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Eric Charlton Phones & Addresses

  • 5307 Applewood Ln, Cedar Falls, IA 50613 (319) 404-8109
  • Waterloo, IA
  • 3445 Bell Ave, Chicago, IL 60618 (773) 281-0232
  • 4911 Kenmore Ave, Chicago, IL 60640 (773) 989-2214
  • 8215 Maloy Mnr, San Antonio, TX 78250 (210) 647-0543
  • Fort Worth, TX
  • Dallas, TX
  • San Diego, CA

Resumes

Resumes

Eric Charlton Photo 1

Eric Charlton

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Location:
Cedar Falls, IA
Industry:
Management Consulting
Work:
Pdcm Insurance
Financial Manager

Next Generation Wireless Apr 2008 - Oct 2010
Controller

Oneneck It Solutions Apr 2008 - Oct 2010
Controller and Associate Manager - Accounting

Clear Channel Mar 2006 - Apr 2008
Assistant Controller

Clear Channel Jun 2004 - Mar 2006
Broadcast Senior Accountant
Education:
Texas Christian University 1993 - 1997
Bachelor of Science, Bachelors, Bachelor of Business Administration, Business Management, Accounting
The University of Texas at San Antonio
Master of Business Administration, Masters
Skills:
Mathematics
Marketing Management
Team Building
Variance Analysis
Sec
Supplies
Market
Channel
Physical Inventory
Shipping
Expenses
Christian
Sales
Cost
Aging
Mentoring
Finance
San
Business Administration
Utilities
Savings
Monthly Close Process
Liability
Film
Texas
Sales Commission
Management
Revenue
Credit Management
Financial Statements
Railway
General Ledger
Data Research
Aggregate
Maintenance and Repair
Commissioned Art
Curriculum Development
Broadcast
Auditing
Powerpoint
Accounting
Percentage of Completion
Human Resources
Lecturing
Seminars
Forecasting
Entry
Cluster
Business Services
Construction Accounting
Publishing
Account Executives
Reports
Organizational Restructuring
Customer Events
Supervision
Managerial Economics
Account Reconciliation
Balance Sheet
Consolidation
Microsoft Office
Budgeting
Microsoft Excel
Risk Management
New Hire Training
Training
Policy
Customer Service
Progression
Radio
Intranet
Part Time
Documentation
Project Management
Streamlining
Research
Reporting
Accounts Payable
Capital
Microsoft
Visual Aids
Chicago
Amortization
Controller
Payroll
Analysis
Premiere
P&L
Financial Systems
Cpa
Yahoo
Coordination
Journal Entries
Star
Training Manuals
Event Planning
Applications
Managerial Finance
Month End
Communication
Detail
Advertising
Depreciation
Strategic Planning
Cost Savings
Miller
Radio Networks
Marketing
Corporate Liaison
Building Automation
Project Planning
Gaap
Sarbanes Oxley Act
Rollout
Contractual Agreements
Analytics
Accounts Receivable
Presentations
Income
Responsibility
Labor Issues
Contract Management
Executive Management
Budget
Teaching
Tax
Vendor Contracts
Disclosure
Guidelines
Plan Administration
San Diego
Compliance
Microsoft Word
Month End Close Process
Us Gaap
Organizational Behavior
Cash
Business Process
Internal Controls
Asset
Theory
Financial Analysis
Invoicing
Decision Making
Budgets
Financial Transactions
Financial Reporting
Staff Development
Problem Solving
Trading
Television
Evaluation
Databases
Interests:
Social Services
Health
Certifications:
Certified Public Accountant
Eric Charlton Photo 2

Consultant

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Location:
Cedar Falls, IA
Work:

Consultant
Education:
Texas Christian University
Eric Charlton Photo 3

Eric Charlton

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Eric Charlton Photo 4

Eric Charlton

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Publications

Wikipedia References

Eric Charlton Photo 5

Eric Charlton

Us Patents

System, Method And Apparatus For Windblast Reduction During Release Or Ejection From Aircraft

