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Patrick M Pilapil

from Kissimmee, FL
Age ~48
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Also known as:
Patrick Manila Pilapil, Patrick S Pilapil
Phone and address:
2654 Hawthorne Ln, Kissimmee, FL 34743
(407) 962-0854
Related to:
Lennies M Simon, 74Erika Camille Broomes, 32Catherine P Ramos, 66Jasmin M Pilapil, 68Noemi P Fouces, 69Marina PilapilSegundo S Pilapil, 75Frederick M Pilapil, 45Beatriz P Broomes, 60
Connected to:
Amelita R Pilapil, 65Christina V Pilapil, 37Jan M Pilapil, 31Josephine C Pilapil, 61Joy A Pilapil, 36Norman J Pilapil, 53Rommel Pilapil, 40Alberto Pilar, 73Cesar A Pilar, 45Danilo P Pilar, 73

Patrick Pilapil Phones & Addresses

  • 2654 Hawthorne Ln, Kissimmee, FL 34743 (407) 962-0854
  • Ocean, NJ
  • Neptune, NJ

Work

Position: Professional/Technical

Emails

p***[email protected]

Resumes

Resumes

Patrick Pilapil Photo 1

Finance Manager

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Location:
2654 Hawthorne Ln, Kissimmee, FL 34743
Industry:
Financial Services
Work:
Western Union
Finance Manager
Metro Pacific Tollways Corporation Jun 1, 2010 - Jun 2014
Associate Finance Manager
Western Union Jun 1, 2010 - Jun 2014
Senior Financial Analyst
Manila North Tollways Corporation Jun 2007 - Jun 2010
Senior Corporate Finance Specialist
Ibm Nov 2004 - May 2005
Accounts Payable and Tax Analyst
Education:
University of the Philippines 1998 - 2003
Bachelors, Bachelor of Science, Business Administration, Accountancy
Skills:
Financial Modeling
Financial Reporting
Variance Analysis
Managerial Finance
Business Development
Enterprise Risk Management
Accounting
Corporate Finance
Financial Analysis
Budget Forecasts
Financial Audits
Valuation
Analysis
Financial Accounting
Interests:
Casinos
Exercise
Home Improvement
Reading
Sports
Collecting Coins
Cooking
Gardening
Cruises
Electronics
Environment
Education
Fitness
Music
Movies
Collecting
Diet
Poverty Alleviation
Disaster and Humanitarian Relief
Travel
Investing
Traveling
Arts and Culture
Languages:
English
Filipino
Patrick Pilapil Photo 2

Patrick Pilapil

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Patrick Pilapil Photo 3

Patrick Pilapil

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Publications

Us Patents

Gas Turbine Seal Arrangement

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US Patent:
20180223683, Aug 9, 2018
Filed:
Jul 20, 2015
Appl. No.:
15/743117
Inventors:
- Orlando FL, US
Abdullatif M. Chehab - Chuluota FL, US
Patrick M. Pilapil - Kissimmee FL, US
Yan Yin - Oviedo FL, US
Christian Xavier Campbell - Charlotte NC, US
Vincent Paul Laurello - Hobe Sound FL, US
International Classification:
F01D 11/00
F01D 11/02
Abstract:
A turbine arrangement including a rotor and a stator surrounding the rotor and comprising guide vane segments, each guide vane segment comprising an airfoil and a radially inner vane platform. A seal arrangement includes a static seal inward from the inner vane platforms and having a radially extending face plate, first and second cylindrical seal walls extending from outer and inner ends of the annular face plate, an annular seal plate extending radially from the second cylindrical seal wall, and an angel wing extending between the first cylindrical seal wall and the annular seal plate to define a first annular cavity and a second annular cavity. Circumferentially spaced cut-outs define passages through the annular seal plate between the first and second annular cavities and are aligned with fasteners that attach the annular face plate to a support ring for supporting the inner vane platform.

Interstage Seal Housing Optimization System In A Gas Turbine Engine

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US Patent:
20170145847, May 25, 2017
Filed:
Aug 8, 2014
Appl. No.:
15/325527
Inventors:
- Orlando FL, US
Patrick M. Pilapil - Kissimmee FL, US
Yan Yin - Oviedo FL, US
Joshua D. Kovac - Oviedo FL, US
International Classification:
F01D 11/00
F01D 25/26
F01D 11/02
Abstract:
An interstage seal system () for adjusting the position of an interstage seal during operation of a gas turbine engine () to increase efficiency of the seal () is disclosed. The interstage seal system () may include a interstage seal housing () formed from a circumferentially extending housing having a seal () positioned on a radially inward surface () of the interstage seal housing (). The interstage seal housing () may biased radially outward via one or more springs () to bias the radially inward surface () of the interstage seal housing () outwardly. The interstage seal housing () may reside in an interstage housing receiving cavity (). The cavity () may be supplied with gases at a higher pressure than on the other side () of the seal housing () during turbine engine operation. As such, the interstage seal housing () is forced radially inwardly to close the gap () within the seal () as the high pressure force directed radially inward overcomes the spring bias directed radially outward.

Turbine Engine Shutdown Temperature Control System

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US Patent:
20140321981, Oct 30, 2014
Filed:
Apr 26, 2013
Appl. No.:
13/871080
Inventors:
Jose L. Rodriguez - Lake Mary FL, US
David A. Little - Chuluota FL, US
Jiping Zhang - Winter Springs FL, US
Patrick M. Pilapil - Kissimmee FL, US
International Classification:
F01D 11/24
US Classification:
415116
Abstract:
A turbine engine shutdown temperature control system configured to foster consistent air temperature within cavities surrounding compressor and turbine blade assemblies to eliminate turbine and compressor blade tip rub during warm restarts of gas turbine engines is disclosed. The turbine engine shutdown temperature control system may include one or more air amplifiers positioned in a turbine case. An exhaust outlet of the air amplifier may extend into a cavity created by a turbine case and may be configured to exhaust air in a generally circumferential direction to entrain air within the cavity to flow circumferentially to establish a consistent air temperature within the cavity thereby preventing uneven cooling of turbine engine components after shutdown and prevent damage to turbine components during a warm restart.
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Patrick M Pilapil from Kissimmee, FL, age ~48 Get Report