Christopher J Hanlon from Philadelphia, PA, age 59

Us Patents

Turbofan Gas Turbine Engine With Combusted Compressor Bleed Flow
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US Patent:

20220356840, Nov 10, 2022
Filed:

May 6, 2021
Appl. No.:

17/313605
Inventors:

- Farmington CT, US
Daniel Bernard Kupratis - Wallingford CT, US
Christopher J. Hanlon - Sturbridge MA, US
International Classification:

F02C 7/052
Abstract:

A gas turbine engine includes a core section including a compressor, a main combustor, and a main turbine. Combustion products from the main combustor drive rotation of the turbine and the compressor. A power turbine is fluidly connected to the main turbine and driven by exhaust from the main turbine. The gas turbine engine further includes a fan section having a fan rotor located fluidly upstream of the core section. The power turbine is operably connected to the fan rotor to drive rotation of the fan rotor via rotation of the power turbine. The gas turbine engine includes a bleed arrangement having one or more bleed passages configured to divert a bleed airflow from the compressor around the main combustor and main turbine, and reintroduce the bleed airflow into the power turbine.

Multi-Engine Architecture With Linkages To Multiple Spools
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US Patent:

20200032702, Jan 30, 2020
Filed:

Jun 4, 2019
Appl. No.:

16/431271
Inventors:

- Farmington CT, US
Neil Terwilliger - Meriden CT, US
Christopher J. Hanlon - Sturbridge MA, US
International Classification:

F02C 3/06
F02C 6/06
F02C 7/32
F02C 7/36
Abstract:

An aircraft gas turbine engine system comprises first and second gas turbine engines. The first gas turbine engine has first and second spools. A first power linkage connects the second gas turbine engine to the first spool of the gas turbine engine, and a second power linkage connects the second gas turbine engine to the second spool of the first gas turbine engine.

Turbofan With Bleed Supercharged Auxiliary Engine
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US Patent:

20190368417, Dec 5, 2019
Filed:

Jun 4, 2019
Appl. No.:

16/431259
Inventors:

- Farmington CT, US
Daniel Bernard Kupratis - Wallingford CT, US
Christopher J. Hanlon - Sturbridge MA, US
International Classification:

F02C 6/08
F02C 6/02
F02C 9/18
F02C 7/143
F02C 7/36
F02C 3/04
H02K 7/20
H02K 7/18
Abstract:

An aircraft gas turbine engine system comprises first and second gas turbine engines connected by an inter-engine gas path. The first gas turbine engine has a first spool with a first compressor section, and a second spool with a second compressor section downstream of and rotationally independent from the first compressor section. The second gas turbine engine is configured to provide power to at least one of the first and second spools of the first gas turbine engine. The inter-engine gas path is disposed to receive gas flow bled from a bleed location in the first gas turbine engine downstream of the first compressor section, and to supply this gas flow to an inlet of the second gas turbine engine.

Hybrid Electric Fan With Stall Free Low Pressure Compressor
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US Patent:

20190353104, Nov 21, 2019
Filed:

May 16, 2018
Appl. No.:

15/980870
Inventors:

- Farmington CT, US
Christopher J. Hanlon - Sturbridge MA, US
William G. Sheridan - Southington CT, US
International Classification:

F02C 7/36
F02C 6/00
F02C 9/00
F16H 1/28
F02K 3/06
H02K 7/14
H02K 7/116
H02K 7/18
Abstract:

A gas turbine engine according to an exemplary embodiment of this disclosure includes among other possible things, a fan section including a plurality of fan blades, a first electric motor assembly that provides a first drive input for driving the fan blades about an axis, a turbine section, and a geared architecture driven by the turbine section and coupled to the fan section to provide a second drive input for driving the fan blades, and second electric motor assembly is coupled to rotate the geared architecture relative to a fixed structure controls a speed of the fan blades provided by a combination of the first drive input and the second drive input.

Electric Heating For Turbomachinery Clearance Control
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US Patent:

20190345835, Nov 14, 2019
Filed:

May 14, 2018
Appl. No.:

15/979085
Inventors:

- Farmington CT, US
Christopher J. Hanlon - Sturbridge MA, US
Patrick D Couture - Tolland CT, US
Coy Bruce Wood - Ellington CT, US
Assignee:

UNITED TECHNOLOGIES CORPORATION - Farmington CT
International Classification:

F01D 11/24
Abstract:

A clearance control system for a gas turbine engine may comprise a rotor blade, an outer structure disposed radially outward from the rotor blade, and a heating element configured to cause the outer structure to be heated in response to electric current being supplied to the heating element, wherein a gap between the rotor blade and the outer structure is at least one of increased, decreased, and maintained in response to the outer structure being heated.

