absorbing composite panelsBOEING CO·Filed 2018·Granted Sep 15, 2020·1 cites·23 claims
- 1053US5041287ASprayable composition using acetone solventDRIGGERS TERRY L·Filed 1990·Granted Aug 20, 1991·49 cites·19 claims
- 1148US5494720ASeams and closures for plastic fabrics and clothingLAKELAND IND INC·Filed 1994·Granted Feb 27, 1996·27 cites·8 claims
- 1246US11001375B2Structurally tunable coresBOEING CO·Filed 2019·Granted May 11, 2021·0 cites·26 claims
- 1345US7309166B2Hub joint for transferring load from a rotating shaft to a stationary bodyBOEING CO·Filed 2005·Granted Dec 18, 2007·0 cites·20 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →