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O&M Gas Turbine Course Phpc , Ha’py Gas Plant Solar Mars100 Man Turbo Gas compressor Turbine Department [email protected] 1 Instructor: Eng. Mohamed Elbarougy Phpc: Turbomachinery Team Leader Mobile : 0100214245 Work : 7638
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Page 1: 00 elbarougy turbine Course Hapy

O&M Gas Turbine

Course Phpc , Ha’py Gas Plant

Solar Mars100 Man Turbo Gas compressor

Turbine Department [email protected]

1

Instructor: Eng. Mohamed Elbarougy Phpc: Turbomachinery Team Leader

Mobile : 0100214245

Work : 7638

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O&M Gas Turbine Course

Turbine Department [email protected]

2

Basic Gas Turbine Knowledge

Basic mechanical Classification

Basic Ex

Basic of Electric and Instrument

Gas Turbine Main components

Ha’py Gas Turbine Systems

Enclosure and ancillary

Gas Compressor and yard valve

Dry Gas Seal

Operation

Solar turbine Manual

Books

شرح مبسط باللغه العربيه

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Turbine History 4

Turbine Department [email protected]

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Brayton Cycle Turbine Department [email protected]

5

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Bryton Cycle in Color 6

Turbine Department [email protected]

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Bearing types 7

Turbine Department [email protected]

BEARINGS CLASSIFICATION

ROLLING CONTACT ( ANTIFRICTION) BEARINGS SLIDING SURFACE ( FRICTION )BEARINGS

JOURNAL BEARINGS

Commonly Known As Roller Bearings Or Ball Bearings, Are Defined As Bearings Which Have Rolling Contact Between Their Surfaces.

THRUST BEARINGS

BALL CYLINDRICAL TAPER SPHERICAL

Deep Groove Cylindrical Spherical Roller Bearing

Tapered Roller Bearing

Angular Contact Thrust Taper Roller Bearing

Split Spherical Bearing

Self-aligning

WHAT IS THE BEARING FUNCTION?

Bearing Arrangement

-BEARINGS MOUNTING

a- Oil Bath

b- Electric Plates c- Induction Heaters

HOT MOUNTING

There Are Several Basic Rules For Mounting

1- Never Directly Strike The Rings ,Cage Or Rolling Elements Of A Bearing

While Mounting, A Ring May Crack Or Metal Fragments May Break Off.

2- Never Apply Pressure To One Ring In Order To Mount The Other.

3- Use An Ordinary Hammer , Since Soft Headed Hammers Leave Fragments.

Heating Tools

a- Oil Bath b- Electric Plates

c- Induction Heaters d- Heating Cabinets

Never Heat The Bearing To A Temperature Greater Than

125˚C,However,Because The Material May Change Metallurgical And

Produce Alterations In Diameter Or Hardness.

Never Heat A Bearing Using An Open Flame ,Local Overheating Must

Be Avoided, Use A Thermometer To Check The Bearing Temperature.

Push The Bearing Along The Shaft And Hold The Bearing In Position,

Pressing Until A Tight Fit Is Obtained.

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Valve types 8

Turbine Department [email protected]

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Seal types Turbine Department [email protected]

B-OPPOSED ARRANGEMENT

SEALING DEVICES

GASKETS

1- Used To Seal Non-moving Connecting Surfaces .

2- Made From Compressible Materials That Can Be

Squeezed. ( Metal , Teflon, Cork, Paper, And Rubber)

Types Of Gaskets

1- Ring Gasket

2- Full-face Gaskets

3- Spiral Wound Gaskets

MEASURING THE CROSS SECTION AND INSIDE DIAMETER

SEAL FEATURE

DIR

EC

TIO

N

OF

R

OT

AT

ION

ROTATING FACE

SPIRAL RIDGE

O-RINGS

PACKING

DRY GAS SEAL

MECHANICAL SEAL

inner and outer diameters are

reinforced with several piles of metal

without filler to give greater stability and

better compression characteristics.

This type of gasket is able to accommodate pressures

from high vacuum to over 700 bar and seal at

temperatures from cryogenic to 1650°C

HOLLOW PUNCH TOOLS

O-RING SEALING APPLICATIONS

1- O-ring seal is a means of closing off

a passageway and preventing an

unwanted loss or transfer of fluid.

