| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 压缩机 | CN200410032970.6 | 2004-04-14 | CN100353059C | 2007-12-05 | 佐伯晓生; 神德哲行; 下俊久; 马场敬明; 村濑仁俊; 杉冈隆弘 |
| 一种压缩机包括斜盘和连接到斜盘的外部周边上的滑履。斜盘的表面在滑履的表面上滑动。滑动膜应用到斜盘的表面。滑动膜由包含固体润滑剂和氧化钛粉末的粘合剂树脂形成。这允许斜盘的表面和滑履的平的表面相互平滑地滑动。 | ||||||
| 2 | 压缩机 | CN200410032970.6 | 2004-04-14 | CN1538062A | 2004-10-20 | 佐伯晓生; 神德哲行; 下俊久; 马场敬明; 村濑仁俊 |
| 一种压缩机包括斜盘和连接到斜盘的外部周边上的滑履。斜盘的表面在滑履的表面上滑动。滑动膜应用到斜盘的表面。滑动膜由包含固体润滑剂和氧化钛粉末的粘合剂树脂形成。这允许斜盘的表面和滑履的平的表面相互平滑地滑动。 | ||||||
| 3 | Compressor | US10823376 | 2004-04-13 | US20050135954A1 | 2005-06-23 | Akio Saiki; Noriyuki Shintoku; Toshihisa Shimo; Noriaki Baba; Hitotoshi Murase |
| A compressor includes a swash plate, and a shoe connected to an outer periphery of the swash plate. A surface of the swash plate slides upon a flat surface of the shoe. A sliding film is applied to the surface of the swash plate. The sliding film is formed of binder resin which contains a solid lubricant and titanium oxide powder. This allows the surface of the swash plate and the flat surface of the shoe to smoothly slide upon each other. | ||||||
| 4 | Gas turbine blade | US10670807 | 2003-09-25 | US20040057832A1 | 2004-03-25 | Robert Fleck; Thomas Jansing; Eckart Schumann |
| Disclosed is a gas turbine blade (1) having a ceramic heat-insulating layer (17). The ceramic heat-insulating layer (17) consists of 10-95% wt. % magnesium aluminate, 5-90 wt. % magnesium oxide and 0-20 wt. % aluminum oxide. Magnesium oxide particles are incorporated into a matrix made of spindle-shaped magnesium aluminate, enabling the thermal expansion coefficient of the ceramic heat-insulating layer (17) to be adapted in a particularly suitable manner to a metallic base body (15) of the gas turbine blade (1). The ceramic heat-insulating layer (17) also has a porosity which is greater that 3 vol. %, thereby guaranteeing sufficiently low heat conductivity. | ||||||
| 5 | Compressor | US10823376 | 2004-04-13 | US07377754B2 | 2008-05-27 | Akio Saiki; Noriyuki Shintoku; Toshihisa Shimo; Noriaki Baba; Hitotoshi Murase; Takahiro Sugioka |
| A compressor includes a swash plate, and a shoe connected to an outer periphery of the swash plate. A surface of the swash plate slides upon a flat surface of the shoe. A sliding film is applied to the surface of the swash plate. The sliding film is formed of binder resin which contains a solid lubricant and titanium oxide powder. This allows the surface of the swash plate and the flat surface of the shoe to smoothly slide upon each other. | ||||||
| 6 | Gas turbine blade | US10670807 | 2003-09-25 | US06887044B2 | 2005-05-03 | Robert Fleck; Thomas Jansing; Eckart Schumann |
| Disclosed is a gas turbine blade (1) having a ceramic heat-insulating layer (17). The ceramic heat-insulating layer (17) consists of 10-95% wt. % magnesium aluminate, 5-90 wt. % magnesium oxide and 0-20 wt. % aluminum oxide. Magnesium oxide particles are incorporated into a matrix made of spindle-shaped magnesium aluminate, enabling the thermal expansion coefficient of the ceramic heat-insulating layer (17) to be adapted in a particularly suitable manner to a metallic base body (15) of the gas turbine blade (1). The ceramic heat-insulating layer (17) also has a porosity which is greater that 3 vol. %, thereby guaranteeing sufficiently low heat conductivity. | ||||||
| 7 | Compressor | JP2003109598 | 2003-04-14 | JP4025832B2 | 2007-12-26 | 俊久 下; 暁生 佐伯; 隆弘 杉岡; 仁俊 村瀬; 哲行 神徳; 敬明 馬場 |
| 8 | Compressor | JP2003109598 | 2003-04-14 | JP2004316499A | 2004-11-11 | SAEKI AKIO; KAMITOKU TETSUYUKI; SHIMO TOSHIHISA; BABA TAKAAKI; MURASE KIMITOSHI |
