Challenges in welding Technology: Space scenario
- Dr. P. V. Venkitakrishnan
- Dy. Director
Materials and Mechanical Entity Vikram Sarabhai Space Centre, ISRO, Trivandrum
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CII Welding conference 2016, Mumbai 16th November, 2016
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
Materials and Mechanical Entity Vikram Sarabhai Space Centre, ISRO, Trivandrum
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CII Welding conference 2016, Mumbai 16th November, 2016
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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
LB EB Plasma TIG
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Considerations and requirements for weldments of aerospace systems
In general industries there is more emphasis
instead of MIG.
acceptable defects
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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Gas Tungsten Arc welding (GTAW) Electron Beam Welding (EBW) Laser Beam Welding (LBW)
Gas Tungsten Arc Welding (GTAW)
tungsten electrode and a work piece
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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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Current, voltage, speed, wire feed are controlled automatically
Welding of Motor Cases – cont…
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* Properties required : High strength and high fracture toughness (75 MPa√ m) * To achieve consistent properties :
Current : 230 + 1 Ampere
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.
Propellant Tank realisation
Why DCSP ?
DCRP DCSP
High Depth to width ratio
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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
problem during welding is porosity
remove oxide
in welding, to minimise this loss, welding with lowest possible heat input
DCSP- GTAW process
Key controlled parameters include:
EBW
PS4 gas bottle
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Forged hemispheres
are made of titanium alloy (Ti-6Al-4V)
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
Laser welding done here
thick aluminum alloy
located close to the weld area
a low heat input process – LASER BEAM WELDING used
LASER WELDING – LITHIUM BATTERIES
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
application with a power reduction aperture
velocity through the use of chemical explosives.
Drawbacks:
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
Al SS
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
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)
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
1400 rpm
solid state bonding process
and temperature
diffusion of atoms
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
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
Two components are held together, and oscillatory shear stresses of ultrasonic frequency are applied to interface to cause coalescence
intimate contact and strong metallurgical bonding between surfaces
Li-ion batteries
20 micron thickness
the main tab [1 mm]
bunch of 10-20 foils
JOINING FOIL ELECTRODES IN Li-ION BATTERIES: ULTRASONIC WELDING
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Sea level Thrust Chamber Assembly : Major parts
Convergent inner shell
milling Nickel ring
Divergent inner shell
Manifold
Convergent outer shell
Divergent outer shell
TYPICAL BRAZING CYCLES
Time Time
5000C 10300C 9800C 9750C 11800C 12300C 950 0C Switch
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
temp stabilises
Convergent- Divergent Assembly Second Divergent Assembly
FIXTURE FOR ROTARY VACUUM BRAZING
TECHNOLOGY DEVELOPMENT
PROBLEMS FACED
Initial hardware lost due to brazing failure
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
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 10VACUUM BRAZING OF 1151-130 AY IN RVBF
ROTATION VACUUMFacility
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
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.
there is a need to create common forum to resolve challenges of dissimilar metal and advanced material joining.
involving metal joining can be explored for costly and strategic materials.
taken up to further reduce the cost of welding.
additional confidence of crack free weld using techniques like ultrasonic inspection.
higher side ~ 50 yrs, which need to be brought down to younger generations.