Turbine Clearance Control System And Method For Improved Variable Cycle Gas Turbine Engine Fuel Burn
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US Patent:

20190048796, Feb 14, 2019
Filed:

Jul 30, 2018
Appl. No.:

16/048738
Inventors:

- Farmington CT, US
Scott A. Carr - Manchester CT, US
Christopher J. Hanlon - Sturbridge MA, US
Peter A. White - West Hartford CT, US
Theodore W. Hall - Berlin CT, US
John R. Farris - Bolton CT, US
Andrew S. Miller - Marlborough CT, US
Christopher W. Robak - Manchester CT, US
David C. Pimenta - Rocky Hill CT, US
David Richard Griffin - Tolland CT, US
Assignee:

United Technologies Corporation - Farmington CT
International Classification:

F02C 3/055
F02C 7/18
F01D 11/24
Abstract:

A method of assembling a gas turbine engine includes setting a build clearance at assembly in response to a running tip clearance defined with a cooled cooling air. A method of operating a gas turbine engine includes supplying a cooled cooling air to a high pressure turbine in response to an engine rotor speed.

High Efficiency Aircraft Parallel Hybrid Gas Turbine Electric Propulsion System
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US Patent:

20180003071, Jan 4, 2018
Filed:

Jul 1, 2016
Appl. No.:

15/200128
Inventors:

- Farmington CT, US
Christopher J. Hanlon - Sturbridge MA, US
Larry W. Hardin - East Hartford CT, US
Jonathan Rheaume - West Hartford CT, US
International Classification:

F01D 15/10
F02C 6/14
F02K 3/06
B64D 27/10
F02C 7/36
F02C 3/04
Abstract:

A gas turbine engine includes a compressor section having a first compressor and a second compressor, the second compressor having a higher pressure than the first compressor, and a turbine section having a first turbine and a second turbine, the second turbine having a higher pressure than the first turbine. The first compressor is connected to the first turbine via a first shaft. The second compressor is connected to the second turbine via a second shaft. An electric motor is connected to the first shaft such that rotational energy generated by the electric motor is translated to the first shaft. A fan is connected to the first shaft via a gear system. The gas turbine engine includes at least a takeoff mode of operations, a top of climb mode of operations and a maximum cruise mode of operations. The gas turbine engine is sized to operate at peak efficiency in the maximum cruise mode of operations.

Turbine Clearance Control System And Method For Improved Variable Cycle Gas Turbine Engine Fuel Burn
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US Patent:

20170328231, Nov 16, 2017
Filed:

Mar 6, 2015
Appl. No.:

14/640060
Inventors:

- Hartford CT, US
Scott A. Carr - Manchester CT, US
Christopher J. Hanlon - Sturbridge MA, US
Peter A. White - West Hartford CT, US
Theodore W. Hall - Berlin CT, US
John R. Farris - Bolton CT, US
Andrew S. Miller - Marlborough CT, US
Christopher W. Robak - Manchester CT, US
David C. Pimenta - Rocky Hill CT, US
David Richard Griffin - Tolland CT, US
International Classification:

F01D 11/24
F02C 7/18
Abstract:

A method of assembling a gas turbine engine includes setting a build clearance at assembly in response to a running tip clearance defined with a cooled cooling air. A method of operating a gas turbine engine includes supplying a cooled cooling air to a high pressure turbine in response to an engine rotor speed.

Resumes

Realtor At Re/Max Edge Realty

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Location:

United States

Senior Catastrophe Modeler

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Location:

Philadelphia, PA

Industry:

Insurance

Work:

Jlt Re Apr 2017 - Jul 2017
Assistant Vice President, Catastrophe Modeling
Chubb Apr 2017 - Jul 2017
Senior Catastrophe Modeler
Jlt Re Jul 2014 - Apr 2017
Catastrophe Modeling Consultant
Penn State University Jun 2011 - Dec 2015
Research Assistant

Education:

Penn State University 2011 - 2014
Doctorates, Doctor of Philosophy, Meteorology, Philosophy Penn State University 2007 - 2011
Bachelors, Bachelor of Science, Energy, Business, Meteorology, Finance

Skills:

Microsoft Office
Matlab
Data Analysis
Statistics
Fortran
Meteorology
Research
Risk Management
Analysis
Microsoft Excel
Science

Executive Director

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Location:

Philadelphia, PA

Industry:

Non-Profit Organization Management

Work:

Ccsa Foundation
Executive Director
Community Education Alliance of West Philadelphia
Executive Director
Beat the Streets Philadelphia Jul 2010 - Feb 2017
Executive Director
Franklin Financial Group Jun 2005 - Jul 2010
Employee Benefits Broker
Penn Grapplers Club Jun 2005 - Jul 2010
Board Member

Education:

University of Pennsylvania 1999 - 2004

Founder, Creative Director Of Hanlon Creative

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Location:

1744 Sumneytown Pike, Kulpsville, PA 19443

Industry:

Marketing And Advertising

Work:

