Claude G. Matalanis

Person

Longmeadow, MA, US

People

Patents Grantslast 30 patents

Information Patent Grant
High speed rotor blade design
- Patent number 12,116,119
- Issue date Oct 15, 2024
- Lockheed Martin Corporation
- Byung-Young Min
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Electrical conductor system for a rotor blade and method of manufac...
- Patent number 12,030,624
- Issue date Jul 9, 2024
- Lockheed Martin Corporation
- Eric S. Parsons
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Grant
Removable trailing edge assembly and system for rotor blade trailin...
- Patent number 11,794,887
- Issue date Oct 24, 2023
- Lockheed Martin Corporation
- Matthew Walter DiPalma
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rotor blade internal structure for trailing edge actuation
- Patent number 11,325,695
- Issue date May 10, 2022
- Lockheed Martin Corporation
- Frank M. Caputo
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Lubricant level sensing for an actuator
- Patent number 11,174,988
- Issue date Nov 16, 2021
- Sikorsky Aircraft Corporation
- Claude G. Matalanis
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Lubricant level sensing for an actuator
- Patent number 10,571,074
- Issue date Feb 25, 2020
- SIKORSKY ARICRAFT CORPORATION
- Claude G. Matalanis
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Active flow control system
- Patent number 10,538,313
- Issue date Jan 21, 2020
- Sikorsky Aircraft Corporation
- Brian E. Wake
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Plate member for reducing drag on a fairing of an aircraft
- Patent number 10,232,929
- Issue date Mar 19, 2019
- Sikorsky Aircraft Corporation
- Patrick Bowles
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Active airflow system and method of reducing drag for aircraft
- Patent number 10,220,939
- Issue date Mar 5, 2019
- Sikorsky Aircraft Corporation
- ByungYoung Min
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Boundary layer ingesting blade
- Patent number 9,688,395
- Issue date Jun 27, 2017
- Sikorsky Aircraft Corporation
- Blake Almy Moffitt
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Electromechanical rotary actuator and method
- Patent number 9,407,121
- Issue date Aug 2, 2016
- Hamilton Sundstrand Corporation
- Claude G. Matalanis
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Grant
Gas turbine engine inlet wall design
- Patent number 9,291,101
- Issue date Mar 22, 2016
- United Technologies Corporation
- Razvan Virgil Florea
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Modular integrated device for rotor blade control
- Patent number 9,278,755
- Issue date Mar 8, 2016
- Sikorsky Aircraft Corporation
- Claude G. Matalanis
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Harmonic data transfer in rotary wing aircraft
- Patent number 9,203,459
- Issue date Dec 1, 2015
- Sikorsky Aircraft Corporation
- Harshad S. Sane
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Low drag high restoring moment airfoils
- Patent number 9,132,914
- Issue date Sep 15, 2015
- Sikorsky Aircraft Corporation
- Claude G. Matalanis
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Active rotor blade control effector system for a rotary-wing aircraft
- Patent number 8,596,974
- Issue date Dec 3, 2013
- Sikorsky Aircraft Corporation
- Claude G. Matalanis
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
ELECTRICAL CONDUCTOR SYSTEM FOR A ROTOR BLADE AND METHOD OF MANUFAC...
- Publication number 20240326994
- Publication date Oct 3, 2024
- Lockheed Martin Corporation
- Eric S. Parsons
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Application
HIGH SPEED ROTOR BLADE DESIGN
- Publication number 20230322373
- Publication date Oct 12, 2023
- Lockheed Martin Corporation
- Byung-Young Min
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
REMOVABLE TRAILING EDGE ASSEMBLY AND SYSTEM FOR ROTOR BLADE TRAILIN...
- Publication number 20230322374
- Publication date Oct 12, 2023
- Lockheed Martin Corporation
- Matthew Walter DiPalma
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ELECTRICAL CONDUCTOR SYSTEM FOR A ROTOR BLADE AND METHOD OF MANUFAC...
- Publication number 20230098029
- Publication date Mar 30, 2023
- Lockheed Martin Corporation
- Eric S. Parsons
- H01 - BASIC ELECTRIC ELEMENTS
Information Patent Application
ROTOR BLADE INTERNAL STRUCTURE FOR TRAILING EDGE ACTUATION
- Publication number 20210323660
- Publication date Oct 21, 2021
- Lockheed Martin Corporation
- Frank M. Caputo
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
LUBRICANT LEVEL SENSING FOR AN ACTUATOR
- Publication number 20200278082
- Publication date Sep 3, 2020
- SIKORSKY AIRCRAFT CORPORATION
- Claude G. Matalanis
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Application
ROTOR BLADE DEFLECTION SENSING SYSTEM
- Publication number 20190241258
- Publication date Aug 8, 2019
- SIKORSKY AIRCRAFT CORPORATION
- Derek Geiger
- G01 - MEASURING TESTING
Information Patent Application
ACTIVE FLOW CONTROL SYSTEM
- Publication number 20180281932
- Publication date Oct 4, 2018
- SIKORSKY AIRCRAFT CORPORATION
- Brian E. WAKE
- H05 - ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
Information Patent Application
LUBRICANT LEVEL SENSING FOR AN ACTUATOR
- Publication number 20170336024
- Publication date Nov 23, 2017
- SIKORSKY AIRCRAFT CORPORATION
- Claude G. Matalanis
- G01 - MEASURING TESTING
Information Patent Application
PLATE MEMBER FOR REDUCING DRAG ON A FAIRING OF AN AIRCRAFT
- Publication number 20170225771
- Publication date Aug 10, 2017
- SIKORSKY AIRCRAFT CORPORATION
- Patrick Bowles
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ACTIVE AIRFLOW SYSTEM AND METHOD OF REDUCING DRAG FOR AIRCRAFT
- Publication number 20170225772
- Publication date Aug 10, 2017
- SIKORSKY AIRCRAFT CORPORATION
- ByungYoung Min
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
VORTEX GENERATORS AND METHOD OF CREATING VORTICES ON AN AIRCRAFT
- Publication number 20170174326
- Publication date Jun 22, 2017
- SIKORSKY AIRCRAFT CORPORATION
- Patrick Bowles
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
DRAG REDUCTION OF HIGH SPEED AIRCRAFT
- Publication number 20170096212
- Publication date Apr 6, 2017
- SIKORSKY AIRCRAFT CORPORATION
- Razvan Virgil Florea
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
BOUNDARY LAYER INGESTING BLADE
- Publication number 20150152733
- Publication date Jun 4, 2015
- SIKORSKY AIRCRAFT CORPORATION
- Blake Almy Moffitt
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE INLET WALL DESIGN
- Publication number 20150122952
- Publication date May 7, 2015
- United Technologies Corporation
- Razvan Virgil Florea
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Harmonic Data Transfer In Rotary Wing Aircraft
- Publication number 20140314130
- Publication date Oct 23, 2014
- Harshad S. Sane
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
LOW DRAG HIGH RESTORING MOMENT AIRFOILS
- Publication number 20140030103
- Publication date Jan 30, 2014
- SIKORSKY AIRCAFT CORPORATION
- Claude G. Matalanis
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ELECTROMECHANICAL ROTARY ACTUATOR AND METHOD
- Publication number 20130320782
- Publication date Dec 5, 2013
- Hamilton Sundstrand Corporation
- Claude G. Matalanis
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Application
MODULAR INTEGRATED DEVICE FOR ROTOR BLADE CONTROL
- Publication number 20120207602
- Publication date Aug 16, 2012
- SIKORSKY AIRCRAFT CORPORATION
- Claude G. Matalanis
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ACTIVE ROTOR BLADE CONTROL EFFECTOR SYSTEM FOR A ROTARY-WING AIRCRAFT
- Publication number 20110164976
- Publication date Jul 7, 2011
- SIKORSKY AIRCRAFT CORPORATION
- Claude G. Matalanis
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...

