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1. 发明授权

US6077038A Brush seal for turbo engines 失效
标题翻译：涡轮发动机刷密封
公开(公告)号：US6077038A
公开(公告)日：2000-06-20
申请号：US994348
申请日：1997-12-19
申请人： Alfons Gail , Uwe Michel , Edgar Pfister , Lothar Reisinger , Thomas Miller
发明人： Alfons Gail , Uwe Michel , Edgar Pfister , Lothar Reisinger , Thomas Miller
IPC分类号： F01D11/00 , F01D11/02 , F01D11/12 , F16J15/00 , F16J15/32 , F01D29/04
CPC分类号： F16J15/002 , F01D11/001 , F01D11/02 , F01D11/025 , F01D11/12 , F16J15/3288 , F05D2240/56
摘要： A brush seal assembly for turbo-engines is provided for sealing off spaces on a circumferential gap which are differently acted upon by pressure, particularly between an engine stator and an engine rotor. A holding device for a bristle bundle is provided on the engine stator, from which holding device the bristle bundle is guided between circumferential webs in a sealing manner against the engine rotor and forms an axial gap in the circumferential direction with respect to one web facing the high-pressure side. The upstream one of the circumferential webs, together with the engine rotor surface, forms an axial ring gap for flow of fluid therethrough. Turbulence reducing structure is disposed upstream of the upstream web in the high pressure space and serves to reduce the turbulence in flow of air from the upstream space through the axial ring gap. This turbulence reducing structure can be in the form of a metal sponge and/or a honey comb structure.
摘要翻译：用于涡轮发动机的刷子密封组件被设置用于密封周向间隙上的空间，其不同地受到压力的作用，特别是在发动机定子和发动机转子之间。用于刷毛束的保持装置设置在发动机定子上，保持装置使刷毛束在周向腹板之间以密封方式被引导到发动机转子上，并且相对于面向所述发动机转子的一个腹板在圆周方向上形成轴向间隙高压侧。周向腹板中的上游侧与发动机转子表面一起形成用于流过其中的流体的轴向环间隙。湍流减少结构设置在高压空间中的上游腹板的上游，并且用于减少来自上游空间的空气的流动通过轴向间隙的紊流。这种湍流减少结构可以是金属海绵和/或蜂巢结构的形式。

2. 发明授权

US5951254A Blade for fluid flow engine having a metallic coating layer, and method of manufacturing and repairing the same 失效
标题翻译：具有金属涂层的流体流动发动机用叶片及其制造和修理方法
公开(公告)号：US5951254A
公开(公告)日：1999-09-14
申请号：US891853
申请日：1997-07-09
申请人： Siegfried Sikorski , Michael Schober , Reinhold Schoenacher
发明人： Siegfried Sikorski , Michael Schober , Reinhold Schoenacher
IPC分类号： F01D5/28 , B29C70/06 , B29C70/10 , B29C73/04 , B29K105/06 , B29L31/08 , B32B15/02 , F04D29/38
CPC分类号： B32B15/02
摘要： A blade for a fluid flow machine such as a jet turbine engine includes a blade body (2) that is to be exposed to the fluid flow and therefore is subject to damage by erosion due to abrasive particle entrained in the fluid flow and due to thermal loading. The blade body (2) is a layered body including base layers (6) of a fiber reinforced synthetic material and a metallic cover layer (7) applied as an erosion protective layer onto at least a portion or the entirety of the surface of the base layers (6). The cover layer (7) includes metallic fibers or threads (9A, 9B) which are bonded with the fiber reinforced synthetic material of the adjacent base layers (6) by the same synthetic resin binder material permeating through and forming a matrix for all the layers (6 and 7). The metallic fibers or threads (9A, 9B) embedded in a synthetic resin matrix are characterized by a high degree of erosion resistance and a good tolerance for defects in the case of local impact or erosion damage. The blade may be a blade of a fan or compressor stage of a jet turbine engine. A method for manufacturing and a method for repairing such blades involves exposing outer layers of fibers of a blade, and applying thereon a cover layer of metallic fibers or threads. An additional outer protective layer may be applied on the cover layer.
摘要翻译：用于诸如喷气涡轮发动机的流体流动机的叶片包括将被暴露于流体流动的叶片体（2），并且因此由于夹带在流体流中的磨料颗粒和由于热量而受到侵蚀而损坏加载。叶片体（2）是包括纤维增强合成材料的基层（6）和作为侵蚀保护层的金属覆盖层（7）的层叠体，其至少部分或全部的基底表面层（6）。覆盖层（7）包括金属纤维或线（9A，9B），其通过相同的合成树脂粘合剂材料与相邻基层（6）的纤维增强合成材料粘合，所述合成树脂粘合剂材料渗透并形成所有层的基质（6和7）。嵌入合成树脂基体中的金属纤维或线（9A，9B）的特征在于在局部冲击或侵蚀损伤的情况下具有高抗侵蚀性和良好的缺陷耐受性。叶片可以是喷气涡轮发动机的风扇或压缩机级的叶片。制造方法和修复这种刀片的方法包括暴露刀片的纤维外层，并在其上涂敷金属纤维或线的覆盖层。可以在覆盖层上施加另外的外部保护层。

