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Inventor profile of:

Michael Winter

City:

New Haven, Connecticut

Country:

United States

Published Applications:

60

Last publication date:

2026-04-30

Top Assignees for applications by Michael Winter

The entities that hold a legal rights for patent applications filed by inventor Winter Michael:

Recent patent applications by Winter Michael

Michael Winter from New Haven, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2026-04-30
US20260117669A1
Mechanical engineering

Aircraft Propulsion System with Telescopic Guide Vane(S)

 #2 | 2026-03-05
US20260063075A1
Mechanical engineering

HYBRID ELECTRIC IDLE AND BRAKING FOR AN AIRCRAFT

 #3 | 2026-02-19
US20260048454A1
Performing operations; transporting

SYSTEM AND METHOD FOR LASER DRILLING OF SHAPED COOLING HOLES

 #4 | 2025-12-30
US18100297
Mechanical engineering

Composite airfoil with integrated anti-icing for an aircraft propulsion system

 #5 | 2025-12-25
US20250389207A1
Mechanical engineering

OIL SYSTEM BREATHER CONFIGURATION TO CAPTURE OIL EMISSIONS

 #6 | 2025-12-11
US20250376990A1
Mechanical engineering

GAS TURBINE ENGINE WITH SPLIT VARIABLE FAN EXIT GUIDE VANES AND AIRFLOW RADIAL TOTAL PRESSURE PROFILE RE-DISTRIBUTION

 #7 | 2025-12-11
US20250376931A1
Mechanical engineering

GAS TURBINE ENGINE WITH VARIABLE FAN EXIT GUIDE VANES

 #8 | 2025-11-20
US20250353383A1
Performing operations; transporting

HYBRID PROPULSION CONTROL SYSTEM UPDATE MODULE

 #9 | 2025-11-06
US20250341165A1
Mechanical engineering

MITIGATING IMPACT OF BLADE OUT EVENT

 #10 | 2025-10-16
US20250319973A1
Performing operations; transporting

ELECTRIC MACHINES FOR AIRCRAFT ENGINE FAULT DETECTION

 #11 | 2025-09-25
US20250296689A1
Performing operations; transporting

FAST THRUST RESPONSE USING OPTIMAL POWER SPLITTING IN HYBRID ELECTRIC AIRCRAFT

 #12 | 2025-06-24
US18106279
Performing operations; transporting

Monitoring and adjusting airfoils of an aircraft propulsion system

 #13 | 2025-05-27
US18734531
Mechanical engineering

Gas turbine engine with hybrid fan exit guide vanes

 #14 | 2024-02-01
US20240035392A1
Mechanical engineering

After-fan system with electrical motor for gas turbine engines

 #15 | 2023-12-28
US20230417186A1
Mechanical engineering

OIL CIRCULATION SYSTEM FOR HYBRID ELECTRIC ENGINE

 #16 | 2023-09-28
US20230303254A1
Performing operations; transporting

CRYOGENIC COOLING SYSTEM FOR AN AIRCRAFT

 #17 | 2023-07-20
US20230227171A1
Performing operations; transporting

ELECTRIC MACHINES FOR AIRCRAFT ENGINE FAULT DETECTION

 #18 | 2023-04-20
US20230122852A1
Performing operations; transporting

CRYOGENIC COOLING SYSTEM FOR AN AIRCRAFT

 #19 | 2023-03-16
US20230077719A1
Mechanical engineering

Attritable engine additively manufactured inlet cap

 #20 | 2022-12-15
US20220397060A1
Mechanical engineering

Oil circulation system for hybrid electric engine

 #21 | 2022-11-10
US20220356849A1
Mechanical engineering

Hybrid electric idle and braking for an aircraft

 #22 | 2022-11-03
US20220348341A1
Performing operations; transporting

HYBRID PROPULSION CONTROL SYSTEM UPDATE MODULE

 #23 | 2022-08-04
US20220243616A1
Mechanical engineering

Asymmetry in annular centering spring

 #24 | 2022-08-04
US20220242581A1
Performing operations; transporting

PROPULSION SYSTEM COOLING CONTROL

 #25 | 2022-06-23
US20220194604A1
Performing operations; transporting

Chilled working fluid generation and separation for an aircraft

 #26 | 2021-08-26
US20210262359A1
Mechanical engineering

After-fan system with electrical motor for gas turbine engines

 #27 | 2021-02-18
US20210047970A1
Mechanical engineering

Rotor dynamics accommodation using electrical power assist

 #28 | 2020-12-10
US20200386160A1
Mechanical engineering

Attritable engine additively manufactured inlet cap

 #29 | 2020-10-15
US20200325852A1
Mechanical engineering

