Santo CHIAPPETTA

Person

Georgetown, CA

People

Patents Grantslast 30 patents

Information Patent Grant
Gas turbine engine with variable speed output
- Patent number 11,623,756
- Issue date Apr 11, 2023
- Pratt & Whitney Canada Corp.
- David Menheere
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Axial inertial particle separator for turbine engine
- Patent number 11,608,782
- Issue date Mar 21, 2023
- Pratt & Whitney Canada Corp.
- David Menheere
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Aircraft and method of operating same
- Patent number 11,585,280
- Issue date Feb 21, 2023
- Pratt & Whitney Canada Corp.
- Santo Chiappetta
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
System and method for increasing bleed air flow to a heat exchanger...
- Patent number 11,390,386
- Issue date Jul 19, 2022
- Pratt & Whitney Canada Corp.
- Daniel Van Den Ende
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Inertial particle separator for turbine engine
- Patent number 11,261,789
- Issue date Mar 1, 2022
- Pratt & Whitney Canada Corp.
- David Menheere
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
System and method for conditioning a fluid using bleed air from a b...
- Patent number 11,215,124
- Issue date Jan 4, 2022
- Pratt & Whitney Canada Corp.
- Daniel Van Den Ende
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine with differential gearbox
- Patent number 11,041,444
- Issue date Jun 22, 2021
- Pratt & Whitney Canada Corp.
- Tim Redford
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
AIRCRAFT AND METHOD OF OPERATING SAME
- Publication number 20220136448
- Publication date May 5, 2022
- Santo CHIAPPETTA
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INERTIAL PARTICLE SEPARATOR FOR TURBINE ENGINE
- Publication number 20210324797
- Publication date Oct 21, 2021
- PRATT & WHITNEY CANADA CORP.
- David MENHEERE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AXIAL INERTIAL PARTICLE SEPARATOR FOR TURBINE ENGINE
- Publication number 20210324795
- Publication date Oct 21, 2021
- Pratt & Whitney Canada Corp.
- David MENHEERE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH VARIABLE SPEED OUTPUT
- Publication number 20210276724
- Publication date Sep 9, 2021
- Pratt & Whitney Canada Corp.
- David MENHEERE
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
SYSTEM AND METHOD FOR CONDITIONING A FLUID USING BLEED AIR FROM A B...
- Publication number 20210062727
- Publication date Mar 4, 2021
- Pratt & Whitney Canada Corp.
- Daniel VAN DEN ENDE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SYSTEM AND METHOD FOR INCREASING BLEED AIR FLOW TO A HEAT EXCHANGER...
- Publication number 20210061476
- Publication date Mar 4, 2021
- Pratt & Whitney Canada Corp.
- Daniel VAN DEN ENDE
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT ENGINE AND METHOD OF OPERATION THEREOF
- Publication number 20200386408
- Publication date Dec 10, 2020
- Pratt & Whitney Canada Corp.
- David MENHEERE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT ENGINE AND METHOD OF OPERATION THEREOF
- Publication number 20200386407
- Publication date Dec 10, 2020
- Pratt & Whitney Canada Corp.
- David MENHEERE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT ENGINE AND METHOD OF OPERATING SAME
- Publication number 20200386405
- Publication date Dec 10, 2020
- Pratt & Whitney Canada Corp.
- David MENHEERE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT ENGINE AND METHOD OF OPERATION THEREOF
- Publication number 20200386406
- Publication date Dec 10, 2020
- Pratt & Whitney Canada Corp.
- Timothy REDFORD
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH POWER TURBINE DRIVEN BOOST COMPRESSOR
- Publication number 20200240327
- Publication date Jul 30, 2020
- Pratt & Whitney Canada Corp.
- David MENHEERE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH DIFFERENTIAL GEARBOX
- Publication number 20200141326
- Publication date May 7, 2020
- Pratt & Whitney Canada Corp.
- Tim REDFORD
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
AUXILIARY POWER UNIT
- Publication number 20200141327
- Publication date May 7, 2020
- Pratt & Whitney Canada Corp.
- Tim REDFORD
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Santo CHIAPPETTA

Person

Patents Grantslast 30 patents

Gas turbine engine with variable speed output

Axial inertial particle separator for turbine engine

Aircraft and method of operating same

System and method for increasing bleed air flow to a heat exchanger...

Inertial particle separator for turbine engine

System and method for conditioning a fluid using bleed air from a b...

Gas turbine engine with differential gearbox

Patents Applicationslast 30 patents

AIRCRAFT AND METHOD OF OPERATING SAME

INERTIAL PARTICLE SEPARATOR FOR TURBINE ENGINE

AXIAL INERTIAL PARTICLE SEPARATOR FOR TURBINE ENGINE

GAS TURBINE ENGINE WITH VARIABLE SPEED OUTPUT

SYSTEM AND METHOD FOR CONDITIONING A FLUID USING BLEED AIR FROM A B...

SYSTEM AND METHOD FOR INCREASING BLEED AIR FLOW TO A HEAT EXCHANGER...

AIRCRAFT ENGINE AND METHOD OF OPERATION THEREOF

AIRCRAFT ENGINE AND METHOD OF OPERATION THEREOF

AIRCRAFT ENGINE AND METHOD OF OPERATING SAME

AIRCRAFT ENGINE AND METHOD OF OPERATION THEREOF

GAS TURBINE ENGINE WITH POWER TURBINE DRIVEN BOOST COMPRESSOR

GAS TURBINE ENGINE WITH DIFFERENTIAL GEARBOX

AUXILIARY POWER UNIT