Temperature Datum System

Slides:



Advertisements
Similar presentations
Supercharging Chapter 8.
Advertisements

Bendix Fuel Control System Theory of Operation
Rev A Sept. 18, Fuel Control S64F Model Helicopter.
Engine Systems J-52-P408 &J-52-P6/P8
FP-2 T-44 Ops Limits Overview System Limitations Propeller Limitations Starting Limitations Engine Limitations Airspeed Limitations Miscellaneous Limitations.
IDLE SPEED CONTROL. §To comply with federal emissions standards, idle speed control systems are used §Idle speed controlled by electronic module §Earlier.
 Systems  Checklist  Company Policies  The air conditioning system is fully automatic and provides continuous renewal of conditioned air in three.
CARBURETOR CIRCUITS AND COMPONENTS
Fuel System Carburetor A device that mixes air and fuel
SMALL ENGINES CARBURETION
Module 6 : Flow control valves
B757 Review Questions.
737 PNEUMATICS MENU PRINCIPAL.
SAFETY MEETING Off Highway Trucks. Brakes There are four separate controls used for braking Service Brake Retarder Secondary Brake Parking Brake.
AST 473 Citation II Systems Pressurization
GM PFI Operation and Testing. Overview Operating Modes Starting Clear Flood Run Acceleration Deceleration Battery Voltage Correction Fuel Cutoff.
Miniature Modular Rack Launcher Combo Senior Design Group 3 Casey Brown Cyril John Keith Kirkpatrick Bryan Rickards.
Circuit Protection  Protective Devices – terminate current flow in a circuit.  Located in series within a circuit  Excessive current flow results from.
Simple Carburettor Fuel System for a Piston Engine
B757 Review Questions.
PISTON ENGINES Part 8 Propeller Control.
ABORT. THROTTLES - IDLE WHEEL BRAKES - AS REQUIRED.
Fuel Evaporation in Ports of SI Engines P M V Subbarao Professor Mechanical Engineering Department Measure of Useful Fuel …..
Cover Your A$$ets Solar Panel Protection Project Team: Krista Miller Sohaib Hasan John Helme.
Thermal Solar Panel Protection Project Team: Krista Miller Sohaib Hasan John Helme.
JET PROPULSION Part 6 Jet Engine Operation Fuel Systems.
AccuMax Multi-Point Injection Mechanics
Piston Engine Operations
Carburetor Systems.
Lesson 7: Fuels And Fuel Systems
AIRCRAFT HANDLING Part 5 Pre-Take Off Checks. Starting Engines Starting engines is a team procedure between the pilot and the ground handling team. The.
B757 Review Questions.
Propellers The engines are equipped with four bladed, full
Continue The information provided in this training module covers the schematic flow charts for all ovens and ranges that utilized a preheat board, Self.
COLD WEATHER OPS When temp. less than 25 deg. F, preheat should be applied to engine Insufficient heat causes hard starting, abnormal wear to internal.
 ABS – Function, Design & Working  ABS types  Recent Advancements  Effectiveness & Limitations  Testing & Validation  Job of the Driver  Closing.
Engine drills & Limitations.
9 Electronic Transmission Controls.
Electronic transmissions Main controls Shift timing is computer controlled Line pressure is computer controlled which controls shift feel Computer can.
CL - 65 Other Limitations, Notes, and Cautions Last update 8/01/03 Please send any comments/suggestions to
BAKE BROIL - SELECT PROGRAM - CONV BAKE CONV BROIL SELF CLEAN On any diagram screen, double click any of the following components to bring you to a description.
® AutoTune ™. ® Always optimal engine setting Higher productivity – Optimal engine performance at all times – No time spent on carburettor adjustments.
CHAPTER Electronic Transmission Controls 27 Copyright © 2016 by Pearson Education, Inc. All Rights Reserved Advanced Engine Performance Diagnosis, 6e James.
PISTON ENGINE PROPULSION Chapter 5 Fuel Systems 1933 Alvis Engine 2014 Hyundai Engine Simple Carburettor Fuel System for a Piston Engine.
TECHNICAL TRAINING INVERTER-Y
Fuel System Carburetor A device that mixes air and fuel in correct proportion for efficient combustion. Stoichiometric Ratio 14.7 : 1 (Air : Fuel)
ENGINE PERFORMANCE COLUMBIA BASIN COLLEGE
GEN1 Fuel Mapping Overview Engine RPM Throttle Opening % Active Cell Active Cell RPM Active Cell Throttle Position Active Cell Map Compare ( See “Map Comparing”
Federal Aviation Administration 0 Composite Wing Tank Flammability November 20, Composite and Aluminum Wing Tank Flammability Comparison Testing.
Husqvarna K 960 Rescue Saw Engine 2 Cycle Horsepower 6.1 Max RPM 9300
7/15/2002PP.AFD.09 1 of 43 Yaskawa Electric America Variable Frequency Drives In HVAC Applications.
AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS)
UH-60L FAMILIARIZATION CW4 Sandbakken
Air Line Pilots Association, International EMB 145 Oral Questions Overhead “C” Select “Slide Show” Use the space bar on your computer to advance the presentation.
Flow Characteristics of Port Fuel Injection System P M V Subbarao Professor Mechanical Engineering Department Matching of Injector with Engine Requirements.
Types of Sensors Used in Multi-Point Fuel Injection System
MENU PRINCIPAL. THIS PRESENTATION INCLUDES THE SOURCES OF AIR, THE MAJOR SYSTEM COMPONENTS AND THE WAY THE CONTROLS AND INDICATORS ARE USED TO OPERATE.
International Trainer Conference
Sensors and Detectors - 1
Comparison between L – Series / K - series
Induction System – carburetor circuit
AutoTuneTM.
Actuators Topics covered in this presentation:
Electronic Fuel Injection
TURBINE OPERATION, INSTRUMENTS, AND MAINTENANCE PP 2
FP-2 T-44 Ops Limits 5/6/15.
How the Idle Air Control Valve Provide Smooth Idling of your Car
Two Common Types of EFI Chapter 22 Lesson 3.
Actuators Chapter 17 Lesson 5.
Presentation transcript:

Temperature Datum System Author: Kev Mc Henry

Identify the components and their location Describe the system Identify the components and their location List significant specifications Describe the system interface Objectives

Temperature Datum System The Temperature Datum (TD) system is used to electronically trim the fuel to the engine. The TD system will: a. Provide over-temperature protection during start and in flight. b. Maintain a selected temperature in flight. The Temperature Datum (TD) system is used to electronically trim the fuel to the engine. The TD system will: a. Provide over-temperature protection during start and in flight. b. Maintain a selected temperature in flight. Temperature Datum System TD system requirements 2

Temperature Datum System Components in the TD system are: The Speed Sense Control. The Thermocouples. The TD Control switch. The TD amplifier. The TD valve. The Co-ordinator/Discriminator. The electronic Fuel Correction lights. The components in the TD system are: 1. The Speed Sense Control. 2. The Thermocouples. 3. The TD Control switch. 4. The TD amplifier. 5. The TD valve. 6. The Co-ordinator/Discriminator. 7. The electronic Fuel Correction lights. Temperature Datum System Photo of TD components 3

TD Overview

Temperature Datum System Co-ordinator/ Discriminator Speed Sense Control TD Valve Show the location of the following: The Speed Sense Control. The Co-ordinator/Discriminator. The TD valve. Temperature Datum System Photo of TD components 4

Fuel System Tubing TD system Operation This slide and the next will explain the ‘Cross-over’ bump. Crossover occurs at 66o throttle position. The TD system changes from Temperature Limiting to Temperature controlling. This change is effected by a micro-switch in the Co-ordinator /Discriminator. Fuel System Tubing TD system Operation 18

Temperature Datum System TD Amplifier Thermocouples Show the location of the following: The Thermocouples. The TD amplifier. Temperature Datum System Photo of TD components 5