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US Patent:
20090321570, Dec 31, 2009
Filed:
Jun 25, 2008
Appl. No.:
12/145558
Inventors:
Mike I. Jones - Azle TX, US
Glenn W. Baird - Fort Worth TX, US
Eric F. Charlton - Grapevine TX, US
Assignee:
LOCKHEED MARTIN CORPORATION - Bethesda MD
International Classification:
B64D 25/115
B64D 1/12
US Classification:
244122AG, 2441374
Abstract:
The invention reduces the impact of flowfield forces on objects launched from high speed aircraft during flight. For example, the invention provides a solution for overcoming ejection windblast injuries to pilots and increases the probability of injury-free or low-injury ejection. The gas flow is used to rapidly create a very short duration protective “bubble” in the incoming air flow ahead of the ejecting pilot. The bubble reduces the local flow velocity and aerodynamic forces on the pilot during the injury-critical time period of ejection. The invention also is suitable for reducing the intensity of flowfield forces that act on released military aircraft ordnance, such as bombs and missiles.

Minimally Intrusive Wingtip Vortex Wake Mitigation Using Microvane Arrays

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US Patent:
20130146715, Jun 13, 2013
Filed:
Dec 13, 2011
Appl. No.:
13/324537
Inventors:
Neal D. Domel - Aledo TX, US
Eric F. Charlton - Grapevine TX, US
Daniel N. Miller - Bainbridge Island WA, US
Assignee:
Lockheed Martin Corroration - Bethesda MD
International Classification:
B64C 23/06
US Classification:
2441994, 2441992
Abstract:
An airfoil tip vortex mitigation arrangement comprising one or more flow directors configured and positioned to re-direct freestream air over a low pressure surface of an airfoil in such a way as to displace and weaken a main tip vortex generated at a tip of the airfoil.

Minimally Intrusive Wingtip Vortex Wake Mitigation Using Inside-Mold-Line Surface Modifications

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US Patent:
20130153711, Jun 20, 2013
Filed:
Dec 15, 2011
Appl. No.:
13/326592
Inventors:
Perry Wooden - Crowley TX, US
Ruble E. Moor - Burleson TX, US
Eric F. Charlton - Grapevine TX, US
Daniel N. Miller - Bainbridge Island WA, US
Edwin L. Blosch - Keller TX, US
Jeffrey J. Azevedo - Hudson Oaks TX, US
Assignee:
Lockheed Martin Corporation - Bethesda MD
International Classification:
B64C 23/06
US Classification:
2441992
Abstract:
An airfoil tip vortex mitigation device comprising an intake port disposed in a first surface of an airfoil and an exit port in fluid communication with the intake port and disposed in a second surface of the airfoil where air pressure is less than at the first surface when the airfoil is producing lift. The channel and exit port are positioned and configured to direct diverted air in such a way as to weaken an airfoil tip vortex that's produced by the airfoil when the airfoil is producing lift.

Adhesive Panels Of Microvane Arrays For Reducing Effects Of Wingtip Vortices

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US Patent:
20160272302, Sep 22, 2016
Filed:
Dec 12, 2014
Appl. No.:
14/569270
Inventors:
Brian T. Rosenberger - Aledo TX, US
Eric Frederick Charlton - Grapevine TX, US
Daniel N. Miller - Bainbridge Island TX, US
International Classification:
B64C 23/06
B64C 21/10
Abstract:
In one embodiment, a wing includes a low pressure side, a high pressure side opposite the low pressure side, and a drag reducing apparatus coupled to the low pressure using an adhesive. The drag reducing apparatus includes a first side coupled to the low pressure side of the wing, and a second side opposite the first side, the second side comprising a plurality of vortex generators arranged in an array configuration, the array configuration of vortex generators operable to weaken a wingtip vortex generated by the wing by generating one or more vane vortices near an end of the low pressure side of the wing.
Eric R Charlton from Cedar Falls, IA, age ~49 Get Report