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Joseph D Rainville, 40Killeen, TX

Joseph Rainville Phones & Addresses

Fort Hood, TX   

397 Zurich Ct, Clarksville, TN 37040    817-4879765   

Kansas City, MO   

2309 S Main St, Cleburne, TX 76033    817-9336237   

Fort Richardson, AK   

Mentions for Joseph D Rainville

Career records & work history

License Records

Joseph M Rainville

Licenses:
License #: EMT07907 - Active
Category: Emergency Medical Services
Issued Date: Jun 7, 2002
Expiration Date: Dec 31, 2018
Type: Emergency Medical Technician

Publications & IP owners

Us Patents

Fuel Cell Cathode Air Pressure Management Systems

US Patent:
2022039, Dec 8, 2022
Filed:
Jun 4, 2021
Appl. No.:
17/339572
Inventors:
- Fort Worth TX, US
Joseph Dean Rainville - Fort Worth TX, US
Assignee:
Bell Textron Inc. - Fort Worth TX
International Classification:
H01M 8/04746
H01M 8/0438
H01M 8/04111
B64D 41/00
B60L 50/70
B60L 58/30
Abstract:
A method of operating an aircraft includes providing a fuel cell system to power the aircraft, providing an airflow path through the fuel cell system, sensing a change mass air flow rate supplied to a compressor of the fuel cell system, and at least one of adjusting a restriction of airflow entering the airflow path in response to the sensed change in mass air flow rate, adjusting a restriction of airflow exiting the airflow path in response to the sensed change in mass air flow rate, and adjusting an air scoop to gather a different amount of air into the airflow path. A method of operating an aircraft includes sensing a change in ambient pressure supplied to an airflow path and adjusting a restriction of airflow exiting the airflow path in response to a sensed change in ambient pressure.

Fuel Cell Powered Aircraft With A Cathode Convertible Between Oxygen And Air And Method For Use Thereof

US Patent:
2022028, Sep 15, 2022
Filed:
May 31, 2022
Appl. No.:
17/829191
Inventors:
- Providence RI, US
Joseph Dean Rainville - Fort Worth TX, US
Assignee:
Textron Innovations Inc. - Providence RI
International Classification:
B64D 31/00
H01M 8/04082
H01M 8/04746
H01M 8/04313
B64D 33/08
B64C 39/02
B60L 58/33
B60L 58/00
B64D 27/24
H01M 8/04029
Abstract:
An aircraft that includes a fuselage, an electric motor driven propulsion system, and a fuel cell system configured to provide electricity to the electric motor. The fuel cell system includes a fuel cell, a hydrogen tank, an oxygen tank, an air channel, and a cathode switch. The cathode switch being configured to convert between an air mode, wherein the fuel cell operates utilizing air from the air channel, and an oxygen mode, wherein the fuel cell operates utilizing oxygen from the oxygen tank.

Air-Cooled Fuel-Cell Freeze-Protection System

US Patent:
2020038, Dec 10, 2020
Filed:
Jun 9, 2019
Appl. No.:
16/435546
Inventors:
- Fort Worth TX, US
Joseph D. Rainville - Fort Worth TX, US
Assignee:
Bell Helicopter Textron Inc. - Fort Worth TX
International Classification:
H01M 8/04223
H01M 8/04014
H01M 8/04007
H01M 8/04701
H01M 8/04992
B64D 41/00
B64C 39/02
Abstract:
An air-cooled fuel-cell freeze-protection system for a rotorcraft using a controller to vary a heating system for an air-cooled fuel cell. The heating system heats supply air for the air-cooled fuel cell, and a butterfly valve varies a pressure of the supply air to the air-cooled fuel cell. The heating system can be an electric heater, a heat exchanger, or a combination of heater and heat exchanger.

