Inventor · disambiguated record
Roger M. Crane
Also filed as: CRANE ROGER M
23 granted patents·667 citations·filing 1983–2006
97Inventor score
Top patents by PatentIndex Score
23 records- 0195US5308675AFlexible high damping structureUS ARMY·Filed 1992·Granted May 3, 1994·105 cites·27 claims
- 0293US7959058B1Hybrid composite welded jointUS NAVY·Filed 2006·Granted Jun 14, 2011·32 cites·14 claims
- 0388US5833782AHigh-energy-absorbing enclosure for internal explosion containmentUS NAVY·Filed 1997·Granted Nov 10, 1998·51 cites·9 claims
- 0487US6799126B1Nondestructive method for detecting structural anomalies in compositesUS NAVY·Filed 2003·Granted Sep 28, 2004·43 cites·38 claims
- 0586US5447765AHigh-damping rib-stiffened composite hollow cylinder core configurationUS ARMY·Filed 1994·Granted Sep 5, 1995·50 cites·11 claims
- 0685US5023845AEmbedded fiber optic beam displacement sensorUS NAVY·Filed 1988·Granted Jun 11, 1991·43 cites·14 claims
- 0784US4581527ADamage assessment system for composite plastic structures using fiber opticsUS NAVY·Filed 1983·Granted Apr 8, 1986·36 cites·5 claims
- 0881US5654053AHigh-energy-absorbing enclosure for internal explosion containmentUS NAVY·Filed 1995·Granted Aug 5, 1997·40 cites·8 claims
- 0970US5108262AHigh damping flexible propeller/implellerUS NAVY·Filed 1990·Granted Apr 28, 1992·42 cites·7 claims
- 1069US4954377ALoad bearing connective damperUS NAVY·Filed 1988·Granted Sep 4, 1990·23 cites·20 claims
- 1168US5379711ARetrofittable monolithic box beam composite hull systemUS ARMY·Filed 1992·Granted Jan 10, 1995·20 cites·27 claims
- 1267US5744221AFlexible high-damping composite structures and fabrication thereofUS ARMY·Filed 1994·Granted Apr 28, 1998·26 cites·29 claims
- 1363US5261616AMulti-layered translated rib-stiffened composite hollow cylinder assemblyUS ARMY·Filed 1992·Granted Nov 16, 1993·19 cites·4 claims
- 1461US4695344AResin impregnation and processing technique for rigidizing net-shaped fibrous skeletal composite preformsUS NAVY·Filed 1985·Granted Sep 22, 1987·22 cites·13 claims
- 1558US6540442B1High energy impact absorption fender system using valvular control logicUS NAVY·Filed 2001·Granted Apr 1, 2003·7 cites·5 claims
- 1656US6053664AElastomeric composite bumper system and method for absorbing high energy impactUS NAVY·Filed 1998·Granted Apr 25, 2000·21 cites·25 claims
- 1754US5573344AHigh damping composite joint for mechanical vibration and acoustic energy dissipationUS ARMY·Filed 1994·Granted Nov 12, 1996·21 cites·28 claims
- 1852US5288114AAttachment methodology for composite cylinder assemblyUS ARMY·Filed 1992·Granted Feb 22, 1994·13 cites·18 claims
- 1950US6283677B1Tailorable elastomeric composite pneumatic fender system for absorbing high energy impactUS NAVY·Filed 1999·Granted Sep 4, 2001·13 cites·23 claims
- 2049US5693166AMethod for fabricating a high-damping rib-stiffened composite hollow cylinder core configurationUS ARMY·Filed 1995·Granted Dec 2, 1997·11 cites·20 claims
- 2147US5284697AComposite structures having organic matrices and duplex zinc/ceramic fire barriersUS ARMY·Filed 1992·Granted Feb 8, 1994·9 cites·2 claims
- 2244US5348052AMulti-layered translated rib-stiffened composite hollow cylinder assemblyUS ARMY·Filed 1993·Granted Sep 20, 1994·14 cites·14 claims
- 2335US5349738AAttachment methodology for composite cylinder assemblyUS ARMY·Filed 1993·Granted Sep 27, 1994·6 cites·21 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →