POWERPLANT INTRO TO TURBINES Spokane Community Community College College.

Slides:

Advertisements

Similar presentations

RECORD KEEPING Cooperative Development of Operational

Advertisements

Engine Systems J-52-P408 &J-52-P6/P8

Auxiliary Power Plant Fundamentals

Jubail Industrial College is pleased to announce Mechanical Engineering Training Short courses For more information, please contact: Special Programs Unit.

Jet Engine Design Idealized air-standard Brayton cycle

Jet Engine Design diffuser compressor combustion chamber turbine nozzle P=constant q out q in T s 1-2 Isentropic compression in.

SAFETY, TOOLS & EQUIPMENT, SHOP PRACTICES

Bench Testing, Maintenance, and Troubleshooting.  Identify three primary steps in bench testing a helitorch.  Identify six considerations in maintaining.

Lecture 3b: Aircraft Engines

The art of Engineering

FLIGHT POWER Know basic engine principles. 1. Define a list of terms related to basic engine principles. 2. Describe the various types and components of.

PNEUMATIC SYSTEMS.  The learning objective of this presentation, To develop the student's knowledge of the vacuum system to meet the basic functions.

 Review Alpena Biorefinery Hearing Conservation Program  Types of Hearing Protection Devices Employee Safety Training

Practical Energy Conservation Tips for Gas Turbine Propulsion Ships.

© 2015 Cengage Learning. All Rights Reserved. May not be scanned, copied, duplicated, or posted to a publicly accessible website, in whole or in part.

 Research and identify ordnance  Assist in the preparation and use of advance robotics  Explosively disposing of hazardous ordnance  Prepare and maintain.

© 2015 Cengage Learning. All Rights Reserved. May not be scanned, copied, duplicated, or posted to a publicly accessible website, in whole or in part.

Jimmy Luo. HistoryHow It WorksCurrent Applications History.

Definitions, Goals and Objectives

GAS TURBINE OPERATION AND MAINTENANCE

Gas Turbine Theory and Construction

Turbine Crane CRANES TURBINE NEA39. Turbine Crane PLANT STATUS! PV Daily Status Report.

Chapter 4: Overview of Preventive Maintenance

FMTV COOLING SYSTEMS 4/23/2017.

Gas Turbine Theory and Construction. Introduction Comprehend the thermodynamic processes occurring in a gas turbine Comprehend the basic components of.

AIRCRAFT ENGINE Lecture 4

Lockout/tagout (LOTO) is a technique used to prevent energy from being released during the servicing of equipment. This is accomplished by placing locks.

Troubleshooting Small Engine Systems Jason Spurlin 4/10/02 Virginia Tech Edited by the CTAE Resource Network February 2011.

Office of Aviation Safety American Airlines Flight 1400 St. Louis, Missouri Maintenance Issues Ron Price.

BEST PRACTICE COMMUNICATING THE WAY: LOTOV

DRAFT. Introduction  Mechanical Power Reciprocating Engines Turbines Turbines are compact machines (high power to weight ratio, having less balancing.

Chapter 1 Why We Have to do Maintenance. Why Maintenance Provides assurance Flight Safety Reliability Airworthiness.

LOCKOOUT/TAGOUT b THE ULTIMATE GOAL IS: To implement policies and procedures to prevent, as necessary, the release of hazardous energy from power sources--or.

Axial Flow Compressors

National Transportation Safety Board Powerplants and Maintenance Issues Dave Keenan Powerplants Group Chairman Dave Keenan Powerplants Group Chairman.

Turbojet engine (Rocket)‏

PARISUTHAM INSTITUTE OF TECHNOLOGY AND SCIENCE DEPARTMENT OF AERONAUTICAL WELCOME STUDENTS BY ANBARASAN.T DEPT. OF AERONAUTICAL.

FAA sUAS ARC Support Documentation © ASTM International. All Rights Reserved. The Unmanned Aircraft System Initiative F38 on Unmanned Aircraft Systems.

Lecture 3b: Aircraft Engines s: Propeller + Piston Engines Era  From 1903 (Wright bros.) until the Early 1940s, all aircraft used the piston.