| <P>PROBLEM TO BE SOLVED: To provide a compressor with improved sliding property and with high reliability. <P>SOLUTION: In the compressor, surfaces 8c, 8d of a swash plate 8 is relatively slid with flat faces 9c, 9d of shoes 9a, 9b. Slide films C31 are formed on the surfaces 8c, 8d of the swash plate 8. Each slide film C 31 is made of binder resin containing solid lubricant and titanium oxide powder. <P>COPYRIGHT: (C)2005,JPO&NCIPI | ||||||
| 9 | Gas turbine blade | JP2002579618 | 2002-03-28 | JP2004526094A | 2004-08-26 | シューマン、エカルト; フレック、ロベルト; ヤンジング、トーマス |
| セラミックス断熱層（１７）を備えたガスタービン翼（１）に関する。 この断熱層は、１０〜９５重量％アルミン酸塩マグネシウムと、５〜９０重量％酸化マグネシウムと、０〜２０重量％酸化アルミニウムとから成り、スピネル型構造の前記アルミン酸塩マグネシウムからなる母材の中に、酸化マグネシウムからなる粒子（２３）が埋設されている。 これによって、セラミックス断熱層（１７）の熱膨張係数を、ガスタービン翼（１）の金属製本体（５）に特に良好に適合させられる。 同時に、セラミックス断熱層（１７）は３容積％より大きな多孔率を有している。 これによって、十分に小さな熱伝導率が保証される。 | ||||||
| 10 | Compressor coating | EP04008761.1 | 2004-04-13 | EP1469199A2 | 2004-10-20 | Saiki, Akio; Shintoku, Noriyuki; Shimo, Toshihisa; Baba, Noriaki; Murase, Hitotoshi |
A compressor includes a swash plate, and a shoe connected to an outer periphery of the swash plate. A surface of the swash plate slides upon a flat surface of the shoe. A sliding film is applied to the surface of the swash plate. |
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| 11 | GASTURBINENSCHAUFEL | EP02727505.6 | 2002-03-28 | EP1373685A1 | 2004-01-02 | JANSING, Thomas; FLECK, Robert; SCHUMANN, Eckart |
| Disclosed is a gas turbine blade (1) having a ceramic heat-insulating layer (17). The ceramic heat-insulating layer (17) consists of 10 - 95 wt. % magnesium aluminate, 5 -90 wt. % magnesium oxide and 0 -20 wt. % aluminium oxide. Magnesium oxide particles are incorporated into a matrix made of spindle-shaped magnesium aluminate, enabling the thermal expansion coefficient of the ceramic heat-insulating layer (17) to be adapted in a particularly suitable manner to a metallic base body (15) of the gas turbine blade (1). The ceramic heat-insulating layer (17) also has a porosity which is greater than 3 vol. %, thereby guaranteeing sufficiently low heat conductivity. | ||||||
| 12 | Compressor coating | EP04008761.1 | 2004-04-13 | EP1469199B1 | 2014-07-02 | Saiki, Akio; Shintoku, Noriyuki; Shimo, Toshihisa; Baba, Noriaki; Murase, Hitotoshi; Takahiro, Sugioka |
| 13 | Gasturbinenschaufel mit einer keramischen Wärmedämmschicht | EP04011322.7 | 2002-03-28 | EP1445425A3 | 2004-08-25 | Fleck, Robert; Jansing, Thomas; Schumann, Eckart Dr. |
Es wird eine Gasturbinenschaufel (1) mit einer keramischen Wärmedämmschicht (17) vorgestellt, wobei die keramische Wärmedämmschicht (17) aus 10 bis 95 Gew.-% Magnesiumaluminat, 5 bis 90 Gew.-% Magnesiumoxid und 0 bis 20 Gew.-% Aluminiumoxid besteht, wobei Körner aus Magnesiumoxid in eine Matrix aus spinellförmigem Magnesiumaluminat eingebettet sind, wodurch eine besonders gute Anpassung des Wärmeausdehnungskoeffizienten der keramischen Wärmedämmschicht (17) an einen metallischen Grundkörper (15) der Gasturbinenschaufel (1) erreicht wird. Gleichzeitig weist die keramische Wärmedämmschicht (17) eine Porosität größer als 3 Vol.-% auf. Hierdurch wird eine ausreichend niedrige Wärmeleitfähigkeit sichergestellt. |
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| 14 | Compressor coating | EP04008761.1 | 2004-04-13 | EP1469199A3 | 2006-05-10 | Saiki, Akio; Shintoku, Noriyuki; Shimo, Toshihisa; Baba, Noriaki; Murase, Hitotoshi |
A compressor includes a swash plate, and a shoe connected to an outer periphery of the swash plate. A surface of the swash plate slides upon a flat surface of the shoe. A sliding film is applied to the surface of the swash plate. |
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| 15 | GASTURBINENSCHAUFEL | EP02727505.6 | 2002-03-28 | EP1373685B1 | 2005-10-19 | JANSING, Thomas; FLECK, Robert; SCHUMANN, Eckart |
