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1. 发明专利

JP2005282361A Power producing device 审中-公开
标题翻译：电力生产设备
公开(公告)号：JP2005282361A
公开(公告)日：2005-10-13
申请号：JP2002383071
申请日：2002-12-06
申请人： Mei Sogo Kenkyusho Kk , 明総合研究所有限会社
发明人： SHIMIZU HIROSHI , SHIMIZU MIDORI , SHIMIZU AKIHIKO
IPC分类号： B63H21/06 , B63B35/00 , B63H21/10 , F01K25/10 , F03G7/05
CPC分类号： Y02E10/34
摘要： PROBLEM TO BE SOLVED: To provide a power producing device for taking out a power from a heat source with room temperature such as the sun.
SOLUTION: This power producing device comprises the systems of a heat engine in which a peripheral fluid with room temperature is used as the heat source, the heat of fusion of ice is used as a cooling source, and refrigerants (ammonia, propane, CFC 21) are used as working fluids. A thermal efficiency is increased by the cogeneration of cooling and the use of solar heat, namely, by adding a double effective system of a cold heat source in which approx. 50% of a latent heat in temperatures between 0°C after the melting of the ice to the temperature of the heat source is used again for power generation. The power producing device is mounted on the marine engine of a hull apparatus. Ice consumed in the power producing device is taken from a sea water in arctic region into an ice container and transported to consuming sites by a tow ship. The ice container can easily transport the ice at low cost.
COPYRIGHT: (C)2006,JPO&NCIPI
摘要翻译：要解决的问题：提供一种用于从例如太阳等室温的热源取出电力的发电装置。解决方案：该发电装置包括使用具有室温的外围流体作为热源的热机的系统，将冰的熔化热用作冷却源，制冷剂（氨，丙烷，CFC 21）用作工作流体。通过冷却热电联产和太阳能热的利用来增加热效率，即通过增加一个双重有效的冷热源系统，在冰融化后的0℃之间的温度与热源的温度之间的50％的潜热被再次用于发电。动力产生装置安装在船体装置的船用发动机上。在发电装置中消耗的冰从北极地区的海水中取出，放入冰箱中，用拖船运送到消费地点。冰箱容易以低成本运输冰块。版权所有（C）2006，JPO＆NCIPI

2. 发明专利

JP2002242693A POWER GENERATING DEVICE 失效
公开(公告)号：JP2002242693A
公开(公告)日：2002-08-28
申请号：JP2001079409
申请日：2001-02-14
申请人： MEI SOGO KENKYUSHO KK
发明人： SHIMIZU HIROSHI , SHIMIZU AKIHIKO , SHIMIZU MIDORI
IPC分类号： F02C1/05 , F02C1/10
摘要： PROBLEM TO BE SOLVED: To provide a power generating device for taking out power from a heat source at a normal temperature by a solar heat. SOLUTION: This power generating device comprises the heat source 1; gas/liquid separator 3 for separating a condensed liquid produced in an outlet of a turbine 2; a pump 4 for pressurizing liquid phase; a compressor 5 for pressurizing a gas phase; a gas/liquid mixer 6 for mixing the gas phase with the liquid phase; a rotary shaft 8 for transmitting a turbine power to the compressor; and a generator 7 for taking out a turbine power.

3. 发明专利

JP2005247675A Erosion resistant coating film 审中-公开
标题翻译：耐腐蚀涂层膜
公开(公告)号：JP2005247675A
公开(公告)日：2005-09-15
申请号：JP2004093740
申请日：2004-03-01
申请人： Mei Sogo Kenkyusho Kk , 明総合研究所有限会社
发明人： SHIMIZU HIROSHI
IPC分类号： F02K9/14 , C04B41/87 , F02K9/34
摘要： PROBLEM TO BE SOLVED: To provide a method of solving a problem that a structural material in a solid fuel rocket nozzle is deeply eroded by the local erosion.
SOLUTION: 1. A carbon-carbon fiber composite material (C/C ) or the like treated to form graphite (carbyne) to prevent the production of the thermally decomposable gas at an operation temperature is used as the structural material. 2. This erosion resistant coating film is formed by sticking or vapor-depositing vitreous carbon or CVD carbon on the surface. 3. The thickness of the provided coating film is determined corresponding to the failure probability of 1/10
6 on reliability and for an example, the maximum thickness of a nozzle throat is B≥5.66 mm in the vitreous carbon film and B≥3.83 mm in the CVD carbon film under a combustion condition of about 100 Bar pressure, about 3,000°C temperature and about 100 sec combustion time. 4. An ultrasonic (about 20 KHz) excitation erosion test or a liquid jet stream collision erosion test at a normal temperature is carried out and the temperature characteristics of the erosion is estimated from the temperature characteristics of tensile strength data.
COPYRIGHT: (C)2005,JPO&NCIPI
摘要翻译：要解决的问题：提供一种解决固体燃料火箭喷嘴中的结构材料被局部侵蚀深深侵蚀的问题的方法。作为结构材料，使用碳 - 碳纤维复合材料（C / C）等被处理以形成石墨（carbyne）以防止在可操作温度下产生可热分解气体。该抗腐蚀涂膜通过在表面上粘附或气相沉积玻璃碳或CVD碳而形成。所提供的涂膜的厚度根据可靠性的1/10 6 的故障概率来确定，例如，玻璃体中喷嘴喉部的最大厚度为B≥5.66mm 碳膜，并且在约100巴压力，约3,000℃温度和约100秒燃烧时间的燃烧条件下，CVD碳膜中B≥3.83mm。 4.在正常温度下进行超声波（约20KHz）的激发侵蚀试验或液体射流碰撞冲蚀试验，根据拉伸强度数据的温度特性估算侵蚀的温度特性。版权所有（C）2005，JPO＆NCIPI

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