2-The classic O-ring seal consists of

two elements, the O-ring itself, and a

STATIC SEALS

LABYRINTH SEAL

TANDEM SEALS

DOUBLE SEALS

OUTSIDE-MOUNTED SEALS

1- used for low-pressure

applications since both seal faces,

the primary ring and mating ring,

are put in tension. This limits the

pressure capability of the seal. HEAVY DUTY MACHINE

EXTENSION GASKET CUTTER

DYNAMIC SEALS

GASKET CUTTING TOOLS

Atmos

Seal Head

2- used to minimize corrosion that might occur if

the metal parts of the seal were directly exposed

to the liquid being sealed.

Circulation Liquid in

and out to cool and

lubricate

Gland

Plate

Mating Rings

Liquid

Housing

Seal Head Seal Head

Neutral

Circulation

Liquid

Gland

Plate Atmos

Mating Rings

Bypass

Liquid

Inlet Housing

Liquid

Gland

Seal Head Seal Head

INSIDE-MOUNTED SEAL.

1- The most common installation

is an inside-mounted seal.

2- the liquid under pressure acts

with the spring load to keep the

seal faces in contact.

Gland

Plate Atmos

Seal Head liquid

1- Packing is used in the stuffing box

to control the leakage of the liquid

out, or the leakage of air in, where

the shaft passes through the casing.

PACKING TYPES

1- Metallic( lead, babbit,

aluminum and

copper)

2- Flexible graphite

3- Non-asbestos

liquid

1- Single seal

a. Internally mounted

b. Externally mounted

1- Dry gas seals are in the positive seal class and have the same basic design features as mechanical face seals with one significant difference. The dry gas seal has shallow grooves cut in the rotating seal face located part way across the face.

2- The grooves may be in a spiral pattern; the exact location and pattern vary from one manufacturer to another. Lubrication and separation is effected by a microscopically thin film of gas.

3- This implies some finite amount of leakage, which is quite small but must be accounted for in the design.

4- The stationery mounted seal unit comprises a spring loaded, ’O’ ring sealed carbon face, held as an integral unit in stainless steel retainer.

5- An 'O' ring sealed rotating seat, normally manufactured from tungsten carbide, is profiled with a series of spiral grooves having a depth of between 0.0025 to 0.010mm as illustrated.

BENEFITS

1- No Wear

2- No Seal Oil System

3- No Process Contaminations

4- Lower Power Consumption

5- Improved Rotor System Stability

6- Improved Operational Safety

Dry gas seal cartridge

Inner ring

hoop Star foil (filler)

outer ring

FLEXSEAL

Spiral

Winding

Manufactured To

ASME B16.20

Nominal Pipe Size

And Pressure Class

( Standard Gasket Only

Inner Ring

Winding Metal

And Filler Material

Manufactures Name

Or Trademark Outer

(Centering)

Ring

Outer Ring Material

( When Other Than

Carbon Steel )

Inner Ring Material

Stamped On Inner Ring

( When Other Than

Carbon Steel Or PTFE)

Advantages:

in which there is

little or no relative

motion between the

mating surfaces;

which must function between

surfaces with definite relative

motion, such as the seal on the

piston of a hydraulic cylinder.

‘ X-Tree’

‘Microdam’

‘ Biro’

‘Phoenix’

‘T’ Slot

Bi-Directional Groove Profiles

Neutral

Circulation

Liquid Gland

Plate

Mating Rings

Housing

Liquid Seal Head

A- BACK TO BACK

2- Multiple seal

a. Double seals

b. Tandem seals

Type 28AT

THE FUNCTION OF THE O-RING

1- The elastomer is contained in the gland and forced

into the surface imperfections of the glands and any

clearance available to it, creating a condition of “zero”

clearance and thus effecting a positive block

to the fluid being sealed.

2- The pressure which forces the O-ring to flow is

supplied by mechanical pressure or “squeeze,”

generated by proper gland design and material

selection and by system pressure transmitted by the

fluid itself to the seal element.

properly designed gland or cavity to contain the

elastomeric material.

Simplest and least expensive

of non-contacting types. Disadvantage :

Highest leakage rate among

non-contacting seals.