Temperature Datum System Electronic Fuel Correction Lights TD Control Switches Show the location of the following: The Electronic fuel correction lights. The TD control switches. Temperature Datum System TD valve 6

Temperature Datum Valve Corrected Fuel Out Null Orifice Bypass Valve Motor/ Generator Take Reset Solenoid Venturi Recap the basic component parts of the TD valve. 20% Take Stop 50% Take Stop Bypassed Fuel (5% - 70% of input fuel) 120% of Required Fuel in from FCU Temperature Datum Valve Bypass valve - null 7

Temperature Datum Valve Corrected Fuel Out Null Orifice Bypass Valve Motor/ Generator Take Reset Solenoid Venturi 20% Take Stop 50% Take Stop Bypassed Fuel (5% - 70% of input fuel) 120% of Required Fuel in from FCU Temperature Datum Valve

Bypass Needle NULL (always bypass 20%) 120% in 100% out Explain the standard bypass rate of 20% when the needle is in NULL. Bypass Needle Bypass valve - Max put 8

Bypass Needle NULL (always bypass 20%) MAX PUT + 15% (bypass 5%) 120% in 100% out 120% in 115% out Explain the bypass rate when the needle is at MAX PUT. Bypass Needle Bypass valve - Max take 9

Bypass Needle NULL (always bypass 20%) MAX PUT + 15% (bypass 5%) MAX TAKE - 20%/50% (bypass 40%/70%) 120% in 100% out 120% in 115% out 120% in 80%/50% out Explain the bypass rate when the needle is at MAX TAKE. (50% up to 94% RPM and 20% above that). Bypass Needle TD system Operation 10

TD Valve Adjustment

Temperature Datum Amplifier

TD Amp Installed

3 things affect the operation of the T.D. system: Position of the TD control switch. (NULL - LOCKED - AUTO). Engine RPM. (<94% & >94%). Throttle position (<66O & >66O). 3 things affect the operation of the TD system: 1. Position of the TD control switch. (NULL - LOCKED - AUTO). 2. Engine RPM. (<94% & >94%). 3. Throttle position (<66O & >66O). T. D. System Operation TD system Operation 11

T. D. System Operation - Null TD Control switch to NULL: If the TD control switch is in the NULL position, the TD Valve will remain in 20% bypass position. In NULL, the Fuel Correction lights behave in the same manner as for AUTO but the TD valve will not move. NB: In ‘NULL’, > 66o throttle, there is NO Overtemperature protection if 1077o is exceeded. TD Control switch in NULL: If the TD control switch is in the NULL position, the TD Valve will remain in 20% bypass position. In NULL, the Fuel Correction lights behave in the same manner as for AUTO but the TD valve will not move. T. D. System Operation - Null TD Controlling check 23

“NULL” TD System OFF

T. D. System Operation - Start Limiting TD Control switch in AUTO: Starting: LSGI selected: RPM <94%. TD system in Start Limiting mode. Maximum permitted TIT - 830oC. Maximum ‘Take’ capability - 50%. (Fuel is taken [trimmed] if temp >830oC). Electronic Fuel Correction light - ON. TD control switch in AUTO: Starting: LSGI selected: RPM <94%. TD system in Start Limiting mode. Maximum permitted TIT - 830oC. Maximum ‘Take’ capability - 50%. (Fuel is taken [trimmed] if temp >830oC). Electronic Fuel Correction light - ON. T. D. System Operation - Start Limiting TD system Operation 12

Start Limiting

T. D. System Operation - Normal Limiting TD Control switch in AUTO: Starting: NGI selected: RPM >94%. TD system in Normal Limiting mode. Maximum permitted TIT - 1077oC. Maximum ‘Take’ capability - 20%. (Fuel is taken [trimmed] if temp >1077oC). Electronic Fuel Correction light - ON. TD control switch in AUTO: Starting: NGI selected: RPM >94%. TD system in Normal Limiting mode. Maximum permitted TIT - 1077oC. Maximum ‘Take’ capability - 20%. (Fuel is taken [trimmed] if temp >1077oC). Electronic Fuel Correction light - ON. T. D. System Operation - Normal Limiting TD system Operation 13

