Technology: Space scenario Dr. P. V. Venkitakrishnan Dy. Director - - PowerPoint PPT Presentation

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Technology: Space scenario Dr. P. V. Venkitakrishnan Dy. Director - - PowerPoint PPT Presentation

Challenges in welding Technology: Space scenario Dr. P. V. Venkitakrishnan Dy. Director Materials and Mechanical Entity Vikram Sarabhai Space Centre, ISRO, Trivandrum CII Welding conference 2016, Mumbai 16 th November, 2016 1 Outline of talk


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SLIDE 1

Challenges in welding Technology: Space scenario

  • Dr. P. V. Venkitakrishnan
  • Dy. Director

Materials and Mechanical Entity Vikram Sarabhai Space Centre, ISRO, Trivandrum

1

CII Welding conference 2016, Mumbai 16th November, 2016

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SLIDE 2

Outline of talk

  • Introduction : Welding Processes
  • Fusion welding and its Applications
  • Solid state welding and its Applications
  • Brazing and its Applications
  • Welding Institutes
  • Future directions

2

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SLIDE 3

Welding Processes

3

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SLIDE 4

Types of Welding Processes

Almost 50 types of welding processes exist Can be categorized into two major classes Fusion welding : Joining is accomplished by melting of the two parts to be joined. Filler metal is added if necessary Examples : TIG Welding, Laser welding, Electron Beam welding, submerged arc welding, gas welding Solid state welding : Heat/pressure are used for joining but no melting of base metals occurs. No filler material is added. Examples: Friction welding, Friction Stir welding, Ultrasonic welding, Diffusion Bonding, Explosive bonding

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SLIDE 5

COMPARISON OF FUSION WELDING PROCESSES

LB EB Plasma TIG

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SLIDE 6

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Considerations and requirements for weldments of aerospace systems

  • Emphasis on quality with minimum defects .

In general industries there is more emphasis

  • n productivity.
  • Choice of process important. TIG preferred

instead of MIG.

  • Joining of dissimilar metals required
  • Extensive NDT is done to ensure joints with

acceptable defects

  • Repair welding is practiced and is essential
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SLIDE 7

Welded components in PSLV

Strap on motor case ,15CDV6 steel (GTAW) PS1 motor case 18Ni250 maraging steel (GTAW) AA2219 tank (PS2) (GTAW/ FSW) Bimetallic adaptor (Explosive bonding/ FSW) Ti-6Al-4V tanks (PS4) (EBW) Ti-6Al-4V Gas bottles (EBW) BMA (Friction welding)

Battery cases (GTAW/ LBW/ Ultrasonic welding)

PS2 Engine impellor (Diffusion bonding)

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SLIDE 8

Important Fusion welding Techniques

8

Gas Tungsten Arc welding (GTAW) Electron Beam Welding (EBW) Laser Beam Welding (LBW)

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SLIDE 9

Gas Tungsten Arc Welding (GTAW)

  • Also known as Tungsten Inert Gas (TIG) welding
  • Uses an arc between a non consumable

tungsten electrode and a work piece

  • Shielding is obtained from a inert gas like Argon
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SLIDE 10

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Welding of Motor Cases

Propellant (Chemical energy) Igniter Hot Gases (Heat energy) High velocity Gases (Kinectic Energy) Nozzle

Material : M250 Maraging steel (Fe-Ni-Co-Mo)

This is a high strength steel [Yield strength- 1800 MPa]

Size : 2800 mm dia Height of one shell : 1500 mm

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SLIDE 11

11

  • Total Weld length : 60 Metres
  • To have uniformity , Auto-TIG process used

Current, voltage, speed, wire feed are controlled automatically

Welding of Motor Cases – cont…

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SLIDE 12

12

* Properties required : High strength and high fracture toughness (75 MPa√ m) * To achieve consistent properties :

  • Close control of parameters , e.g.

Current : 230 + 1 Ampere

  • Interpass cleaning
  • Overall process cleanliness
  • Use of high purity Ar gas (4 ppm of oxygen max.)

Welding of Motor Cases – cont..

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SLIDE 13

WELDING PROCESS

Selected Process: DCSP –TIG

For Propellant Tank realisation

Why DCSP ? Aim :

To achieve 180 MPa( min) without any post weld treatment and with R1 repair. Change over to DCSP TIG from AC TIG yielded a payload gain of 41 Kg.

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SLIDE 14

Propellant Tank realisation

Why DCSP ?

