Overview of the Japanese National Project for Super/Hyper-Sonic Transport Propulsion System

1992 ◽  
Author(s):  
Osamu Ichimaru ◽  
Makoto Ishizuka ◽  
Kanji Muhashima
Keyword(s):  
Research And Development ◽  
High Performance ◽  
Science And Technology ◽  
Propulsion System ◽  
National Project ◽  
Ramjet Engine ◽  
Turbojet Engine ◽  
Project Forecasting ◽  
Industrial Science

The Agency of Industrial Science and Technology (AIST), MITI of Japan, started research and development on a super/hypersonic transport propulsion system in FY1989 as an eight year project. The project, forecasting a flight cruise capability of up to Mach 5, aims at establishing basic technologies for an engine that combines a ramjet engine and a high performance turbojet engine. This paper presents the background, objective, organization, contents, etc., of this national project.

Current Status of Advanced Reheat Gas Turbine AGTJ-100A: Part 3 — Experimental Results of Shop Tests

1984 ◽  
Author(s):  
Kazuo Takeya ◽  
Yasuo Oteki ◽  
Hajime Yasui
Keyword(s):  
International Trade ◽  
Research And Development ◽  
Gas Turbine ◽  
Pilot Plant ◽  
Science And Technology ◽  
Experimental Results ◽  
Current Status ◽  
Technical Problems ◽  
Industrial Science

The outline of plans for the research and development of an advanced reheat gas turbine under the Moonlight Project (Agency of Industrial Science and Technology, Ministry of International Trade and Industry) has already been announced in 1981 at Houston (81-GT-28), while technical problems related to the pilot plant (Paper No. 83-TOKYO-IGTC-117) as well as performance and characteristics (Paper No. 83-TOKYO-IGTC-40) have been announced at the 1983 Tokyo International Gas Turbine Congress. No-load shop tests conducted on the pilot reheat gas turbine during the period of May to July, 1983, were consummated with highly satisfactory results, so this paper is dedicated primarily to giving a description of the shop tests.

Using roadmaps for evaluating strategic research and development: lessons from Japan's Institute for Advanced Industrial Science and Technology

2008 ◽  
Vol 17 (4) ◽  
pp. 265-271 ◽  
Author(s):  
Osamu Nakamura ◽  
Shinichi Ito ◽  
Kunio Matsuzaki ◽  
Hironori Adachi ◽  
Tetsuo Kado ◽  
...  
Keyword(s):  
Research And Development ◽  
Science And Technology ◽  
Strategic Research ◽  
Industrial Science

Fundamental Magnesium Researches in Japan

2005 ◽  
Vol 488-489 ◽  
pp. 9-16 ◽  
Author(s):  
Yo Kojima ◽  
Shigeharu Kamado
Keyword(s):  
Research And Development ◽  
Magnesium Alloys ◽  
High Performance ◽  
Large Scale ◽  
Mechanical Performance ◽  
Science And Technology ◽  
Base Material ◽  
Joint Research ◽  
Practical Utilization ◽  
Research Fields

In the current four-year term project in Japan, new platform science and technology is proposed as a core concept of research and development of advanced magnesium alloys together with understanding of their intrinsic characteristics. The research fields related to advanced super-light magnesium alloys for 21st Century have been focused to the selected three categories; ecomaterial design and processing, high qualification of mechanical performance, and high performance design and processing in functionality. On the basis of the obtained results, platform science and technology for environmentally benign and high performance magnesium alloys is constructed as an industrial base material for the next generation. As a result, numerous large-scale joint research and development projects on magnesium alloys based on partnerships between industries, academia and government has already started towards practical utilization since last year.

scholarly journals Inter-laboratory comparison between NMIJ and KRISS of calibration capabilities for torque measuring devices in the range from 50 N·m to 2 kN·m

