Inventor · disambiguated record
Edward B. Thayer
Also filed as: THAYER EDWARD · THAYER EDWARD B
25 granted patents·1 pending application·684 citations·filing 1975–2006
97Inventor score
Top patents by PatentIndex Score
26 records- 0191US7299135B2Methods for identifying discrete populations (e.g., clusters) of data within a flow cytometer multi-dimensional data setIDEXX LAB INC·Filed 2005·Granted Nov 20, 2007·27 cites·29 claims
- 0291US5706650AVectoring nozzle using injected high pressure airUNITED TECHNOLOGIES CORP·Filed 1995·Granted Jan 13, 1998·70 cites·24 claims
- 0389US4836451AYaw and pitch convergent-divergent thrust vectoring nozzleUNITED TECHNOLOGIES CORP·Filed 1987·Granted Jun 6, 1989·81 cites·7 claims
- 0488US4819876ADivergent flap actuation system for a two-dimensional exhaust nozzleUNITED TECHNOLOGIES CORP·Filed 1987·Granted Apr 11, 1989·47 cites·4 claims
- 0585US5261605AAxisymmetric nozzle with gimbled unison ringUNITED TECHNOLOGIES CORP·Filed 1992·Granted Nov 16, 1993·51 cites·2 claims
- 0680US5335489AGas turbine vectoring exhaust nozzleUNITED TECHNOLOGIES CORP·Filed 1993·Granted Aug 9, 1994·39 cites·9 claims
- 0780US3973731AFlap-type two-dimensional nozzleUNITED TECHNOLOGIES CORP·Filed 1975·Granted Aug 10, 1976·30 cites·5 claims
- 0878US4848664AYaw thrust vectoring exhaust nozzleUNITED TECHNOLOGIES CORP·Filed 1987·Granted Jul 18, 1989·32 cites·4 claims
- 0977US5619851ARocket nozzle for a rocket engineUNITED TECHNOLOGIES CORP·Filed 1989·Granted Apr 15, 1997·36 cites·9 claims
- 1076US4753392ATwo dimensional gas turbine engine exhaust nozzleUNITED TECHNOLOGIES CORP·Filed 1984·Granted Jun 28, 1988·29 cites·9 claims
- 1174US4798328AArea controlled, thrust vectoring vane cascade with nutating control vaneUNITED TECHNOLOGIES CORP·Filed 1987·Granted Jan 17, 1989·28 cites·3 claims
- 1271US4760960ALinkage for area controlled, thrust vectoring vane cascadeUNITED TECHNOLOGIES CORP·Filed 1987·Granted Aug 2, 1988·25 cites·8 claims
- 1369US4993641AGas turbine spherical exhaust nozzleUNITED TECHNOLOGIES CORP·Filed 1989·Granted Feb 19, 1991·22 cites·7 claims
- 1465US4714197A2-D propulsive lift nozzleUNITED TECHNOLOGIES CORP·Filed 1986·Granted Dec 22, 1987·20 cites·7 claims
- 1562US5343698AHexagonal cluster nozzle for a rocket engineUNITED TECHNOLOGIES CORP·Filed 1993·Granted Sep 6, 1994·27 cites·10 claims
- 1659US4805401AControl vent for diverting exhaust nozzleUNITED TECHNOLOGIES CORP·Filed 1987·Granted Feb 21, 1989·21 cites·7 claims
- 1756US4591097AThrust reverser/exhaust nozzle assembly for a gas turbine engineUS AIR FORCE·Filed 1984·Granted May 27, 1986·20 cites·6 claims
- 1856US4005823AFlap-type two-dimensional nozzle having a plugUNITED TECHNOLOGIES CORP·Filed 1975·Granted Feb 1, 1977·21 cites·9 claims
- 1955US4382551AFlap-type nozzle with built-in reverserUNITED TECHNOLOGIES CORP·Filed 1981·Granted May 10, 1983·13 cites·10 claims
- 2055US2008108510A1Method for estimating error from a small number of expression samplesTHAYER EDWARD·Filed 2006·Application pending·0 cites
- 2148US5683033ARocket nozzle for a rocket engineUNITED TECHNOLOGIES CORP·Filed 1990·Granted Nov 4, 1997·15 cites·7 claims
- 2244US5098022AFlow diverting nozzle for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1991·Granted Mar 24, 1992·12 cites·6 claims
- 2342US5161752AIn-flight reverserUNITED TECHNOLOGIES CORP·Filed 1991·Granted Nov 10, 1992·11 cites·6 claims
- 2434US5209432AAircraft reverser port doorUNITED TECHNOLOGIES CORP·Filed 1992·Granted May 11, 1993·4 cites·6 claims
- 2532US5292069AConvertible plug nozzleUNITED TECHNOLOGIES CORP·Filed 1993·Granted Mar 8, 1994·3 cites·9 claims
- 2627US5150862AIn-flight reverserUNITED TECHNOLOGIES CORP·Filed 1991·Granted Sep 29, 1992·0 cites·8 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →