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公开(公告)号：JPH074314A
公开(公告)日：1995-01-10
申请号：JP14917993
申请日：1993-06-21
Applicant: NAT AEROSPACE LAB , MITSUBISHI HEAVY IND LTD
Inventor： SHINNO MASAYUKI , TOKUNAGA KEN , TOGAWA MORIHITO
Abstract: PURPOSE:To add the rocket propulsion function to a scram jet engine which is provided with a flow passage putting a front opening part, a center cavity part, and a rear opening part in a row, and provided with a hydrogen jetting device in the center cavity part, so as to be usable even at take-off or outer space flight. CONSTITUTION:A part of a member constituting the circumference of a flow passage putting a front opening part A, a center cavity part B, a rear opening part, and the like in a row, is constructed to be movable so as to close the front opening part, and an oxygen jetting device is additionally provided in the center cavity part B.
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公开(公告)号：JPH0579629B2
公开(公告)日：1993-11-04
申请号：JP18737086
申请日：1986-08-08
Applicant: NAT AEROSPACE LAB , KOGYO GIJUTSUIN , DAIKIN IND LTD
Inventor： SHINNO MASAYUKI , YATSUYANAGI NOBUYUKI , IKEUCHI JUN , SATA NOBUHIRO , HIRANO TOORU , SUMYOSHI KANICHIRO
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公开(公告)号：JPH0510854A
公开(公告)日：1993-01-19
申请号：JP16437991
申请日：1991-07-04
Applicant: NAT AEROSPACE LAB , MITSUBISHI HEAVY IND LTD
Inventor： KUMAGAI TATSUO , SAKURANAKA NOBORU , UEDA SHUICHI , SAITO TOSHIHITO , KUSAKA KAZUO , WAKAMATSU YOSHIO , SHINNO MASAYUKI , ADACHI NAOTO , NAGATA SATOSHI , SAKAMOTO AKIRA
Abstract: PURPOSE:To enable a large heat-resistance material and a sample such as a cooling structure to be heated for achieving an evaluation test by allowing a high-temperature high-speed gas to be discharged by receiving supply of a fuel and an oxidizer and this gas flow to be directed toward the sample. CONSTITUTION:A high-temperature high-speed gas is generated by allowing a fuel f to be combusted in a combustion equipment 10 and a gas flow is accelerated in a nozzle 11, thus forming a field of a high-temperature high-speed gas flow h. Then, a heat-resistance material, a sample 12 in cooling structure, etc., are installed within the field of this flow h and is heated, thus enabling them to be evaluated. Since this structure is based on a rocket-engine structure. a flow rate of a high-temperature gas can be set to a high level. thus enabling a test device to be large, especially an exit diameter of the nozzle 11 to be large. This increase in size allows a field of a large gas flow h to be formed, thus enabling the large heat-resistance material and the sample such as a cooling structure to be heated and evaluation test to be performed.
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公开(公告)号：JPH03146603A
公开(公告)日：1991-06-21
申请号：JP28426989
申请日：1989-10-31
Applicant: WATANABE RYUZO , KAWASAKI AKIRA , NAT AEROSPACE LAB , ISHIKAWAJIMA HARIMA HEAVY IND
Inventor： WATANABE RYUZO , KAWASAKI AKIRA , SHINNO MASAYUKI , YUKI MASAHIRO , MURAYAMA TOSHIICHI , IRISAWA TOSHIO
Abstract: PURPOSE:To manufacture a gradated functional material having different property at the front and the back by heating the surface of a powder green compact with laser beam after heating it near to starting temp. of sintering, cooling the back face and sintering while giving temp. gradation. CONSTITUTION:For example, the powder green compact W composed of ceramic on the front face and metal on the back face, is set on a cooling device 25 in a sintering furnace 13 and the inner part of the furnace is made to an inert gas atmosphere with a vacuum suction device 18 and gas introducing hole 19. Successively, after uniformly heating in the sintering furnace 13 near to the starting temp. of sintering to the powder green compact W with an electric heating device 11, the powder green compact W is irradiated with the laser beam in a laser beam heating device 22 through a laser beam irradiating aperture 21 to heat the surface thereof. Simultaneously, cooling gas is supplied from a cooling device 25 to cool the back face of powder green compact W, and the sintering is executed under the condition of existence of the temp. inclination between the front and the back. By this method, as coming from the front face to the back face, the gradated functional material continuously varying the property at atomic and molecular level, is obtd.