ROTAATING FACE

TUGETEN CARBIDE OR

SILICON CARBIDE

STATIONARY FACE

CARBON

GAP

SEAL GAS IN

GAS LEAKAGE

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Compressor Type -1

Turbine Department [email protected]

10

DISPLACEMENT COMPRESSORS

ROTARY RECIPROCATING

SLIDING VANE SCREW

DYNAMIC

COMPRESSORS CLASSIFICATION

In Which Compression And Displacement Is Effected By The Positive

Action Of Rotating Elements; Gas Trapped Between Elements Is

Compressed And Displaced

1- Consists Of A Cylindrical Rotor In Which Flat, Sliding

Vanes Fit Into Radial Slots.

2-As The Rotor Turns, The Sliding Vanes Move Out Against

The Casing Wall Due To Centrifugal Force. Pockets Of Gas

Are Trapped Between The Vanes And The Wall. Due To The

Eccentricity, These Pockets Decrease In Volume, Thus

Compressing The Gas.

1-Consists Of Two Intermeshing Rotors, Machined In The Form Of

An Axial Screw And Enclosed In A Close-fitting Casing.

2-The Male Rotor Has Four Convex Lobes And The Female Rotor

Has Six Concave Flutes. The Rotors Do Not Come In Contact With

Each Other Or With The Casing, Thus Internal Lubrication Is Not

Required.

3-The Male Rotor Is Usually The Driven One And, In Turn, Drives

The Female Rotor By Means Of Timing Gears.

TIMING

GEARS

OIL

SEALS

AIR SEALS

DRIVEN GEAR

BALANCE

PISTON

MALE

ROTOR

FEMALE

ROTOR

BEARING

S

BEARING

S

WATER

JACKET

LOBE 1- Has Two Rotors, Revolving In Opposite Directions

Within A Casing.

2-one Rotor Is Driven Directly By The Driver And The

Other Is Driven Through The Timing Gears.

3- A Pocket Of Air Is Trapped Between The Lobe And

The Casing Wall. It Is Then Carried Around To The

Discharge On The Opposite Side Of The Casing.

ADVANTAGES

1-Compact.

2-Require No Inlet Or Discharge Valves

3-And Produce An Even Flow Of Oil Free Air.

Cylinder barrel, head and air passages

Are thoroughly water jacketed for cooling

Easily removable

cylinder head has

simple gasket

seal

Connectin

g

Rod

Crank Pin

Main

Bearing

crosshead

Piston

Air Packing Valve

Distance Piece

1- In Which The Air Is Compressed By A Piston Moving In A Reciprocating Manner Within A Cylinder.

2- The Cylinder Is Equipped With Intake And Discharge Valves To Control The Flow Of Air Entering And

Leaving. This Type Of Compressor Is Used In A Wide Variety Of Applications ,It Is Suitable For All

Ranges Of Pressure.

3- High Speed Units (800 - 1800 Rpm) -Low Speed Units (300 - 600 Rpm)

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Compressor Type -2

Turbine Department [email protected]

11

DYNAMIC COMPRESSORS

AXIAL CENTRIFUGAL

COMPRESSORS CLASSIFICATION

DISPLACEMENT

OPERATION

1- Gas Is Drawn Into The Eye Of The Impeller Where It Is Accelerated

Through Centrifugal Force And Velocity Energy Is Imparted To The

Gas. As The Gas Is Discharged From The Impeller It Flows Into The

Diffuser Or Volute Where It Decelerates. This Velocity Is Transformed

Into Pressure Energy. The Process Is Repeated Through Every Stage

Of The Compressor, Resulting In A Higher Pressure Ratio For Multi-

stage Compressors.

COMPRESSOR CASINGS

HORIZONTALLY SPLIT

IMPELLERS

1- Consist Of Several Stages And Are Generally Used To

Move Large Volumes Of Gas

2- The Gas In An Axial Flow Compressor Flows In An

Axial Direction Through A Series Of Rotating Blades

(Rotor Disc) And Stationary Vanes (Stator) That Me

Attached To The Casing.

3- The Rotor Blades Increase The Gas Velocity. The

Velocity Is Then Converted Into Pressure As The Gas

Enters The Stator Section And Is Slowed Down.