Normal Limiting

TD Control switch in AUTO: On Speed, >66o throttle: TIT @ crossover 820oC (+/- 20oC). Temperature scheduled from 820oC to 1077oC between 66o and 90o throttle position. Maximum ‘Take’ - 20%. Maximum ‘Put’ - 15%. Electronic Fuel Correction light - OUT. TD control switch in AUTO: On Speed, >66o throttle: TIT @ crossover 820oC (+/- 20oC). Temperature scheduled from 820oC to 1077oC (1067oC - 1083oC) between 66o and 90o throttle position. Maximum ‘Take’ - 20%. Maximum ‘Put’ - 15%. Electronic Fuel Correction light - OUT. T. D. System Operation TD system Operation 15

T. D. System Operation - Controlling TD Control switch in AUTO: As the throttles are advanced through 66o (crossover), the TD system normally ‘cuts back’ the fuel to set 820oC (+/- 20oC). This is known as the crossover bump. Between throttle settings of 66o & 90o , a specific temperature is scheduled. The TD valve will either ‘put’ or ‘take’ fuel to achieve the required temperature. TD control switch in AUTO: As the throttles are advanced through 66o (crossover), the TD system normally ‘cuts back’ the fuel to set 820oC (+/- 20oC). This is known as the crossover bump. Between throttle settings of 66o & 90o, a specific temperature is scheduled. The TD valve will either ‘put’ or ‘take’ fuel to achieve the required temperature. T. D. System Operation - Controlling TD system Operation 16

Controlling (Sel Temp 820 - 1077°C)

TD Control switch in LOCKED: The crossover ‘bump’ can be an inconvenience, especially during formation and tactical flying and also during take-off in very cold weather. To overcome this, the TD valve is electronically locked in position and will alter the fuel hydro-mechanically with throttle selection. The TD valves are normally locked in pairs, above crossover. TD Control switch in LOCKED: The crossover ‘bump’ can be an inconvenience, especially during formation and tactical flying and also during take-off in very cold weather. To overcome this, the TD valve is electronically locked in position and will alter the fuel hydro-mechanically with throttle selection. The TD valves are normally locked in pairs, above crossover. T. D. System Operation TD system Operation 20

T. D. System Operation 18O MAX TORQUE = 19600’’/LBS 66O 20000 1077oC 18000 16000 14000 12000 T O R Q U E 820oC 10000 8000 6000 4000 This slide and the next will explain the ‘Cross-over’ bump. Crossover occurs at 66o throttle position. The TD system changes from Temperature Limiting to Temperature controlling. This change is effected by a micro-switch in the Co-ordinator /Discriminator. 2000 600oC 0O 10O 20O 30O 40O 50O 60O 70O 80O 90O T. D. System Operation THROTTLE TD system Operation 18

T. D. System Operation 18O MAX TORQUE = 19600’’/LBS 66O 20000 1077oC 18000 16000 Torque, Fuel flow and TIT reduce at Crossover 14000 12000 T O R Q U E 820oC 10000 8000 Crossover ‘BUMP’ 6000 4000 The TD system causes a temperature of 820oC +/- 20oC to be scheduled. Generally speaking the TD system will have to cut back the amount of fuel going to the burners to achieve the desired temperature. This cut-back can be seen on the TIT, torque and fuel flow gauges along with the Fuel Correction lights going out. 2000 600oC 0O 10O 20O 30O 40O 50O 60O 70O 80O 90O T. D. System Operation THROTTLE TD system Operation 19

Locked In Correction

Overtemp Release

T. D. System Operation 18O 34O 66O 100% 94% 90% 80% 70% 60% R P M 50% C R O S V E 40% G R O U N D F L I G H T 30% I D L E I D L E 20% This and the next 3 slides give a graphic representation of the operation of the TD system. 10% 0% 0O 10O 20O 30O 40O 50O 60O 70O 80O 90O T. D. System Operation THROTTLE TD system Operation 25