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公开(公告)号：JPS62156938A
公开(公告)日：1987-07-11
申请号：JP29704285
申请日：1985-12-28
Applicant: NAT AEROSPACE LAB , HIRAI TOSHIO , WATANABE RYUZO , DAIKIN IND LTD , SUMITOMO ELECTRIC INDUSTRIES
Inventor： SHINNO MASAYUKI , SUZUKI AKIO , HIRAI TOSHIO , WATANABE RYUZO , HIRANO TORU , KUROISHI ATSUSHI
IPC: B32B18/00 , B22F3/11 , B22F7/02 , B32B7/04 , B32B15/04 , C23C4/02 , C23C4/06 , C23C14/02 , C23C14/06 , C23C14/22 , C23C16/02 , C23C16/30 , C23C16/44
Abstract: The present invention relates to a method of producing a functionally gradient material whose components and structure are continuously adjusted by the coating, plating and powder metallurgy techniques to change its function in turn and provides a method of producing a functionally gradient material superior in heat-resistance, corrosion-reistance and resistance to thermal fatigue by distributing a third component having a lower Young's modulus or formed of high-strength material sufficiently durable to the fracture strength among ceramics as a first component and metals or other ceramics as a second component to change the function.
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Patent Agency Ranking
公开(公告)号：JP2001108643A
公开(公告)日：2001-04-20
申请号：JP28565199
申请日：1999-10-06
Applicant: NAT AEROSPACE LAB
Inventor： MORIYA SHINICHI , TADANO MAKOTO , SATO MASAHIRO , KUMAGAI TATSUO , WILLIAM KUMETEIKU , KUSAKA KAZUO , SHINNO MASAYUKI
IPC: G01N25/72
Abstract: PROBLEM TO BE SOLVED: To provide an inspection system by which a face to be inspected can be inspected in a short time, with good efficiency and in a noncontact manner toy a continuous scanning operation without damaging and contaminating an object to be inspected and which can be applied even when the coating layer of the object to be inspected is thin. SOLUTION: A means by which the surface of an object to be inspected is irradiated with a laser beam is provided. A means wherein infrared rays radiated by a spot which is irradiated with the laser beam and which is heated are received so as to be input to an infrared radiation thermometer is provided. A scanning means wherein a sensor member on which the irradiation part of the laser beam and an infrared receiving part are arranged is scanned with reference to the surface of the object to be inspected is provided. A means by which the detected value of the infrared radiation thermometer is compared with standard data and by which the state of the coating layer of the object to be inspected is analyzed is provided.
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公开(公告)号：JPH1022532A
公开(公告)日：1998-01-23
申请号：JP18675296
申请日：1996-06-27
Applicant: NAT AEROSPACE LAB
Inventor： TANJI YASUNORI , KUMAGAI TATSUO , MORIYA SHINICHI , OSHIMA TAMIO , SHINNO MASAYUKI , TADA YASUO
Abstract: PROBLEM TO BE SOLVED: To prevent deterioration of thermoelectric conversion characteristics caused by sublimation and oxidation, etc., of an element in PbTe, for example and attain stable thermoelectric conversion for a long period by crowning at least a high temperature side end part of a thermo-element with a conductive block having a recessed part in which the end part is force-fitted. SOLUTION: Since edge parts 1H and 1L of a thermo-element 1 are crowned with a conductive block 3, the end part can be electrically and thermally combined to other parts by the conductive block 3. The thermo-element 1 and the conductive block 3 are combined by force-fitting a thermo-element end part to the recessed part 1 of the conductive block 3. Since there is a possibility of generation of a gap between a thermo-element and a conductive block microscopically, generation of heat shearing stress can be avoided even if the high temperature side end part 1H is subjected to high temperature heating. Furthermore, it is possible to avoid generation of sublimation and oxidation of a constituent element of the thermo-element 1 and prevent variation of an element and deterioration of characteristics.