After-fan system for a gas turbine engine

 #30 | 2020-06-18
US20200189041A1
Performing operations; transporting

System and method for laser drilling of shaped cooling holes

 #31 | 2020-06-18
US20200189040A1
Performing operations; transporting

System and method for laser drilling of shaped cooling holes

 #32 | 2019-09-26
US20190293346A1
Mechanical engineering

Propulsion system cooling control

 #33 | 2019-09-26
US20190292982A1
Mechanical engineering

Chilled working fluid generation and separation for an aircraft

 #34 | 2019-09-26
US20190291877A1
Performing operations; transporting

Cryogenic cooling system for an aircraft

 #35 | 2016-11-03
US20160319667A1
Mechanical engineering

Gas turbine engine compressor rotor vaporization cooling

 #36 | 2016-10-06
US20160290239A1
Mechanical engineering

Variable area nozzle assisted gas turbine engine restarting

 #37 | 2015-12-17
US20150361880A1
Mechanical engineering

Gas turbine engine with distributed fans with drive control

 #38 | 2014-01-02
US20140000278A1
Mechanical engineering

Turbomachine thermal energy exchange

 #39 | 2013-05-23
US20130125561A1
Mechanical engineering

GEARED TURBOFAN WITH DISTRIBUTED ACCESSORY GEARBOXES

 #40 | 2012-05-17
US20120117940A1
Mechanical engineering

GAS TURBINE ENGINE WITH PYLON MOUNTED ACCESSORY DRIVE

 #41 | 2011-03-31
US20110072828A1
Mechanical engineering

Gas turbine engine system providing simulated boundary layer thickness increase

 #42 | 2011-01-06
US20110004388A1
Mechanical engineering

TURBOFAN TEMPERATURE CONTROL WITH VARIABLE AREA NOZZLE

 #43 | 2011-01-06
US20110000217A1
Mechanical engineering

Managing spool bearing load using variable area flow nozzle

 #44 | 2010-09-23
US20100236216A1
Mechanical engineering

Turbofan engine with variable area fan nozzle and low spool generator for emergency power generation and method for providing emergency power

 #45 | 2010-06-10
US20100139285A1
Mechanical engineering

Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle

 #46 | 2010-03-18
US20100068039A1
Mechanical engineering

Turbofan engine with variable bypass nozzle exit area and method of operation

 #47 | 2010-03-04
US20100050596A1
Mechanical engineering

Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle

 #48 | 2010-02-25
US20100043390A1
Mechanical engineering

Detecting ice buildup on an aircraft engine and actuating the turbofan exit nozzle to break the ice

 #49 | 2009-10-08
US20090252600A1
Mechanical engineering

Actuation of a turbofan engine bifurcation to change an effective nozzle exit area

 #50 | 2009-09-24
US20090235638A1
Mechanical engineering

Variable area nozzle assisted gas turbine engine restarting

 #51 | 2009-07-16
US20090178416A1
Mechanical engineering

Bifurcation and aft vent used to vary fan nozzle exit area

 #52 | 2009-06-18
US20090155072A1
Mechanical engineering

Fan nacelle flow control

 #53 | 2009-06-04
US20090139243A1
Mechanical engineering

Gas turbine engine with pylon mounted accessory drive

 #54 | 2009-04-09
US20090092482A1
Mechanical engineering

Systems and methods for altering inlet airflow of gas turbine engines

 #55 | 2009-01-08
US20090008508A1
Mechanical engineering

Variable contour nacelle assembly for a gas turbine engine

 #56 | 2008-12-25
US20080317588A1
Mechanical engineering

Managing spool bearing load using variable area flow nozzle

 #57 | 2008-11-20
US20080283676A1
Mechanical engineering

Variable contraction ratio nacelle assembly for a gas turbine engine

 #58 | 2008-10-30
US20080267762A1
Mechanical engineering

Nacelle assembly having inlet airfoil for a gas turbine engine

 #59 | 2008-05-15
US20080112799A1
Mechanical engineering

Gas turbine engine providing simulated boundary layer thickness increase

 #60 | 2008-01-03
US20080001039A1
Mechanical engineering

Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle
InventorID:

253666 ⎘