Claude G. Matalanis

Person

Patents Grantslast 30 patents

High speed rotor blade design

Electrical conductor system for a rotor blade and method of manufac...

Removable trailing edge assembly and system for rotor blade trailin...

Rotor blade internal structure for trailing edge actuation

Lubricant level sensing for an actuator

Lubricant level sensing for an actuator

Active flow control system

Plate member for reducing drag on a fairing of an aircraft

Active airflow system and method of reducing drag for aircraft

Boundary layer ingesting blade

Electromechanical rotary actuator and method

Gas turbine engine inlet wall design

Modular integrated device for rotor blade control

Harmonic data transfer in rotary wing aircraft

Low drag high restoring moment airfoils

Active rotor blade control effector system for a rotary-wing aircraft

Patents Applicationslast 30 patents

ELECTRICAL CONDUCTOR SYSTEM FOR A ROTOR BLADE AND METHOD OF MANUFAC...

HIGH SPEED ROTOR BLADE DESIGN

REMOVABLE TRAILING EDGE ASSEMBLY AND SYSTEM FOR ROTOR BLADE TRAILIN...

ELECTRICAL CONDUCTOR SYSTEM FOR A ROTOR BLADE AND METHOD OF MANUFAC...

ROTOR BLADE INTERNAL STRUCTURE FOR TRAILING EDGE ACTUATION

LUBRICANT LEVEL SENSING FOR AN ACTUATOR

ROTOR BLADE DEFLECTION SENSING SYSTEM

ACTIVE FLOW CONTROL SYSTEM

LUBRICANT LEVEL SENSING FOR AN ACTUATOR

PLATE MEMBER FOR REDUCING DRAG ON A FAIRING OF AN AIRCRAFT

ACTIVE AIRFLOW SYSTEM AND METHOD OF REDUCING DRAG FOR AIRCRAFT

VORTEX GENERATORS AND METHOD OF CREATING VORTICES ON AN AIRCRAFT

DRAG REDUCTION OF HIGH SPEED AIRCRAFT

BOUNDARY LAYER INGESTING BLADE

GAS TURBINE ENGINE INLET WALL DESIGN

Harmonic Data Transfer In Rotary Wing Aircraft

LOW DRAG HIGH RESTORING MOMENT AIRFOILS

ELECTROMECHANICAL ROTARY ACTUATOR AND METHOD

MODULAR INTEGRATED DEVICE FOR ROTOR BLADE CONTROL

ACTIVE ROTOR BLADE CONTROL EFFECTOR SYSTEM FOR A ROTARY-WING AIRCRAFT