SECTIONAL VERTICALLY SPLIT OPEN SEMI-CLOSED CLOSED

1- Simplest Design,

Usually Single Stage,

2-Consist Of A Series Of

Vanes Radiating Out From

A Central Hub.

3-Can Be Found In Rough

Service Environments And

Where Dirty Gases Need

To Be Moved.

1-Used In A Many Compressors,

And May Be Used In A Single

Stage Or Multi-stage Or Even As

The Final Stage In An Axial

Compressor.

2-The Blades Can Be Straight

Radial , Backward Leaning ,

Forward Leaning, Or A

Combination Of The Blades

1-Used Extensively In Single

And Multi-stage Units.

2-The Enclosure Of The

Vane Permits Higher

Pressure Ratios To Be

Achieved And The Close

Tolerances Between Impeller

And Diffusers Minimizes

Leakage, Resulting In Higher

Efficiencies.

1- Found On Small Units With Low-

pressure Ratios And Small Volumes.

2- Consist Of A Number Of

Sections, Each Bolting To Another

By Means Of Tie Rods.

1-Vertically Split Or Barrel Casings Are

Used In High-pressure Applications (Up To

10 000 Psig)

2- The Compressor Rotor And Impellers Are

Housed Inside A Horizontally Split Casing

Which Is Then Contained Within The Barrel.

3-The Barrel Casing Is Sealed By The Front

Cover, Which Is Bolted And Sealed With An

O-ring. Some Designs Incorporate A Single

End Cover Whereas Others Allow The

Removal Of Both Ends.

1-Enable Easy Removal Of The Upper

Section, Allowing Inspection Of The Rotor,

Impellers, Bearings And Seals.

2-The Casing Is Split Along The Centre Line

Of The Housing And Bolted Together By

Means Of A Large Flanged Area.

3-Sealing Is Metal To Metal, Which Presents

A Problem When Higher Pressures Are

Required. For This Reason, Horizontally

Split Casings Are Usually Limited To Less

Than 1000 Psig.

Advantages

1- High Horsepower Per Unit Of Space And

Weight

3- Easily Automated For Remote Operations

4- Skid Mounted Self-contained

5- Low Initial Costs Per Horsepower

6- Lower Maintenance Cost Than

Reciprocating

7- High Availability Factor

8- Larger Capacity Available Per Unit

Disadvantages

1- Lower Compressor Efficiency

2- Limited Flexibility For Capacity

3- Higher Fuel Rate Than Reciprocating

Units

4- Larger Horsepower Outage Disrupts

Process Or Pipeline Capabilities

NOTE

Thrust Bearing Failure Is One Of The Worst Types Of Failure That Can

Occur In A Dynamic Compressor. Due To The High Rotational Speeds

And The Close Clearances Between The Stationary And Rotating

Elements, Any Contact Due To Shaft Movement Results In Instant

Compressor Failure.

Blades fixation methods

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Explosion proof Turbine Department [email protected]

12

• Zone Vs Div

• Ex protection and symbol

• photo

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DC Current

Turbine Department [email protected]

13

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14 Ac Current

Turbine Department [email protected]

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AC single and 3 phases

Turbine Department [email protected]

15

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16 Ac motor wiring

Turbine Department [email protected]

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17 Ac motor wiring 2

Turbine Department [email protected]

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Turbine SLD

Turbine Department [email protected]

18

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Turbine MCC

Turbine Department [email protected]

19

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Instrument loop

Turbine Department [email protected]

20

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Final control element

Turbine Department [email protected]

21

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Final control , Controller , Measuring device

Turbine Department [email protected]

22

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Instrument loop diagram

Turbine Department [email protected]

23

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Turbine main Componants

Turbine Department [email protected]

25

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Mars Engine Main Subassemblies

Turbine Department [email protected]

26

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Mars 90/100 Compressor Assembly

Turbine Department [email protected]

27

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Compressor Blades and Stators

Turbine Department [email protected]

28

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Mars 90/100 Variable Compressor Vane Assembly

Turbine Department [email protected]

29

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Combustor types

Turbine Department [email protected]

30

• Can-Annular combustor

• Annular-combustor

• Can combustor

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Turbine Radial Inflow

Turbine Department [email protected]

31

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Turbine Axial flow

Turbine Department [email protected]

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Turbine Nozzle and Rotor Reaction

Turbine Department [email protected]