T. D. System Operation 18O 34O 66O 100% 94% 90% GROUND IDLE 80% 70% START TEMP LIMITING MAX TEMP 830OC MAX TAKE 50% NO PUT EFC LIGHT ON 60% R P M 50% C R O S V E 40% G R O U N D F L I G H T 30% I D L E I D L E 20% Ground Idle - Throttles in Ground Idle detent - RPM < 94%. Start Temp limiting - 830oC. Max take 50%, No put capability. Electronic Fuel Correction light ON. 10% 0% 0O 10O 20O 30O 40O 50O 60O 70O 80O 90O T. D. System Operation THROTTLE TD system Operation 26

T. D. System Operation 106% 18O 34O 66O 100% NGI 94% 90% GROUND IDLE NORMAL TEMPERATURE LIMITING UP TO 1077OC OVERTEMP PROTECTION @ 1077OC MAX TAKE 20% NO PUT CAPABILITY EFC LIGHT ON 80% 70% START TEMP LIMITING MAX TEMP 830OC MAX TAKE 50% NO PUT EFC LIGHT ON 60% R P M 50% C R O S V E 40% G R O U N D F L I G H T 30% I D L E I D L E 20% NGI up to 66o throttle, RPM > 94%. Normal Temp limiting - 1077oC (1067oC to 1083oC), Overtemp protection. Max take 20%, No put capability. Electronic Fuel Correction light ON. 10% 0% 0O 10O 20O 30O 40O 50O 60O 70O 80O 90O T. D. System Operation THROTTLE TD system Operation 27

T. D. System Operation 106% 18O 34O 66O 100% NGI 94% 90% GROUND IDLE NORMAL TEMPERATURE LIMITING UP TO 1077OC OVERTEMP PROTECTION @ 1077OC MAX TAKE 20% NO PUT CAPABILITY EFC LIGHT ON TEMPERATURE CONTROLLING 820°C - 1077OC SCHEDULED AT 90O THROTTLE MAX TAKE 20% MAX PUT +15% NO OVERTEMP PROTECTION IN AUTO EFC LIGHT OUT (UNLESS O’TEMP IN LOCKED) 80% 70% START TEMP LIMITING MAX TEMP 830OC MAX TAKE 50% 60% R P M 50% C R O S V E 40% G R O U N D F L I G H T 30% I D L E I D L E 20% > 66o throttle, RPM 100%. Temp Controlling - 820°C - 1077oC (1067oC to 1083oC) scheduled, NO Overtemp protection unless LOCKED has been selected. Max take 20%, Max Put +15%. Electronic Fuel Correction light OUT (unless O/Temp in LOCKED). 10% 0% 0O 10O 20O 30O 40O 50O 60O 70O 80O 90O T. D. System Operation THROTTLE TD system Operation 28

TD Control switch in LOCKED: The TD valve will only unlock if an over-temp occurs (>1077oC), or if ‘NULL’ or ‘AUTO’ is selected. The Fuel Correction lights will remain in the state they were in when locked was selected. If locked was selected above crossover, when an overtemp occurs the Fuel Correction light will come on to advise that controlling action has occurred. TD Control switch in LOCKED: The TD valve will only unlock if an over-temp occurs (>1077oC), or if ‘NULL’ or ‘AUTO’ is selected. The Fuel Correction lights will remain in the state they were in when locked was selected. If locked was selected above crossover, when an overtemp occurs the Fuel Correction light will come on to advise that controlling action has occurred. T. D. System Operation TD system Operation 21

TD Control switch in LOCKED: If it is required to re-lock the TD valves, the throttles must be selected back above crossover with the TD switches in AUTO then LOCKED re-selected. TD Control switch in LOCKED: If it is required to re-lock the TD valves, the throttles must be selected back above crossover with the TD switches in AUTO then LOCKED re-selected. T. D. System Operation TD system Operation 22

ANY QUESTIONS?