Multimedia Thematic Project – Part III Lesson II F-18E/F Maintenance Research Joe King University of Phoenix Designing and Producing Educational Technology.

Module 4 Reaction Turbines: Kaplan Turbine. Module 4 Reaction Turbines: Kaplan Turbine. Introduction.

Office of Aviation Safety Aircraft Maintenance and Inspections.

PC Support & Repair Chapter 4 Preventive Maintenance & Troubleshooting.

JET ENGINE PROPULSION Chapter 0 Introduction. GAS TURBINE ENGINE A GAS TURBINE ENGINE OPERATES SIMILARILY TO A PISTON ENGINE. THE DIFFERENCE BEING THAT.

Definitions, Goals and Objectives Embry-Riddle Aeronautical University Chapter 3.

1 Engine Mechanical Labs R. Bortignon. 2 Repair Information – essential! locate model number!

TURBINE ENGINE REMOVAL AND OVERHAUL. TURBINE ENGINE REMOVAL REASONS FOR: Engine Life Span (TBO) Usually specified components Not necessarily engine assembly.

POWERPLANT INTRO TO TURBINES PP2 Spokane Community Community College College.

Troubleshooting Small Engines by Jason Spurlin 4/10/02 Virginia Tech This presentation has not been edited by the Georgia Curriculum Office.

© 2008 Cisco Systems, Inc. All rights reserved.Cisco ConfidentialPresentation_ID 1 Chapter 4: Overview of Preventive Maintenance IT Essentials 5.0.

TURBINE ENGINE REMOVAL AND OVERHAUL

Prepared by: Kamil Bin Sahidin

Automotive Engines Theory and Servicing

Parking brake selector valve

GROUND SERVICING OF VARIOUS SUB SYSTEMS

Troubleshooting Small Engines by Jason Spurlin 4/10/02 Virginia Tech This presentation has not been edited by the Georgia Curriculum Office.

Gas Turbine Theory and Construction

GROUND SERVICING OF VARIOUS SUB SYSTEMS

14 Refrigerant Recovery, Recycling, and Recharging.

Aeronautical PUBLICATIONS

Overhaul of Combustion Turbines Under NSR Regulations

Who is an Aviation Maintenance technician?

AIR CONDITIONING SYSTEM MAINTENANCE

Cylinder Head: Parts and Service

Small Engine Ignition Systems

Tracey Johnson Service Engineering Boeing Commercial Aviation Services

Automotive Engines Theory and Servicing

Presentation transcript:

POWERPLANT INTRO TO TURBINES Spokane Community Community College College

READING ASSIGNMENT

FAA REQUIREMENTS 1. Exhibits knowledge of at least two of the following— a. turbine engine theory of operation. b. checks necessary to verify proper operation. c. turbine engine troubleshooting procedures. d. procedures required after the installation of a turbine engine. e. causes for turbine engine performance loss. f. purpose/function/operation of various turbine engine components. g. turbine engine maintenance procedures.

2. N/A 3. Demonstrates the ability to perform at least one of the following: a. repair a turbine engine compressor blade by blending. (Level 3) b. remove and/or install a turbine engine component. (Level 3) c. determine cycle life remaining between overhaul of a turbine engine life limited component. (Level 2) d. check rigging of a turbine engine inlet guide vane system. (Level 3) e. measure compressor or turbine blade clearance. (Level 3) f. troubleshoot a turbine engine. (Level 3) g. locate and identify turbine engine components. (Level 2) h. inspect turbine engine components. (Level 3) NOTE: T. AUXILIARY POWER UNITS may be tested at the same time as AREA B. No further testing of auxiliary power units is required.

S. TURBINE POWERED AUXILIARY POWER UNITS Objective. To determine that the applicant: 1.Exhibits knowledge of at least two of the following: a. inspection to ensure proper operation of turbine driven auxiliary power unit. b. replacement procedure for an igniter plug. c. servicing an auxiliary power unit. d. troubleshooting an auxiliary power unit. e. function and operation of auxiliary power unit(s).

Early reaction engine concepts

Balloon analogy of the jet engine

Heinkel He-178 World’s first jet-powered aircraft (1939)