Earle Palmer Brown May 1996 - Jan 2000
Senior Art Director
Hanlon Creative May 1996 - Jan 2000
Founder, Creative Director of Hanlon Creative
Brownstein Group Nov 1993 - May 1996
Art Director

Education:

University of Delaware 1989 - 1993
Bachelors, Bachelor of Science, Visual Communications, Design, Advertising

Skills:

Advertising
Creative Direction
Art Direction
Branding and Identity
Email Marketing
Creative Strategy
Adobe Creative Suite
Corporate Branding
Integrated Marketing
Social Media Marketing
Web Design
Logo Design
Graphic Design
Marketing Strategy
Social Media
Marketing Communications
Corporate Identity
Indesign
Typography
Copywriting
Online Advertising
Direct Mail
Graphics
Brochures
Website Development
Project Management
Layout
Concept Development
Photoshop
Powerpoint
Customer Service
Packaging
Posters
Interactive Advertising
Information Architecture
User Experience
User Interface Design
Interactive Marketing
Outdoor Advertising
Image Manipulation
Illustrator
Interaction Design
Visual Communication
Brand Implementation
Microsoft Office
Microsoft Excel
Collateral
Creative Services
Quarkxpress
Catalogs

Interests:

Children

Creative Director And Partner

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Location:

Norristown, PA

Industry:

Marketing And Advertising

Work:

Hanlon Creative
Creative Director and Partner

Education:

University of Delaware Sep 1989 - May 1993
Bachelors, Bachelor of Science, Visual Communications

Christopher Hanlon

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Location:

Philadelphia, PA

Work:

Liberty University
Student

Christopher Hanlon

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Location:

United States

Telecommunications Consultant And Professional

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Location:

Greater Philadelphia Area

Industry:

Telecommunications

Medicine Doctors

Christopher T. Hanlon

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Specialties:

Anesthesiology

Work:

University Of Florida Anesthesia
1600 SW Archer Rd, Gainesville, FL 32610
(352)2650077 (phone), (352)2656922 (fax)

Education:

Medical School
University of Alabama School of Medicine
Graduated: 2011

Languages:

English

Description:

Dr. Hanlon graduated from the University of Alabama School of Medicine in 2011. He works in Gainesville, FL and specializes in Anesthesiology. Dr. Hanlon is affiliated with UF Health Shands Hospital.

Christopher Thomas Hanlon

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Specialties:

Surgery

Christopher John Hanlon

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Specialties:

Internal Medicine
Sports Medicine

Education:

State University of New York Downstate (1986)

Name / Title

Company / Classification

Phones & Addresses

Christopher J. Hanlon

PERSONAL PROTECTION 1ST LLC

Christopher J. Hanlon
President

Resort at Singer Island Properties, Inc

Christopher J. Hanlon
President, Director

Wci Ireland Inn Corp
Residential Construction

Christopher J. Hanlon
President, President, Director

Jyc Holdings, Inc
Subdivider/Developer

(239)9472600

Christopher J. Hanlon
Director

Wci Towers Northeast U.S., Inc

Christopher J. Hanlon
President, Director

Pelican Landing Properties, Inc

Christopher J. Hanlon
Director, Vice President

The Colony at Pelican Landing Golf Club, Inc

Christopher J. Hanlon
President, Director

Wci Towers, Inc
Residential Construction

Amazon

America's England: Antebellum Literature and Atlantic Sectionalism (Oxford Studies in American Literary History)

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The wealth of transatlantic scholarship to emerge in recent years has greatly enriched our understanding of the mutual, far-reaching cultural exchange between Great Britain and the United States. Yet scholars often lose sight of this relationship in the years immediately leading up to the outbreak o...

Author
Christopher Hanlon

Binding
Hardcover

Pages
256

Publisher
Oxford University Press

ISBN #
0199937583

EAN Code
9780199937585

ISBN #
2

America's England: Antebellum Literature and Atlantic Sectionalism (Oxford Studies in American Literary History) by Hanlon Christopher (2013-04-01) Hardcover

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Author
Hanlon Christopher

Binding
Hardcover

ISBN #
6

America's England: Antebellum Literature and Atlantic Sectionalism (Oxford Studies in American Literary History) 1st edition by Hanlon, Christopher (2013) Hardcover

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Author
Christopher Hanlon

Binding
Hardcover

Publisher
Oxford University Press

ISBN #
5

Scholar Intellectuals in Early Modern India: Discipline, Sect, Lineage and Community (Routledge South Asian History and Culture Series)

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In recent years, scholars from a wide range of disciplines have examined the revival in intellectual and literary cultures that took place during India’s ‘early modern’ centuries. This was both a revival as well as a period of intense disputation and critical engagement. It took in the relationship ...

Binding
Hardcover

Pages
202

Publisher
Routledge

ISBN #
1138905704

EAN Code
9781138905702

ISBN #
7