Inventor · disambiguated record
Edward T. Piesik
Also filed as: PIESIK EDWARD · PIESIK EDWARD T
24 granted patents·488 citations·filing 1975–2016
97Inventor score
Files withGEN DYNAMICS POMONA DIV13GEN DYNAMICS CORP6GEN DYNAMICS AIR DEFENSE2HUGHES MISSILE SYSTEMS2PIESIK EDWARD1
Top patents by PatentIndex Score
24 records- 0189US4934241ARocket exhaust deflectorGEN DYNAMICS CORP·Filed 1987·Granted Jun 19, 1990·48 cites·23 claims
- 0287US4044648ARocket exhaust plenum flow control apparatusGEN DYNAMICS CORP·Filed 1975·Granted Aug 30, 1977·40 cites·30 claims
- 0385US4324167AFlexible area launch tube rear coverGEN DYNAMICS POMONA DIV·Filed 1980·Granted Apr 13, 1982·37 cites·17 claims
- 0485US4134327ARocket launcher tube post-launch rear closureGEN DYNAMICS CORP·Filed 1977·Granted Jan 16, 1979·35 cites·14 claims
- 0579US4373420ACombustion suppressorGEN DYNAMICS POMONA DIV·Filed 1980·Granted Feb 15, 1983·30 cites·8 claims
- 0678US4686884AGas management deflectorGEN DYNAMICS POMONA DIV·Filed 1985·Granted Aug 18, 1987·32 cites·19 claims
- 0776US4173919ATwo-way rocket plenum for combustion suppressionGEN DYNAMICS CORP·Filed 1977·Granted Nov 13, 1979·25 cites·12 claims
- 0875US5194688AApparatus for limiting recirculation of rocket exhaust gases during missile launchHUGHES MISSILE SYSTEMS·Filed 1992·Granted Mar 16, 1993·32 cites·11 claims
- 0971US4683798AGas management transition deviceGEN DYNAMICS POMONA DIV·Filed 1985·Granted Aug 4, 1987·25 cites·10 claims
- 1069US4796510ARocket exhaust recirculation obturator for missile launch tubeGEN DYNAMICS POMONA DIV·Filed 1987·Granted Jan 10, 1989·23 cites·5 claims
- 1168US4404887ARecoil reducerGEN DYNAMICS POMONA DIV·Filed 1982·Granted Sep 20, 1983·20 cites·2 claims
- 1268US4186647AMultiple area rear launch tube coverGEN DYNAMICS CORP·Filed 1978·Granted Feb 5, 1980·18 cites·8 claims
- 1367US4327624ATip off rate reducerGEN DYNAMICS POMONA DIV·Filed 1980·Granted May 4, 1982·19 cites·7 claims
- 1461US4756226AMissile support structure for a launch tubeGEN DYNAMICS POMONA DIV·Filed 1987·Granted Jul 12, 1988·17 cites·8 claims
- 1555US4733751ARocket exhaust disrupterGEN DYNAMICS POMONA DIV·Filed 1985·Granted Mar 29, 1988·15 cites·8 claims
- 1655US4545284AProtection device for rocket launcher railGEN DYNAMICS POMONA DIV·Filed 1983·Granted Oct 8, 1985·12 cites·19 claims
- 1754US11020543B1Decubitus ulcer healing airflow devicePIESIK EDWARD·Filed 2016·Granted Jun 1, 2021·1 cites·6 claims
- 1852US5162605ASelf-activated rocket launcher cell closureGEN DYNAMICS CORP·Filed 1992·Granted Nov 10, 1992·15 cites·9 claims
- 1949US4685533AExhaust dissipator deviceGEN DYNAMICS POMONA DIV·Filed 1985·Granted Aug 11, 1987·16 cites·7 claims
- 2043US5136922ASelf-actuating rocket chamber closures for multi-missile launch cellsGEN DYNAMICS AIR DEFENSE·Filed 1991·Granted Aug 11, 1992·10 cites·10 claims
- 2141US4480522ARocket exhaust-gas deflectorGEN DYNAMICS POMONA DIV·Filed 1981·Granted Nov 6, 1984·6 cites·20 claims
- 2239US5206450AMulti-missile canister gas management systemGEN DYNAMICS AIR DEFENSE·Filed 1991·Granted Apr 27, 1993·8 cites·12 claims
- 2332US5422443ARocket exhaust disrupter shapesHUGHES MISSILE SYSTEMS·Filed 1993·Granted Jun 6, 1995·2 cites·12 claims
- 2431US4709780AExhaust dissipator/disrupter deviceGEN DYNAMICS POMONA DIV·Filed 1985·Granted Dec 1, 1987·2 cites·7 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →