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公开(公告)号:JPH08316533A
公开(公告)日:1996-11-29
申请号:JP14688695
申请日:1995-05-23
Applicant: NAT AEROSPACE LAB
Inventor: SUDO TAKAYUKI , CHIN RITSUTOU , KIZARA KATSUHITO , KUMAGAI TATSUO
Abstract: PURPOSE: To provide a thermoelectric element performance evaluation method and a device, wherein a one-dimensional heat flow condition can be realized so as to accurately evaluate the performance of a thermoelectric element of gradient structure under a condition of large temperature difference. CONSTITUTION: A thermoelectric element arranged between a primary heat source 2 and a cooling source to measure a thermoelectromotive force or the like is surrounded with a heat shield 7, and an auxiliary heat source 3 is provided to heat the outside of the heat shield 7 from across so as to make the temperature distribution of the heat shield 7 nearly equal to a temperature distribution induced in the thermoelectric element due to a temperature difference between the primary heat source 2 and the cooling source. A temperature distribution around the thermoelectric element is set nearly equal to that of the element, whereby the thermoelectric element is kept under a condition of one-dimensional heat flow.
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公开(公告)号:JP2003227784A
公开(公告)日:2003-08-15
申请号:JP2002024716
申请日:2002-01-31
Applicant: NAT AEROSPACE LAB
Inventor: YOSHIDA MAKOTO , NOSAKA MASATAKA , SUDO TAKAYUKI , KIKUCHI MASATAKA , SATO MASAKI , TAKADA HITOSHI
Abstract: PROBLEM TO BE SOLVED: To provide a stress-testing method and a stress-testing apparatus for greatly improving the evaluation of a light material such as a compound material by allowing a stress state to be solved in a state of including the lamination structure of a shell-like specimen and end face treatment and obtaining the temperature dependency of the amount of permeation of helium. SOLUTION: A shell-like specimen 1 comprising a carbon-fiber reinforced resin-based compound material that is used for a thin shell structure is fixed to an apparatus body 11, and the pressure of a helium gas supplied to a pressure chamber 21 is allowed to operate on the recessed surface side of a dome section 2 in the shell-like specimen 1. The displacement in a top section 2a of the dome section 2 is detected by a laser displacement meter 12. The shell-like specimen 1 is cooled to an arbitrary temperature via a partition board 18 that is cooled by an extremely low-temperature fluid supplied to a cooling chamber 22. The amount of the helium gas through the shell-like specimen 1 is detected by a helium leakage detector 33 for sucking through a negative pressure chamber 30. COPYRIGHT: (C)2003,JPO
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公开(公告)号:JPH10144970A
公开(公告)日:1998-05-29
申请号:JP31424996
申请日:1996-11-11
Applicant: NAT AEROSPACE LAB
Inventor: NODA YASUTOSHI , KOU ENSEI , MORIYA SHINICHI , SUDO TAKAYUKI , MORO AKIO
Abstract: PROBLEM TO BE SOLVED: To avoid the breakdown of each part and improve thermoelectric conversion property and reliability by constituting the heat conductive part of a thermoelectric conversion module out of a metallic plate or a metallic layer coated with a ceramic layer. SOLUTION: Heat conducting parts 26H and 26L are constituted of a metallic plate 28 or a metallic layer coated with a ceramic layer 27, so as to materialize electric insulation or good heat conduction between metallic segments 15A and 15B of a thermoelectric covering element 10 and heat conductive parts 26H and 26L. For example, after boring a through screw hole or the like in the required place of the metallic plate 28, the whole surface is flame-coated with Al2 O3 which is high in heat conductivity into a thickness in the range 10μm-50μm to coat it with a ceramic layer 27. Then, the heat conducting part 26H on high temperature side and the heat conducting part 26L on the cooling side made that way are fixed by fixing screws 18 such as insulating ceramic, teflon, or the like, so as to set up a thermoelectric conversion module.
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公开(公告)号:FR2826117A1
公开(公告)日:2002-12-20
申请号:FR0207254
申请日:2002-06-13
Applicant: NAT AEROSPACE LAB
Inventor: YOSHIDA MAKOTO , OIKE MAMORU , NOSAKA MASATAKA , KIKUCHI MASATAKA , SUDO TAKAYUKI , WATANABE YOSHIAKI
Abstract: The system has double-cylinder type cartridge whose inner cylindrical portion is made to internally contact the bearing balls and an outer cylindrical portion is connected to the inner cylindrical portion through a ring-type support. The strain gauges for measuring bearing load are arranged on the surface of the outer cylindrical portion.
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公开(公告)号:FR2826117B1
公开(公告)日:2004-05-28
申请号:FR0207254
申请日:2002-06-13
Applicant: NAT AEROSPACE LAB
Inventor: YOSHIDA MAKOTO , OIKE MAMORU , NOSAKA MASATAKA , KIKUCHI MASATAKA , SUDO TAKAYUKI , WATANABE YOSHIAKI
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