33

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Turbine Nozzle and Rotor Reaction

Turbine Department [email protected]

34

Gas turbines are in general or experimental use in

the following applications:

• Aircraft

• Power plants

• Standby equipment

• Boat and ship propulsion

• Gas pipeline compressor drives

• Railroad (have been used but are not common)

• Automotive (extensive experimentation in the past)

• Heavy mobile equipment (experimentation)

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Turbine Nozzle and Rotor Reaction

Turbine Department [email protected]

35

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Turbine Systems

Turbine Department [email protected]

36

Lube Oil System

Start System

Air Intake and air utility

Fuel System

Enclosure

Fire and Gas

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Turbine Department [email protected]

37

Lube Oil System

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Typical Radial & Axial Tilt Pad Bearing

Turbine Department [email protected]

38

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Start System

Turbine Department [email protected]

39

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Mars Accessory Gear Box Starter Motor

Turbine Department [email protected]

40

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Mars 90/100 Accessory Drive Assembly

Turbine Department [email protected]

41

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Air Intake Systems

Turbine Department [email protected]

42

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Mars 90/100 Location of Air/Oil Seals

Turbine Department [email protected]

43

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Mars 90/100 Engine Oil Seal Pressurization Airflow Turbine Department [email protected]

44

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Labyrinth Seal Turbine Department [email protected]

45

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Typical First Stage Cooled Blade

Turbine Department [email protected]

46

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Bleed Valve Using a ExLar Actuator

Turbine Department [email protected]

47

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Mars 90/100 Bleed Air System Diagram

Turbine Department [email protected]

48

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Fuel System

Turbine Department [email protected]

49

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Mars SoLoNOx Fuel Injector and Torch

Turbine Department [email protected]

50

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Fuel Components (after 1999)

Turbine Department [email protected]

51

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Mars SoLoNOx Fuel Module Fuel Control Valves

Turbine Department [email protected]

52

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Mars SoLoNOx Injector

Turbine Department [email protected]

53

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SoLoNox Fuel System

Mars Gas Fuel

Turbine Department [email protected]

54

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Earlier Version of Mars SoLoNOx Engine Pre 1999

Turbine Department [email protected]

55

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Mars SoLoNOx Engine Post 1999

Turbine Department [email protected]

56

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NOX and CO Formation Turbine Department [email protected]

57

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Standard Engine Combustor Emissions Characteristics

Turbine Department [email protected]

58

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Typical SoLoNOx Emissions Characteristics

Turbine Department [email protected]

59

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Temperature Stations on a Typical

Turbine Engine

Turbine Department [email protected]

60

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Temperature Stations on a Typical Turbine Engine

Turbine Department [email protected]

61

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Turbine Department [email protected]

62

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Mars 90/100 Exhaust Collector Assembly

Turbine Department [email protected]

63

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Package Orientation

Turbine Department [email protected]

64

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Orientation

Turbine Department [email protected]

65

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Mars Driver Skid (Prime Mover)

Turbine Department [email protected]

66

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Typical Skid Mounting Pad

Turbine Department [email protected]

67

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Off-Skid Control Console

Turbine Department [email protected]

68

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Mars Driver Full Enclosure

Turbine Department [email protected]

69

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Fire Control Operator Interface

Turbine Department [email protected]

70

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Gas Compressor and Yard Valve

Turbine Department [email protected]

72

Onshore Compression P&ID

Gas Compressor

Dry Gas Seal

Nitrogen Package

Yard Valve Components

Yard valve sequence

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Gas Compressor Barrel type Turbine Department [email protected]

73

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Gas Compressor Internal parts Turbine Department [email protected]

74

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Gas Compressor Turbine Department [email protected]

75

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Dry Gas Seal location Turbine Department [email protected]

76

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Dry Gas Seal capsule Turbine Department [email protected]

77

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Dry Gas Seal working Principle Turbine Department [email protected]

78

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Nitrogen Package Turbine Department [email protected]

80

Generon Nitrogen package

Nitrogen P&ID

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Turbine Operation

Turbine Department [email protected]

81

HMI Screens D2D

HMI screen turbine

Normal , Alarm & Shutdown Reading

Start up program

Turbine Flow Diagram

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Turbine Discussion

Turbine Department [email protected]

82