DCRP DCSP

High Depth to width ratio

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SLIDE 15

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Welding of LOX, LH2 and L40 tanks

Material : AA 2219 Aluminum Alloy This is a Aluminum- copper alloy with good properties at cryogenic temperatures

  • Aluminum alloys – main

problem during welding is porosity

  • Rigorous cleaning with alkali to

remove oxide

  • Mechanical properties reduction

in welding, to minimise this loss, welding with lowest possible heat input

DCSP- GTAW process

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SLIDE 16

Key controlled parameters include:

  • Speed of the electrons (ACCELERATING VOLTAGE)
  • Number of electrons in the beam (BEAM CURRENT)
  • Energy density at the joint (FOCUS)
  • Speed of welding (TIME)

EBW

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SLIDE 17

PS4 gas bottle

17

Forged hemispheres

  • High Pressure Gas bottles/ propellant tanks

are made of titanium alloy (Ti-6Al-4V)

  • Titanium has low density

Titanium – highly reactive to oxygen/ nitrogen GTAW welding – poor quality welds Welding in vacuum required Electron beam welding is the best choice

TITANIUM ALLOY GAS BOTTLES - EBW

PS4 propellant tank

INSAT/ GSAT tank

PS2 gas bottle

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SLIDE 18

LASER BEAM WELDING

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SLIDE 19

Laser welding done here

  • Lithium–ion batteries for satellites
  • Cell casing made of 1mm

thick aluminum alloy

  • Separators made of polymer

located close to the weld area

  • To minimise damage to polymer,

a low heat input process – LASER BEAM WELDING used

LASER WELDING – LITHIUM BATTERIES

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SLIDE 20

Wire sizing, Globule formation, flattening& Welding Process

Cryo Initiator Bridge wire Welding

Wire holding fixture Laser beam

Punch &Die for Globule flattening

Laser beam Inert Gas chamber Laser welded Initiators

  • Source : 400W Pulsed Nd:YAG laser.
  • Tailored the workstation for microwelding

application with a power reduction aperture

  • Wire : 80micron/ Nichrome
  • A dedicated facility established in VSSC
  • Flight proven in GSLV F05
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SLIDE 21

Explosive bonding Ultrasonic welding

Important Solid state Welding

Friction Stir welding Diffusion Bonding Friction welding

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SLIDE 22

Explosive bonding

  • Welding is accomplished by accelerating one of the components at extremely high

velocity through the use of chemical explosives.

Drawbacks:

  • Low joint strength in tension
  • High fabrication cost
  • Material wastage
  • Low yield because of defects
  • Hazardous process
  • Noise and vibration
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SLIDE 23

Explosive bonding for bimetallic adaptors

Features of explosive bonding: (i) Interfacial pressure of 102 Mbar maintained for few microseconds & diffusion rate is small. (ii) Jet formation removes surface defects/ contaminations.

Al alloy AA2219 – stainless steel 12X18H10T (ICSS 321) with interlayer of Al

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SLIDE 24

Friction welding

Al SS

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SLIDE 25

Friction Stir Welding

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SLIDE 26

Major Considerations in Tool Configuration

  • Strength
  • Ratio of swept volume to static volume
  • Minimum slip
  • Shear layer velocity
  • Minimum flash

Approximate Heat Input Linear Velocity at shoulder periphery – 1.3 m/s Linear velocity at extreme end of probe – 0.5 m/s (Sq probe) Energy due to friction heat – 4220 W Energy due to interfacial shear stress – 477 W NEW RETRACTABLE TOOL

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SLIDE 27

Photographs of the Al-SS joints

Al Al Al Al SS SS SS Friction surfaced coating of AA2014 CMT welding of AA4047

Alternate option for Bi-metallic joining by using Friction stir + Cold metal transfer (FS+CMT)

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SLIDE 28

Examples of joints

Step 1: Annealing of AA2219-T87 base material Step 2: Bending of AA2219 and AISI321 base materials Step 3: Joining of AA2219 aluminium alloy (Al/Al) Step 4: Post weld heat treating of AA2219 joints to T6 condition Step 5: Joining of AISI321 stainless steel (SS/SS) Step 6: Joining of AISI321 and AA2219 joints (SS/Al) - a plus shaped coupon

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SLIDE 29

Microstructure at different rpm of tool

1400 rpm

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SLIDE 30

Diffusion Bonding

  • Diffusion bonding is a

solid state bonding process

  • Process under pressure

and temperature

  • Bonding happens by

diffusion of atoms

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SLIDE 31

Impeller body and cover parts before bonding Material : Titanium alloy Diffusion bonding parameters Temp 9600C Time 2.5 Hrs Load 3Ton

Diffusion bonding on LH2 impeller

100X

Vacuum Hot Press

Capacity : 250 T

Bond interface

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SLIDE 32

CERAMIC + METAL JOINING

Oxides : Al2O3, ZrO2, Nitrides : Si3N4, AlN Carbide : SiC, Al & Ni are used as interlayers Required duration : 2–4 s Welding pressure : 10–30 MPa Si3N4 + Al (interlayer) + Cu used as inserts Al2O3 + Cu Used in terminal seal Li-ion batteries

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SLIDE 33

ULTRASONIC WELDING

Two components are held together, and oscillatory shear stresses of ultrasonic frequency are applied to interface to cause coalescence