Fuel Cells Configured To Deliver Bi-Polar High Voltage Dc Power

US Patent:
2020023, Jul 30, 2020
Filed:
Jan 25, 2019
Appl. No.:
16/257726
Inventors:
- Fort Worth TX, US
Joseph Dean Rainville - Fort Worth TX, US
Assignee:
Bell Helicopter Textron Inc. - Fort Worth TX
International Classification:
B64D 27/24
B64C 27/04
H01M 8/04537
H01M 8/04858
B64D 41/00
Abstract:
A fuel-cell system at 540 VDC for powering an electrical load of a rotorcraft with a first fuel cell and a second fuel cell. Each fuel cell is configured identically and features a positive electrical node and a negative electrical node. Each fuel cell is configured to provide one half of the electrical load of the rotorcraft and one half of the voltage of the electrical load.

Fuel Cell Stack Array

US Patent:
2020023, Jul 30, 2020
Filed:
Jan 25, 2019
Appl. No.:
16/257750
Inventors:
- Fort Worth TX, US
Joseph Dean Rainville - Fort Worth TX, US
Assignee:
Bell Helicopter Textron Inc. - Fort Worth TX
International Classification:
B64D 27/24
H01M 8/04537
H01M 8/04858
H01M 8/04664
B64C 27/04
B64D 41/00
Abstract:
A stack fuel cell array featuring paired fuel-cell systems combined to generate 540 VDC for a rotorcraft. Power from the hydrogen-based fuel cells is provided to the rotorcraft. A rated electrical load of the rotorcraft helps determine how many paired fuel-cell systems are needed during any fuel-cell systems failures. Each of the paired fuel-cell systems is coupled to an electrical load of the rotorcraft. The system detects any fuel cell failures and removes other working fuel cells as needed to balance the electrical system.

Thermal Management System

US Patent:
2020023, Jul 30, 2020
Filed:
Jan 30, 2019
Appl. No.:
16/262059
Inventors:
- Fort Worth TX, US
Joseph Dean Rainville - Fort Worth TX, US
Assignee:
Bell Helicopter Textron Inc. - Fort Worth TX
International Classification:
B64D 33/08
H01M 8/04007
B64C 27/28
B64C 27/20
B64C 27/26
Abstract:
A thermal management system includes a plurality of passages through a leading edge of a component of an aircraft. The thermal management system is configured to circulate coolant from a heat source through the plurality of passages in order to maximize heat transfer from the coolant to the airflow passing over the leading edge.

Fuel Cell Powered Aircraft With A Cathode Convertible Between Oxygen And Air And Method For Use Thereof

US Patent:
2020018, Jun 11, 2020
Filed:
Dec 10, 2018
Appl. No.:
16/214735
Inventors:
- Fort Worth TX, US
Joseph Dean Rainville - Fort Worth TX, US
Assignee:
Bell Helicopter Textron Inc. - Fort Worth TX
International Classification:
B64D 31/00
H01M 8/04082
H01M 8/04746
H01M 8/04313
B64C 39/02
B64D 33/08
Abstract:
An aircraft that includes a fuselage, an electric motor driven propulsion system, and a fuel cell system configured to provide electricity to the electric motor. The fuel cell system includes a fuel cell, a hydrogen tank, an oxygen tank, an air channel, and a cathode switch. The cathode switch being configured to convert between an air mode, wherein the fuel cell operates utilizing air from the air channel, and an oxygen mode, wherein the fuel cell operates utilizing oxygen from the oxygen tank.

Autonomous Hydrogen Refueling

US Patent:
2020018, Jun 11, 2020
Filed:
Dec 10, 2018
Appl. No.:
16/214765
Inventors:
- Fort Worth TX, US
Joseph Dean Rainville - Fort Worth TX, US
Assignee:
Bell Helicopter Textron Inc. - Fort Worth TX
International Classification:
B64F 1/28
B64D 37/30
Abstract:
A system and a method for autonomous hydrogen refueling of vertical lift aircraft using a landing pad with sensors, a hydrogen storage tank, a refueling arm configured to couple the hydrogen storage tank to the aircraft and a controller configured to control a flow of fuel from the hydrogen storage tank to the aircraft.

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