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公开(公告)号：JPH0712708A
公开(公告)日：1995-01-17
申请号：JP15230193
申请日：1993-06-23
Applicant: NAT AEROSPACE LAB , MITSUBISHI HEAVY IND LTD
Inventor： SAKURANAKA NOBORU , WAKAMATSU YOSHIO , SHINNO MASAYUKI , ADACHI NAOTO
Abstract: PURPOSE:To evaluate a heat-resistant material and a cooling structure test specimen in severer aerodynamic heating environment by generating a hotter high-speed gas flow. CONSTITUTION:In a hot gas flow evaluation test device in which a fuel 2 is burned with oxidizing agent 3 in a combustor 1 to generate hot gas, the gas is led to a nozzle as it is and accelerated to a supersonic speed, and a test specimen 6 is set in a high temperature and high speed gas flow 5 to make various types of evaluations, an arc heating device 11 is set in the downstream side from the combustor 1, and a hot gas generated by combustion of the fuel 2 and oxidizing agent 3 in the combustor 1 is further heated.
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公开(公告)号：JPH06205549A
公开(公告)日：1994-07-22
申请号：JP35855092
申请日：1992-12-28
Applicant: NAT AEROSPACE LAB
Inventor： SHINNO MASAYUKI
Abstract: PURPOSE:To make it possible to utilize energy from a moon power station on the ground, by converting the generated energy from the moon power station into an ultraviolet laser and converting the ultraviolet laser into an infrared laser at a space base and converting the infrared laser into a power at a ground base. CONSTITUTION:A solar light power station or a nuclear power station 3 is installed on the surface of the moon 2. A satellite 4 as a relay base can be relayed to a receiving base 5 on the ground. An ultraviolet laser 6 is used between the moon 2 and the satellite 4, and an infrared laser 7 is used between the satellite 4 and the ground base 5. That is, the ultraviolet laser 6 is converted into the infrared laser 7 by the satellite 4, and the infrared laser 7 is transmitted to the ground base 5. In the ground base 5, the infrared laser 7 is converted into a power by a photoelectric converter made of P/1/N, and the power is transmitted to necessary places. Thus, an energy from the solar light power station or the nuclear power station 3 installed on the surface of the moon 2 can be utilized on the ground.
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公开(公告)号：JPH03146607A
公开(公告)日：1991-06-21
申请号：JP28426889
申请日：1989-10-31
Applicant: WATANABE RYUZO , KAWASAKI AKIRA , NAT AEROSPACE LAB , ISHIKAWAJIMA HARIMA HEAVY IND
Inventor： WATANABE RYUZO , KAWASAKI AKIRA , SHINNO MASAYUKI , YUKI MASAHIRO , MURAYAMA TOSHIICHI , IRISAWA TOSHIO
Abstract: PURPOSE:To enable joining with the wall-known welding method by varying composition to joining end direction in a material and allowing the most outer end part to be a weldable composition. CONSTITUTION:Raw material powder 31 of ceramic 12, raw material powder 32 of metal 13 and binder 33 are prepared and composition ratio is adjusted with each composition ratio control valve 34, and they are mixed with a mixing nozzle 35 and injected and filled up into a metallic mold 36. Then, the metallic mold 36 is shifted to X-Y direction and they are filled up so that the front face 11a is the ceramic 12 and the back face 11b and the joining end part 11c are the metal 13 and the composition toward the end part 11c from the center part continuously varies in binary condition, and pressurized and formed to the prescribed shape to make the gradated functional material 11. Successively, the material 11 is heated under the condition of giving the temp. gradation corresponding to the gradation of composition in the raw material powder by using a device combining a sintering furnace and laser beam heating device for uniform heating and held to the sintering temp. for each composition. By this method, the metal 13 having 100% at the joining end part 11c is obtd. and the metal- made structural materials can be joined respectively.
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