  • Oscillatory motion breaks down any surface films to allow

intimate contact and strong metallurgical bonding between surfaces

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SLIDE 34

Li-ion batteries

  • Positive electrodes – aluminum foils of

20 micron thickness

  • Negative electrodes - pure copper foils
  • f 20 micron thickness
  • These electrodes have to be joined to

the main tab [1 mm]

  • Ultrasonic welding used to to make a

bunch of 10-20 foils

JOINING FOIL ELECTRODES IN Li-ION BATTERIES: ULTRASONIC WELDING

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SLIDE 35

Brazing

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Rotary vacuum brazing Static brazing

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SLIDE 36

Sea level Thrust Chamber Assembly : Major parts

Convergent inner shell

  • Cu alloy plates
  • Deep forming
  • Profile machining
  • 5 axis Channel

milling Nickel ring

  • Ring forging
  • Machining
  • EDM

Divergent inner shell

  • Cu alloy plates
  • Deep forming
  • Profile machining
  • 5 axis machining

Manifold

  • SS sheets 4 mm
  • Forming

Convergent outer shell

  • SS shaped forging
  • Machining

Divergent outer shell

  • SS shaped forging
  • Machining
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SLIDE 37

TYPICAL BRAZING CYCLES

Time Time

5000C 10300C 9800C 9750C 11800C 12300C 950 0C Switch

  • ff power

850 0C VP on 5 min 5 min 1130 0C Switch off power 900 0C VP on 1-8 min till temp stabilises 0-8 min

  • r till

temp stabilises

Convergent- Divergent Assembly Second Divergent Assembly

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SLIDE 38

FIXTURE FOR ROTARY VACUUM BRAZING

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SLIDE 39

TECHNOLOGY DEVELOPMENT

PROBLEMS FACED

  • Cracks noticed on the steel outer shell.
  • Blockages noticed inside the channels.
  • Bulging during hydro test (de-bond).
  • Thermocouple failure.
  • Fixture problems.
  • Induction heating related problems.
  • PLC problems.
  • Facility related issues.

Initial hardware lost due to brazing failure

  • Material, Structural, Thermal,

Instrumentation, Vac. system, Furnace Engg, Electrical, Electronics, Process Engg.

SYNERGISING MULTI- DISCIPLINARY EXPERTISE IN-HOUSE & OUTSIDE Modifications in Process, material, fixture design, facility tune-up, procedure, review

  • SUCCESSFUL BRAZING
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SLIDE 40

ROTARY VACUUM BRAZING for Cryo Thrust Chamber

INNER CHAMBER BRAZE FOIL OUTER SHELL COOLING CHANNELS

Complex process as it involves precise control of many variables like temperature, time, vacuum, pressure and rotational speed

VACUUM 10
  • 2
VACUUM 10
  • 2
RADIATION RADIATION INDUCTION COILS ARGON Pr. Pr. Pr. Pr. MUFFLE

VACUUM BRAZING OF 1151-130 AY IN RVBF

ROTATION VACUUM

Facility

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SLIDE 41

Static vacuum compression brazing furnace

Static brazing process using electroplated Cu and Ag for the Semi-Cryo engine realization

Hardware after copper and silver coating a) Outer shell (03X12H10T) b) Inner shell (Cu-Cr-Zr-Ti)

a) b)

Hardware as dismantled

Hardware welded for vacuum lines

Hardware assembly wrapped with heating pad for brazing

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SLIDE 42

Major welding Institutions in India

  • WRI/ BHEL, Trichy
  • IGCAR, Kalpakkam
  • VSSC, Triavndrum
  • BATL, Trivandrum
  • BARC, Mumbai
  • Godrej, Mumbai
  • Walchandnagar industries Ltd.
  • L&T Mumbai
  • ARCI, Hyderabad
  • NML, Jamshedpur
  • DMRL, Hyderabad
  • IISc, Bangalore
  • IIT, Madras, IIT, Kharagpur, Other IITs and NITs
  • R&D Tata Steel Jamshedpur
  • Professional institutions: IIW Kolkata, ISW Delhi, ESAB

Objectives of professional institutions Application of various welding processes catering to the appropriate needs of industries. Dissemination of knowledge in welding and allied areas through Training, documentation services, publications. Collaborative research in areas specific to any industry or a cluster of industries. Technology diffusion to Industry and the individual. Promote health & safety in welding.

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SLIDE 43

Future Directions……….

  • Several institutes and industries are involved in welding. But,

there is a need to create common forum to resolve challenges of dissimilar metal and advanced material joining.

  • Evolution of alternate and cost effective method of fabrication

involving metal joining can be explored for costly and strategic materials.

  • Indigenisation of welding consumables and equipment can be

taken up to further reduce the cost of welding.

  • Concerted efforts required in the area of non-destructive testing
  • f weldment and post weld heat treatment especially to provide

additional confidence of crack free weld using techniques like ultrasonic inspection.

  • Towards human resources, average age of people involved is on

higher side ~ 50 yrs, which need to be brought down to younger generations.

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SLIDE 44

Th Than ank k Yo You