CARLOS JAVIER FIGUEROA
Pilots at Congress Ave, West Palm Beach, FL
License number
Florida A4832233
Issued Date
Jul 2013
Expiration Date
Jul 2014
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
2000 N Congress Ave LOT 137, West Palm Beach, FL 33409
Professional information
President Owner At American Eagle Loan Restructuring Inc.
Position:
Owner at American Eagle Loan Modification Inc., President Owner at American Eagle Loan Restructuring Inc., Owner at American Eagle Loan Modification Inc.
Location:
West Palm Beach, Florida Area
Industry:
Financial Services
Work:
American Eagle Loan Modification Inc.
since Sep 2008
-
Owner
American Eagle Loan Restructuring Inc.
since Aug 2006
-
President Owner
American Eagle Loan Modification Inc.
since Oct 1998
-
Owner
Homekey Mortgage
Jan 1998 - Dec 2003
-
Senior Loan Consultant
Education:
Suffolk County Community College 1984 - 1985
Interests:
Looking for prospective clients that need their home mortgage modifyied
Do You Want To Save Your Home ?
Position:
Owner at American Eagle Loan Mod Inc., PRESIDENT / OWNER at American Eagle Loan Modification Inc.
Location:
West Palm Beach, Florida Area
Industry:
Financial Services
Work:
American Eagle Loan Mod Inc.
-
Owner
American Eagle Loan Modification Inc.
since Aug 2008
-
PRESIDENT / OWNER
Interests:
Help people to stay at their homes, by dealing with banks and get for my clients a reduction in monthly payments.
Honor & Awards:
Top Producer two years in a row at "Home Key Mortgage", Ronkonkoma, NY.
Owner At American Eagle Loan Mod. Inc
Position:
Owner at American Eagle Loan Mod. Inc
Location:
West Palm Beach, Florida Area
Industry:
Financial Services
Work:
American Eagle Loan Mod. Inc
-
Owner
Owner, American Eagle Loan Mod.
Position:
Owner at AMERICAN EAGLE LOAN MOD.
Location:
West Palm Beach, Florida Area
Industry:
Financial Services
Work:
AMERICAN EAGLE LOAN MOD.
-
Owner
Self-Aligning Liner Support Hanger
US Patent:
7861535, Jan 4, 2011
Filed:
Sep 24, 2007
Appl. No.:
11/903670
Inventors:
Carlos G. Figueroa - Wellington FL, US
Jeffrey S. Smith - Storrs CT, US
Russell Nachtman - Jupiter FL, US
Robert K. Hon - Palm Beach Gardens FL, US
Jeffrey S. Smith - Storrs CT, US
Russell Nachtman - Jupiter FL, US
Robert K. Hon - Palm Beach Gardens FL, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02C 7/20
US Classification:
60796, 60766
Abstract:
A self-aligning hanger for use in a gas turbine engine exhaust system comprises a first bracket, a second bracket, a rod, a first ball joint and a second ball joint. The first bracket is for connecting to an exhaust duct of the gas turbine exhaust system. The second bracket is for connecting to an exhaust duct liner of the gas turbine exhaust system. The rod extends between the first bracket and the second bracket. The first ball joint connects a first end of the rod with the first bracket. The second ball joint connects a second end of the rod with the second bracket.
Forced Air Cooled Gas Turbine Exhaust Liner
US Patent:
5755093, May 26, 1998
Filed:
May 1, 1995
Appl. No.:
8/431542
Inventors:
Mark E. Palusis - Jupiter FL
Carlos G. Figueroa - Wellington FL
Daniel C. Friedberg - Juno Beach FL
Debora F. Kehret - Jupiter FL
Carlos G. Figueroa - Wellington FL
Daniel C. Friedberg - Juno Beach FL
Debora F. Kehret - Jupiter FL
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02K 182, F02K 100
US Classification:
60266
Abstract:
The exhaust in a gas turbine engine is lined with stacks of hollow cooling blocks made of a composite material. Air is pumped into each stack and escapes into the exhaust flow from a slot between the blocks in each stack. In addition, the blocks contain passages so that some of the airflow escapes to a space between the stacks. The blocks are attached using special fasteners that does not create mechanical stresses on the composite material.
