Search

Mark Palusis Phones & Addresses

  • 15864 118Th Trl N, Jupiter, FL 33478 (561) 575-7580
  • 6190 Riverwalk Ln, Jupiter, FL 33458 (561) 747-9192
  • 22 Tattersall Ln, Florence, KY 41042 (859) 647-2836
  • Chicago, IL
  • Stuart, FL
  • Palm Beach, FL
  • 15864 118Th Ter N, Jupiter, FL 33478 (561) 575-7580

Work

Company: Parametric solutions, inc. Jan 2013 Position: Senior mechanical engineer

Education

School / High School: University of Illinois at Urbana - Champaign 1988 to 1989 Specialities: Aviation, Mechanical Engineering

Skills

Engineering • Project Management • Presentation Skills • Structural Analysis • 3D Modeling • Professional Mentoring

Emails

Industries

Aviation & Aerospace

Resumes

Resumes

Mark Palusis Photo 1

Senior Mechanical Engineer

View page
Location:
900 east Indiantown Rd, Jupiter, FL 33458
Industry:
Aviation & Aerospace
Work:
Parametric Solutions, Inc.
Senior Mechanical Engineer

Spiritech Advanced Products, Inc Nov 2002 - Dec 2012
Senior Mechanical Engineer

Engineering Evaluation & Design, Inc. Nov 2000 - Nov 2002
Senior Mechanical Engineer

Pratt & Whitney Jun 1989 - Nov 2000
Mechanical Design Engineer
Education:
University of Illinois at Urbana - Champaign 1988 - 1989
North Central College 1985 - 1988
Bachelors, Bachelor of Arts, Physics, Mechanical Engineering
Skills:
Engineering
Project Management
Presentation Skills
Structural Analysis
3D Modeling
Professional Mentoring

Business Records

Name / Title
Company / Classification
Phones & Addresses
Mark Palusis
Director
Harvest Community Church of Jupiter, Inc
Religious Organization
100 S Pennock Ln, Jupiter, FL 33458
(561) 746-7962, (561) 746-1599

Publications

Us Patents

Brittle Composite Structure For Resiliently Accomodating Thermal Expansion

View page
US Patent:
61026107, 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
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.

Attaching Brittle Composite Structures In Gas Turbine Engines For Resiliently Accommodating Thermal Expansion

View page
US Patent:
55928145, 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
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.

Composite Fastener For Use In High Temperature Environments

View page
US Patent:
60453109, Apr 4, 2000
Filed:
Oct 2, 1998
Appl. No.:
9/165913
Inventors:
Robert J. Miller - North Palm Beach FL
Mark E. Palusis - Jupiter FL
David C. Jarmon - Kensington CT
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F16B 3502
F16B 3504
US Classification:
411383
Abstract:
A fastener includes a composite body and a metal coupling attached to the body. The metal coupling includes an attachment structure to connect the fastener to an external structure. An assembly of components includes a first metallic component having a first coefficient of thermal expansion, a second non-metallic component having a second coefficient of thermal expansion different from the first thermal expansion and having a groove that receives a fastener that extends between the groove and the second component, the fastener slidably engaging the groove to accommodate relative expansion between the components.

Forced Air Cooled Gas Turbine Exhaust Liner

View page
US Patent:
57550930, 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
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.
Mark E Palusis from Jupiter, FL, age ~59 Get Report