| 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 | 把热转换成功的方法和装置 | CN98122377.X | 1998-12-02 | CN1104553C | 2003-04-02 | F·杜尔斯特; M·维克拉斯 |
| 本发明涉及一种把热转化成功的方法，气体燃料被压缩并随后被燃烧，燃烧导致的体积膨胀使驱动装置2运动。为了低污染地燃烧，按本发明规定：压缩的气体燃料在充满燃烧室的多孔体8中燃烧。 | ||||||
| 2 | 把热转换成功的方法和装置 | CN98122377.X | 1998-12-02 | CN1232135A | 1999-10-20 | F·杜尔斯特; M·维克拉斯 |
| 本发明涉及一种把热转化成功的方法,气体燃料被压缩并随后被燃烧,燃烧导致的体积膨胀使驱动装置2运动。为了低污染地燃烧,按本发明规定:压缩的气体燃料在多孔体8中燃烧。 | ||||||
| 3 | 回转式压缩机 | CN201310519886.6 | 2009-01-23 | CN103527484A | 2014-01-22 | 前山英明; 石井稔; 伏木毅; 加藤太郎; 石园文彦 |
| 本发明提供一种能够在各滑动部抑制制冷剂的化学反应所导致的分解或聚合的回转式压缩机，上述制冷剂是结构中含碳双键的卤化烃、结构中含碳双键的碳氢化合物、包括结构中含碳双键的卤化烃或结构中含碳双键的碳氢化合物中的至少任意一种的混合物。本发明的回转式压缩机（200）压缩结构中含碳双键的卤化烃、结构中含碳双键的碳氢化合物、包括结构中含碳双键的卤化烃或结构中含碳双键的碳氢化合物中的至少任意一种的混合物中的任意一种制冷剂，其特征在于，设置于对制冷剂进行压缩的压缩元件（101）上并构成滑动部的部件的至少一方，至少其滑动表面由非金属构成。上述压缩元件使用EO比例为50%以下的PAG作为润滑上述滑动部的冷冻机油。 | ||||||
| 4 | 回转式压缩机 | CN200910009702.5 | 2009-01-23 | CN101608620A | 2009-12-23 | 前山英明; 石井稔; 伏木毅; 加藤太郎; 石园文彦 |
| 本发明提供一种能够在各滑动部抑制制冷剂的化学反应所导致的分解或聚合的回转式压缩机，上述制冷剂是结构中含碳双键的卤化烃、结构中含碳双键的碳氢化合物、包括结构中含碳双键的卤化烃或结构中含碳双键的碳氢化合物中的至少任意一种的混合物。本发明的回转式压缩机(200)压缩结构中含碳双键的卤化烃、结构中含碳双键的碳氢化合物、包括结构中含碳双键的卤化烃或结构中含碳双键的碳氢化合物中的至少任意一种的混合物中的任意一种制冷剂，其特征在于，设置于对制冷剂进行压缩的压缩元件(101)上并构成滑动部的部件的至少一方，至少其滑动表面由非金属构成。 | ||||||
| 5 | FAN CASING FOR A JET ENGINE | US12639181 | 2009-12-16 | US20100150696A1 | 2010-06-17 | Olaf Lenk |
| A fan casing (2) for a jet engine has a burst protection arrangement (7) made up of layers at least in an area of fan blades (5). To contain detached fan blades (5) within a fan casing (2) of a jet engine by use of a low-weight and easily manufacturable burst protection arrangement (7), the fan casing (2) is made of a fiber-composite material which itself forms at least one layer provided with at least one inorganic, non-metallic protective layer (8). | ||||||
| 6 | Heat resistant super alloy and its use | US10995993 | 2004-11-22 | US20050238526A1 | 2005-10-27 | Gerald Schall |
| A heat resistant super alloy suffices the following conditions: carbon0.01-0.2percent in weight chromium8-10percent in weight aluminum4-6percent in weight titanium2-4percent in weight molybdenum1.5-2.8percent in weight tungsten10-13.5percent in weight niobium1.5-2.5percent in weight boron0 < B ≦ 0.04percent in weight zircon0 < Zr ≦ 0.15percent in weight the contents of hafnium and lanthanum together amounts to 0 < Hf + La ≦ 1.5 percent in weight, optionally traces of tantalum, the remainder being nickel. Such an alloy is preferably used for turbine wheels and particularly for turbochargers. | ||||||
| 7 | Reinforced rotor disk assembly | US577073 | 1995-12-22 | US5632600A | 1997-05-27 | Peter R. Hull |
| A reinforced rotor disk assembly includes a rotor disk having a rim, hub, and web therebetween. The web includes at least one annular extension spaced radially inwardly of the rim. A plurality of rotor blades extend outwardly from the rim. And, a reinforcing ring is disposed radially around the extension for restraining radial outward growth thereof to react centrifugal load in the disk. The reinforcing ring preferably includes a plurality of circumferentially extending structural fibers in a corresponding matrix for carrying hoop loads therein. | ||||||
| 8 | Abradable non-metallic seal for rotating turbine engines | US733559 | 1991-07-22 | US5304032A | 1994-04-19 | Alexander A. Bosna; Louis M. Riccio |
