Functional Compound Combustion Synthesis under Centrifugal Force and - - PowerPoint PPT Presentation

functional compound combustion synthesis under
SMART_READER_LITE
LIVE PREVIEW

Functional Compound Combustion Synthesis under Centrifugal Force and - - PowerPoint PPT Presentation

Finnish-Japanese Workshop on Functional Materials May 25-26, 2009 / Espoo and Helisinki, Finland Functional Compound Combustion Synthesis under Centrifugal Force and Microgravity Osamu Odawara Dept. Innovative & Engineered Materials, Tokyo


slide-1
SLIDE 1

Functional Compound Combustion Synthesis under Centrifugal Force and Microgravity

Osamu Odawara

  • Dept. Innovative & Engineered Materials, Tokyo Institute of Technology

E-mail: odawara.o.aa@m.titech.ac.jp

Finnish-Japanese Workshop on Functional Materials

May 25-26, 2009 / Espoo and Helisinki, Finland

Combustion Synthesis < Centrifugal Force > composite-layer formation < Microgravity > fine composite formation Highly Potential Materials Synthesis

Reaction propagation Thermal expansion Products wetness Thermal convection

slide-2
SLIDE 2

Centrifugal-Thermite Process

30 mmφ x 100 mm 〜 500 mmφ x 6,000 mm

3MeO + 2Al Al2 O3 + 3Me + Q

Centrifugal force applied for forming composite layered pipes (Centrifugal-casting technology) + Thermite reaction achieving for self-sustaining high-temperature reaction

For casing pipes on geothermal energy utilization For pipes against erosion-corrosion

slide-3
SLIDE 3

Al Fe SEI BEI

Outer metal layer Product layers metal ceramic

Fe2 O3 + 2Al Al2 O3 + 2Fe + Q

slide-4
SLIDE 4
slide-5
SLIDE 5
slide-6
SLIDE 6

(D) (E)

slide-7
SLIDE 7
slide-8
SLIDE 8

Functionally Graded Materials Project

slide-9
SLIDE 9
slide-10
SLIDE 10

Dilute magnetic compounds: Mn-InP and Mn-(Ga, In)P

μg 1g

Optoelectronic compounds: GaP, InP and CuInS2

5 μm 5 μm

Micro-gravitational Combustion Synthesis

Light-induced ferromagnetism lightening

magnetic semiconductor magnetic semiconductor

iron

2xGa2 O3 + 2(1-x) In2 O3 + 8P = 4Gax In(1-x) P + P4 O6 3Cu2 O + 3In2 O3 + 12S + 8P = 6CuInS2 + 2P4 O6

slide-11
SLIDE 11

Space-DRUMS Space-Dynamically Responding Ultrasonic Matrix System

  • Short, Shaped, Ultrasonic Acoustic Pulses Projected at Sample
  • Acoustic Beam Focused by Shaped Transducer
  • Reflecting Wave Packet Transfers Momentum to Sample
  • Pulses Digitally Controlled by Video Cameras in Feedback Loop

Dynamic Acoustic Dynamic Acoustic

Acoustic Projector Wave Packet Sample

Retractable Sample Insertion Rod and Igniter Sample, Electrically Ignited Sample Viewed by 3 Orthogonal IR Video Cameras in Feedback Loop with Acoustic Projectors 20 Acoustic Projectors at Vertices of Dodecahedron

slide-12
SLIDE 12

[Activity Plan of Space Combustion Synthesis Working Group] [Activity Plan of Space Combustion Synthesis Working Group]

Japan Research Association on Combustion Synthesis Innovative Research WG, Tokyo Tech.

Technology Transfer to JEM/ISS Programs

R&D on In-situ Resource Utilization and In-space Fabrication&Repair

< Branding of Space Combustion Synthesis > System Factor : advanced with external forces

[ignition-propagation-formation]

External Factor: efficient to reaction propagation

[gravity-pressure-composition]

Space Combustion Synthesis WG

Inert Combustion Synthesis Experiments

{Key Tech.: Heat and Mass Transport after ignition} {Int’l. Corp. Scenario: Application of SpaceDRUMS}

<Advanced Combustion Synthesis>

Energy saving

(self sustaining high temperature zone)

Reaction heat control

(exothermic chemical oven)

Easy performance

(ignition and wave front formation)

Rapid temperature increase

( tens mm/s in velocity)