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Newsletter  2015.12  Index

Theme : "Mechanical Engineering Congress, 2015 Japan (MECJ-15) Part 2"

  1. Preface
    T.TAKEMURA, I.KINEFUCHI, H.FUJII, H.YOKOYAMA
  2. Development of CFD for Design Problems of Fluid System
    Kazuhiro TANAKA (Kyushu Institute of Technology)
  3. Workshop on Innovative Development of Frontier Fluids Engineering based on Functional Fluids Research
    Hidemasa TAKANA, Hideya NISHIYAMA (Tohoku University)
  4. Applications of Plasma Flow and Ionic Liquid to Energy Technologies
    Hidemasa TAKANA (Tohoku University)
  5. Bioengineering Application of Electro-conjugate Fluid
    Kenjiro TAKEMURA (Keio University)
  6. Development of Innovative Energy Conversion and Control using Magnetic Functional Fluids
    Yuhiro IWAMOTO (Doshisha University)
  7. Advanced Energy and Aerospace Technologies using Magnetohydrodynamics
    Takayasu FUJINO (University of Tsukuba)

 

Advanced Energy and Aerospace Technologies using Magnetohydrodynamics


Takayasu FUJINO
University of Tsukuba

Abstract

Advanced Energy and Aerospace Technologies using Magnetohydrodynamics
Magnetohydrodynamics(MHD) is concerned with an interaction between electrically conducting fluids and electromagnetic field. MHD power generator is one of engineering applications of Magnetohydrodyanmics. MHD power generator is based on Fleming’s right-hand rule, that is, electro motive force is induced by the movement of conducting fluids such as plasma and liquid metal under an externally applied magnetic field. The MHD power generator has no moving parts unlike steam and gas turbine generators, so that it can use high temperature heat sources above 2000 K. Therefore, a power plant using MHD power generator is expected to has a conversion efficiency higher than that of the current most-advanced combined cycle power plants.

Figure 1 shows the conceptual configuration of closed-cycle MHD power plant(CCMHD). In the CCMHD, noble gas seeded with a small amount of alkali metal vapor is generally utilized as working gas. This power plant targets the total efficiency of 60 %. The performance of MHD power generator required for realizing this system is the enthalpy extraction ratio (E.E.) of 30% and the isentropic efficiency of more than 80%. Figure 2 depicts the recent results of high performance noble gas MHD power generation experiments which were conducted in Tokyo Institute of Technology. The enthalpy extraction ratio has already reached the target value of 30%. However, the isentropic efficiency obtained in the experiments was low compared with the target value. Therefore, the most important issue in future research for the realization of CCMHD is the improvement in isentropic efficiency.

Recently, a number of feasibility studies on applications of MHD on aerospace engineering field have been conducted by a lot of researchers in the US, Russia, Italy, Japan and many other nations. As one of the MHD applications, the active heat shield in Earth reentry and other atmospheric planetary entry flights, which is called “MHD flow control” or “MHD heat shield, has been proposed. In MHD flow control, a magnetic field is applied to a weakly ionized plasma flow in shock layer ahead of an entry vehicle, as shown in Fig. 3. The interaction between the magnetic field and the plasma flow induces the Lorentz force. The plasma flow is retarded by the Lorentz force, which leads to the enlargement of shock layer and the reduction of velocity gradient in a boundary layer around the vehicle. Consequently, the convective heating is mitigated by MHD flow control. Furthermore, the reaction force of the Lorentz force acts on a magnet installed in the vehicle, and as a result, a drag force can be increased by MHD flow control and a flight velocity can be reduced by it. Both the effects of shock layer enlargement and flight velocity reduction lead to mitigate convective aerodynamic heating.

The author has studied the possibility and usefulness of MHD flow control by means of magnetohydrodynamic numerical simulation. Figures 4 and 5 show examples of our numerical simulation results, which indicate the influence of MHD flow control on shock layer and convective wall heat flux, respectively, in the situation of Earth reentry flight. These figures successfully demonstrate the idea of MHD flow control and a considerable mitigation of convective wall heat of reentry vehicle by MHD flow control.

 

Key words

Magnetohydrodynamics, MHD power Generator, MHD flow control

 

Figures


Fig. 1 Conceptual Configuration of Closed Cycle MHD Power Plant.


Fig.2 Performance Data of High Performance Noble-Gas MHD Power Generation Experiments in Tokyo Institute of Technology.


Fig.3 Conceptual Illustration of MHD Flow Control


Fig.4 Influence of MHD Flow Control on Shock Layer in Earth Reentry Flight


Fig.5 Influence of MHD Flow Control on Wall Heat Flux in Earth Reentry Flight

Last update: 12.16.2015