Sample of Our Projects
| Field | Model Name | Date | Client |
|---|---|---|---|
| Architecture Aerodynamics | Japanese Temple Multipoint Pressure Measurement Model | May-09 | Shimizu Institute of Technology |
| Characteristics | image | ||
| Super Precise Reproduction Model Architectural aerodynamic test model with curved face 420 point high density multipoint pressure measurement Pressure measured on face & back @3mm thickness |
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| Field | Model Name | Date | Client |
|---|---|---|---|
| Airplane | Airplane landing gear model for noise measurement | Oct-09 | JAXA Airplane Group & Nippon Univ. |
| Characteristics | image | ||
| Small gear model 28 removable pieces |
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| Field | Model Name | Date | Client |
|---|---|---|---|
| Architecture Aerodynamics | Dome model | Jan-10 | Shimizu Institute of Technology |
| Characteristics | image | ||
| 170 point pressure measure points Pressure transmission with separate tubes |
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| Field | Model Name | Date | Client |
|---|---|---|---|
| Airplane | Gas turbine internal flow reproduction system | Mar-10 | JAXA Airplane Group |
| Characteristics | image | ||
| Stereolithography+powder molding+aluminum internal flow reproduced with DC motor Internal flow measured w/ 16 probes in direction of circumference |
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| Field | Model Name | Date | Client |
|---|---|---|---|
| Wind Power Generator | Design of vertical axis wind power generator | Mar-10 | GTI Ltd. |
| Characteristics | image | ||
| Commission of vertical axis wind mill plan Improvement in low speed start-up characteristic Anti-over rev aero brake |
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| Field | Model Name | Date | Client |
|---|---|---|---|
| Airplane | Supersonic passenger airplane low speed aerodynamic model | Aug-10 | JAXA Airplane Group |
| Characteristics | image | ||
| Stereolithography on wing + aluminum on body Pressure measurement aperture 20 points on main wing, 16 points on body placed Pressure measurement aperture placed on aft edge of main wing with 1mm thickness |
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| Field | Model Name | Date | Client |
|---|---|---|---|
| Spaceship | Supersonic wind tunnel tester | Nov-10 | Tottori Univ. Dept. of Engineering |
| Characteristics | image | ||
| Powder molding High attack angle supersonic (Mach 4) airflow test |
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| Field | Model Name | Date | Client |
|---|---|---|---|
| Spaceship | BOV3 Spaceship for technical demo | Mar-10 | JAXA Airplane Group |
| Characteristics | image | ||
| Stereolithograph RCS parts (Jet flow control parts) molded with high pressure air exhaust nozzle Engine air intake with powder molding main part of the bodywork in aluminum alloy machining (70 series) |
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