| Disclosed is a gas turbine blade (1) having a ceramic heat-insulating layer (17). The ceramic heat-insulating layer (17) consists of 10 - 95 wt. % magnesium aluminate, 5 -90 wt. % magnesium oxide and 0 -20 wt. % aluminium oxide. Magnesium oxide particles are incorporated into a matrix made of spindle-shaped magnesium aluminate, enabling the thermal expansion coefficient of the ceramic heat-insulating layer (17) to be adapted in a particularly suitable manner to a metallic base body (15) of the gas turbine blade (1). The ceramic heat-insulating layer (17) also has a porosity which is greater than 3 vol. %, thereby guaranteeing sufficiently low heat conductivity. | ||||||
| 16 | Gasturbinenschaufel mit einer keramischen Wärmedämmschicht | EP04011322.7 | 2002-03-28 | EP1445425A2 | 2004-08-11 | Fleck, Robert; Jansing, Thomas; Schumann, Eckart Dr. |
Es wird eine Gasturbinenschaufel (1) mit einer keramischen Wärmedämmschicht (17) vorgestellt, wobei die keramische Wärmedämmschicht (17) aus 10 bis 95 Gew.-% Magnesiumaluminat, 5 bis 90 Gew.-% Magnesiumoxid und 0 bis 20 Gew.-% Aluminiumoxid besteht, wobei Körner aus Magnesiumoxid in eine Matrix aus spinellförmigem Magnesiumaluminat eingebettet sind, wodurch eine besonders gute Anpassung des Wärmeausdehnungskoeffizienten der keramischen Wärmedämmschicht (17) an einen metallischen Grundkörper (15) der Gasturbinenschaufel (1) erreicht wird. Gleichzeitig weist die keramische Wärmedämmschicht (17) eine Porosität größer als 3 Vol.-% auf. Hierdurch wird eine ausreichend niedrige Wärmeleitfähigkeit sichergestellt. |
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| 17 | Gasturbinenschaufel | EP01108371.4 | 2001-04-03 | EP1247941A1 | 2002-10-09 | Fleck, Robert; Jansing, Thomas; Schumann, Eckart, Dr. |
Es wird eine Gasturbinenschaufel (1) mit einer keramischen Wärmedämmschicht (17) beschrieben. Die keramische Wärmedämmschicht (17) besteht aus 10 bis 95Gew.-% Magnesiumaluminat, 5 bis 90Gew.-% Magnesiumoxid und 0 bis 20Gew.-% Aluminiumoxid, wobei Körner aus Magnesiumoxid in eine Matrix aus spinellförmigem Magnesiumaluminat eingebettet sind, wodurch eine besonders gute Anpassung des Wärmeausdehnungskoeffizienten der keramischen Wärmedämmschicht (17) an einen metallischen Grundkörper (15) der Gasturbinebschaufel (1) erreicht wird. Gleichzeitig weist die keramische Wärmedämmschicht (17) eine Porosität größer als 3Vol.-% auf. Hierdurch wird eine ausreichend niedrige Wärmeleitfähigkeit sichergestellt. |
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| 18 | 압축기 | KR1020040023093 | 2004-04-02 | KR100576281B1 | 2006-05-04 | 사이끼아끼오; 신또꾸노리유끼; 시모도시히사; 바바노리아끼; 무라세히또또시 |
| 보다 슬라이딩성이 향상되고 높은 신뢰성을 얻는 것이 가능한 압축기를 제공한다. 사판 (8) 의 표면 (8c,8d) 과 슈 (9a,9b) 의 평탄면 (9c,9d) 이 상대 슬라이딩하는 압축기에 있어서, 사판 (8) 의 표면 (8c,8d) 에 슬라이딩막 (C31) 이 형성되어 있다. 이 슬라이딩막 (C31) 은 고체 윤활제 및 산화티탄 분말을 함유하는 바인더 수지로 이루어진다. | ||||||
| 19 | 압축기 | KR1020040023093 | 2004-04-02 | KR1020040089489A | 2004-10-21 | 사이끼아끼오; 신또꾸노리유끼; 시모도시히사; 바바노리아끼; 무라세히또또시 |
| PURPOSE: A compressor is provided to improve sliding performance and reliability by forming a sliding film on one of first and second sliding surfaces sliding relatively to each other. CONSTITUTION: A compressor has a first sliding surface of a first member and a second sliding surface of a second member which slide relatively to each other. A sliding film(C31) made from binder resin containing at least a solid lubricant and an inorganic particle is formed in at least one of the first and second sliding surfaces. The sliding film contains a coupling agent. The binder resin is polyamide-imide. The inorganic particle is titanium dioxide. The primary average diameter of the titanium dioxide particle is below 1 micrometer. The sliding film consists of the titanium dioxide particle of 5¯35 wt% for the binder resin. | ||||||