| A turbine engine having an interior housing and one or more annular abradable seals for the turbine blades. The abradable seal comprises a resin having fractured hollow inorganic non-metallic microspheres forming nooks, crannies and undercuts in the resin and a solid lubricant in the resin and in the nooks and crannies and undercuts formed by the fractured hollow non-metallic inorganic microspheres. | ||||||
| 9 | Fluid motion device | US3514237D | 1968-07-25 | US3514237A | 1970-05-26 | SPYRIDAKIS EMANUEL G |
| 10 | Armored vane | US62875767 | 1967-04-05 | US3398884A | 1968-08-27 | KAATZ HERBERT W; LEO TOBACMAN |
| 11 | Oilless pump | US10249349 | 1949-07-01 | US2616615A | 1952-11-04 | SCOTT WALTER A |
| 12 | Heat-resistant super alloys and their use | JP2004337379 | 2004-11-22 | JP4583894B2 | 2010-11-17 | ゲラルド・シャル |
| 13 | Compressor | JP2009029751 | 2009-02-12 | JP2010185357A | 2010-08-26 | TAKAHASHI SHINICHI |
| <P>PROBLEM TO BE SOLVED: To suppress occurrence of high temperature due to mutual direct contact of metal so that decomposition and polymerization of material having a double bond between carbon atoms are suppressed. <P>SOLUTION: A compressor 200 includes: a compression element 101 having a sliding member 3 and compressing coolant; and an electric element 102 driving the compression element 101, and uses, as the coolant, either a halogenated hydrocarbon having a double bond between carbon atoms in the composition; a hydrocarbon having a double bond between carbon atoms in the composition; or a mixture including at least either a halogenated hydrocarbon having a double bond between carbon atoms in the composition or a hydrocarbon having a double bond between carbon atoms in the composition. In the compressor 200, at least either a surface of a sliding contact part 3a of the sliding member 3 of the compression element 101, or a surface of a sliding contact part of a counter part member 1 with which the sliding member 3 slidingly contacts is made of a nonmetal material. <P>COPYRIGHT: (C)2010,JPO&INPIT | ||||||
| 14 | Pump | JP2874383 | 1983-02-21 | JPS59153995A | 1984-09-01 | SEKI MASAAKI; MATSUMOTO AKIO |
| PURPOSE: To provide the pumping characteristics with good durability and stabilization by coating the end faces of vanes with a resin having excellent abrasion resistance, heat resistance and slidability. CONSTITUTION: The end faces of vanes in the axial direction in sliding with bracket 1 and housing 6 are coated with resin to form layers 51, 52. These resin coating layers 51, 52 serve reduction of the friction coefficient between the vanes 5 and bracket 1 or housing 6 to ensure enhancement of the sliding characteristic, and further the use of a resin excellent in heat and abrasion resistances will prevent drop of the pumping characteristics as well as enhance the durability. COPYRIGHT: (C)1984,JPO&Japio | ||||||
| 15 | Heat resistant super alloy and its use | US12105024 | 2008-04-17 | US09051844B2 | 2015-06-09 | Gerald Schall |
| A heat resistant super alloy suffices the following conditions: carbon0.01-0.2percent in weight chromium8-10percent in weight aluminum4-6percent in weight titanium2-4percent in weight molybdenum1.5-2.8percent in weight tungsten10-13.5percent in weight niobium1.5-2.5percent in weight boron0 < B ≦ 0.04percent in weight zircon0 < Zr ≦ 0.15percent in weight the contents of hafnium and lanthanum together amounts to 0 < Hf + La ≦ 1.5 percent in weight, optionally traces of tantalum, the remainder being nickel. Such an alloy is preferably used for turbine wheels and particularly for turbochargers. | ||||||