ACTA IMEKO ◽  
2017 ◽  
Vol 6 (2) ◽  
pp. 21
Author(s):  
Koji Ogushi ◽  
Atsuhiro Nishino ◽  
Kazunaga Ueda ◽  
Min-Seok Kim ◽  
Yon-Kyu Park
Keyword(s):  
High Performance ◽  
Science And Technology ◽  
National Metrology Institute ◽  
Small Deviations ◽  
Measuring Devices ◽  
Calibration And Measurement Capabilities ◽  
Korea Research Institute ◽  
Calibration Unit ◽  
Measurement Capabilities ◽  
Industrial Science

<p class="Abstract">An inter-laboratory comparison of the calibration capability for torque measuring devices (TMDs) was conducted between the National Metrology Institute of Japan (NMIJ) in the National Institute of Advanced Industrial Science and Technology (AIST) and the Korea Research Institute of Standards and Science (KRISS). Three high-performance torque transducers having rated capacities of 100 N·m, 1 kN·m, and 2 kN·m, and a bridge calibration unit (BN100A) were used as the transfer devices. The 1 kN·m and 2 kN·m transducers had one bridge, but the 100 N·m transducer had two bridges that acquired data more reliably. An identical indicator/amplifier type (DMP40) owned by each laboratory was used. All of the transducers and BN100A were transferred from NMIJ to KRISS. For the comparison, NMIJ used 1 kN·m and 20 kN·m deadweight torque standard machines (TSMs), and KRISS used a 2 kN·m deadweight TSM. In particular, the capability of the 1 kN·m TSM at NMIJ was examined after some improvements. In the calibration range from 50 N·m to 2 kN·m, relative deviations were less than 3.0 × 10<sup>-5</sup> for increasing torques. Sufficiently small deviations were obtained between the calibration results in the two laboratories, as compared with their calibration and measurement capabilities (CMCs), which were 3.5 × 10<sup>-5</sup> for the 1 kN·m TSM at NMIJ, 7.0 × 10<sup>-5</sup> for the 20 kN·m TSM at NMIJ, and 5.0 × 10<sup>-5</sup> for the 2 kN·m TSM at KRISS (as relative expanded uncertainties).</p><p class="Abstract"> </p>

Driving Taiwanese science and technology research

Impact ◽  
2020 ◽  
Vol 2020 (6) ◽  
pp. 4-5
Author(s):  
Dar-Bin Shieh
Keyword(s):  
Research And Development ◽  
Science And Technology ◽  
Technology Research ◽  
Technological Research ◽  
Deputy Minister

Professor Dar-Bin Shieh, Deputy Minister at the Taiwan Ministry of Science and Technology, shares with us details of the efforts undertaken at the Ministry to promote and support scientific and technological research and development in Taiwan, including his response to the COVID-19 pandemic

A novel hybrid aircraft propulsion based on the DEA compressor—Part A: Design

2021 ◽  
pp. 095441002110253
Author(s):  
Babak Aryana
Keyword(s):  
High Performance ◽  
Static Condition ◽  
Propulsion System ◽  
Hybrid Propulsion ◽  
Pulse Detonation ◽  
Low Emission ◽  
Wide Range ◽  
Exit Nozzle ◽  
Distributed Propulsion ◽  
Detonation Process

This two-part article introduces a novel hybrid propulsion system based on the DEA compressor. The system encompasses a Pulse Detonation TurboDEA as the master engine that supplies several full-electric ancillary thrusters called DEAThruster. The system, called the propulsion set, can be categorized as a distributed propulsion system based on the design mission and number of ancillary thrusters. Part A of this article explains the design process comprising intake, compressor, detonation process, diffuser, axial turbine, and the exit nozzle. The main target is to design a high-performance low emission propulsion system capable of serving in a wide range of altitudes and flight Mach numbers that covers altitudes up to 20,000 m and flight Mach number up to the hypersonic edge. Designing the propulsion set, the design point is considered at the static condition in the sea level. Design results show the propulsion set can satisfy all requirements necessary for its mission.

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