Attaching Brittle Composite Structures In Gas Turbine Engines For Resiliently Accommodating Thermal Expansion
US Patent:
5592814, Jan 14, 1997
Filed:
Dec 21, 1994
Appl. No.:
8/360937
Inventors:
Mark E. Palusis - Jupiter FL
Carlos G. Figueroa - Wellington FL
Daniel C. Friedberg - Juno Beach FL
Gary D. Jones - Jensen Beach FL
Gunther Eichhorn - Palm Beach Gardens FL
Carlos G. Figueroa - Wellington FL
Daniel C. Friedberg - Juno Beach FL
Gary D. Jones - Jensen Beach FL
Gunther Eichhorn - Palm Beach Gardens FL
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02C 720
US Classification:
60271
Abstract:
Two composite parts, such as sheet and a hollow gas turbine liner tile, are fastened together using a fastening system that includes a journal bearing that fits in a bore in the sheet and springs to support a bolt fastener that is tightened to hold the parts together. Resilient spacers are placed between the sheet and the liner. The springs may comprise a stack of rings, each ring being a tightly wound helical spring, giving the ring a hollow cross section and resilient qualities.
Brittle Composite Structure For Resiliently Accomodating Thermal Expansion
US Patent:
6102610, Aug 15, 2000
Filed:
Oct 7, 1996
Appl. No.:
8/726978
Inventors:
Mark E. Palusis - Jupiter FL
Carlos G. Figueroa - Wellington FL
Daniel C. Friedberg - Juno Beach FL
Gary D. Jones - Jensen Beach FL
Gunther Eichhorn - Palm Beach Gardens FL
Carlos G. Figueroa - Wellington FL
Daniel C. Friedberg - Juno Beach FL
Gary D. Jones - Jensen Beach FL
Gunther Eichhorn - Palm Beach Gardens FL
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F16B 502
US Classification:
403388
Abstract:
Two composite parts, such as sheet and a hollow gas turbine liner tile, are fastened together using a fastening system that includes a journal bearing that fits in a bore in the sheet and springs to support a bolt fastener that is tightened to hold the parts together. Resilient spacers are placed between the sheet and the liner. The springs may comprise a stack of rings, each ring being a tightly wound helical spring, giving the ring a hollow cross section and resilient qualities.
Flow Sleeve Impingement Cooling Baffles
US Patent:
2013000, Jan 3, 2013
Filed:
Jul 19, 2012
Appl. No.:
13/553076
Inventors:
Jaisukhlal V. Chokshi - Palm Beach Gardens FL, US
Craig F. Smith - Ashford CT, US
Carlos G. Figueroa - Wellington FL, US
Larry C. George - Jupiter FL, US
Craig F. Smith - Ashford CT, US
Carlos G. Figueroa - Wellington FL, US
Larry C. George - Jupiter FL, US
Assignee:
UNITED TECHNOLOGIES CORPORATION - Hartford CT
International Classification:
F02C 7/00, F23R 3/26
US Classification:
60755
Abstract:
A combustor assembly for a turbine engine includes a combustor liner, a flow sleeve and a baffle ring. The flow sleeve surrounds the combustor liner. An annulus is formed between the flow sleeve and the combustor liner. A plurality of row of cooling holes are formed in the flow sleeve. The baffle ring radially surrounds the combustor liner and is located in the annulus.
Flow Sleeve Impingement Cooling Baffles
US Patent:
8291711, Oct 23, 2012
Filed:
Jul 25, 2008
Appl. No.:
12/179671
Inventors:
Jaisukhlal V. Chokshi - Palm Beach Gardens FL, US
Craig F. Smith - Ashford CT, US
Carlos G. Figueroa - Wellington FL, US
Larry C. George - Jupiter FL, US
Craig F. Smith - Ashford CT, US
Carlos G. Figueroa - Wellington FL, US
Larry C. George - Jupiter FL, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02C 1/00
US Classification:
60772, 60758, 60760
Abstract:
A combustor assembly for a turbine engine includes a combustor liner, a flow sleeve and a baffle ring. The flow sleeve surrounds the combustor liner. An annulus is formed between the flow sleeve and the combustor liner. A plurality of row of cooling holes are formed in the flow sleeve. The baffle ring radially surrounds the combustor liner and is located in the annulus.