| 16 | Inner diameter shroud assembly for variable inlet guide vane structure in a gas turbine engine | US13531679 | 2012-06-25 | US08951010B2 | 2015-02-10 | Daniel W. Major; John C. Ditomasso; Nathan F. Champion |
| An inner shroud assembly includes an aft core segment mountable to a forward core segment to support a multiple of vanes for rotational movement relative thereto. A shroud backing plate segment engageable with the aft core segment and at least one fastener which passes through the shroud backing plate, the aft core segment and the forward core segment. | ||||||
| 17 | ASSEMBLY FOR PREVENTING FLUID FLOW | US13012380 | 2011-01-24 | US20120189435A1 | 2012-07-26 | Victor John Morgan; Rebecca Evelyn Hefner; Stephen Gerard Pope |
| According to one aspect of the invention, an assembly for preventing fluid flow between turbine components includes a shim and a first woven wire mesh layer that includes a first surface coupled to a first side of the shim and a second surface of the woven wire mesh layer opposite the first surface. The assembly also includes a first outer layer coupled to the second surface of the woven wire mesh layer, where the first outer layer includes a high temperature non-metallic material. | ||||||
| 18 | INNER DIAMETER SHROUD ASSEMBLY FOR VARIABLE INLET GUIDE VANE STRUCTURE IN A GAS TURBINE ENGINE | US12478955 | 2009-06-05 | US20100310358A1 | 2010-12-09 | Daniel W. Major; John C. Ditomasso; Nathan F. Champion |
| An inner shroud assembly includes an aft core segment mountable to a forward core segment to support a multiple of vanes for rotational movement relative thereto. A shroud backing plate segment engageable with the aft core segment and at least one fastener which passes through the shroud backing plate, the aft core segment and the forward core segment. | ||||||
| 19 | HEAT RESISTANT SUPER ALLOY AND ITS USE | US12105024 | 2008-04-17 | US20080271822A1 | 2008-11-06 | Gerald Schall |
| A heat resistant super alloy suffices the following conditions: carbon0.01-0.2percent in weight chromium8-10percent in weight aluminum4-6percent in weight titanium2-4percent in weight molybdenum1.5-2.8percent in weight tungsten10-13.5percent in weight niobium1.5-2.5percent in weight boron0 < B ≦ 0.04percent in weight zircon0 < Zr ≦ 0.15percent in weight the contents of hafnium and lanthanum together amounts to 0 < Hf + La ≦ 1.5 percent in weight, optionally traces of tantalum, the remainder being nickel. Such an alloy is preferably used for turbine wheels and particularly for turbochargers. | ||||||
| 20 | Method and device for converting heat into work | US198835 | 1998-11-24 | US6125815A | 2000-10-03 | Franz Durst; Miroslaw Weclas |
| The invention relates to a method for converting heat into work, a gaseous fuel being compressed and subsequently burnt and a drive means 2 being moved due to volumetric expansion generated as a result of combustion. In order to allow low-pollutant combustion, there is provision, according to the invention, for the compressed gaseous fuel to be burnt in a porous body 8. | ||||||
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