3. 发明授权

US5765376A Gas turbine engine flame tube cooling system and integral swirler arrangement 失效
标题翻译：燃气涡轮发动机火焰管冷却系统和整体旋流器布置
公开(公告)号：US5765376A
公开(公告)日：1998-06-16
申请号：US570776
申请日：1995-12-12
申请人： Nikolaos Zarzalis , Gunter Meikis
发明人： Nikolaos Zarzalis , Gunter Meikis
IPC分类号： F02C7/18 , F23R3/10 , F23R3/42 , F23R3/60
CPC分类号： F23R3/10 , F05B2260/201 , Y02T50/675
摘要： A system is provided for cooling especially the backplate of a flame tube of a combustion chamber for gas turbine engines, of the type having at least one burner arranged on the backplate and having a fuel nozzle and at least one swirler arranged coaxially with the fuel nozzle for the supply of combustion air. The backplate is cooled with compressed air diverted from a compressor and ducted to a head end of the combustion chamber. The backplate forms at least one cooling air duct to carry the compressed air supplied for backplate cooling, and the cooling air duct communicates at its outlet end at the burner with the flame tube such that the compressed air issuing from the cooling air duct enters into combustion in the primary zone. At its outlet end the cooling air duct can communicate with the air inlets of at least one swirler.
摘要翻译：一种用于燃气涡轮发动机燃烧室的火焰管的背板的系统，其特征在于，具有至少一个燃烧器布置在背板上并具有燃料喷嘴和与燃料喷嘴同轴设置的至少一个旋流器用于供应燃烧空气。背板用压缩空气从压缩机转向并被引导到燃烧室的前端进行冷却。背板形成至少一个冷却风道，以承载用于背板冷却的压缩空气，并且冷却风道在其燃烧器的出口端处与火焰管连通，使得从冷却空气管道排出的压缩空气进入燃烧在主要区域。在其出口端，冷却风道可以与至少一个旋流器的空气入口连通。

4. 发明授权

US5749706A Turbine blade wheel assembly with rotor blades fixed to the rotor wheel by rivets 失效
标题翻译：涡轮叶片组件，转子叶片由铆钉固定在转子轮上
公开(公告)号：US5749706A
公开(公告)日：1998-05-12
申请号：US794191
申请日：1997-01-24
申请人： Karl Maar
发明人： Karl Maar
IPC分类号： F01D5/30 , F01D5/32
CPC分类号： F01D5/323 , F01D5/326 , Y10T29/49321 , Y10T29/4992 , Y10T29/49956
摘要： Rotor blades (1) are held by means of toothed roots (3) in correspondingly profiled axial grooves (4) of a rotor wheel rim (5). Between each root end and the base of an axial groove (4), there is formed a radial gap (S) accommodating a rivet (6). Each rivet (6) is centrally guided on two inserts (9, 9') resting against the base of the axial groove (4) in the radial gap (S) and having bent or angled end parts (10, 10') resting against the front and rear faces of the wheel rim (5). Seating wedges (11, 11') surround the upset head (8) and the set head (7) of the rivet (6) and are axially and radially clamped to wedge-shaped complementary surfaces (G, G') of the root end and of the respective insert (9, 9') by riveting. As a result, an improved radial and axial clamping of the rotor blades is achieved.
摘要翻译：转子叶片（1）通过齿根（3）保持在转子轮缘（5）的相应成型的轴向槽（4）中。在轴向槽（4）的每个根端和底座之间，形成容纳铆钉（6）的径向间隙（S）。每个铆钉（6）在径向间隙（S）中的两个插入件（9,9'）的中心引导，该两个插入件（9,9'）靠在轴向槽（4）的基部上，并且具有弯曲或成角度的端部（10,10'），轮辋（5）的前后表面。座榫（11,11'）围绕镦锻头（8）和铆钉（6）的固定头（7），并且被轴向和径向夹紧到根端的楔形互补表面（G，G'）和相应的刀片（9,9'）铆接。结果，实现了改进的转子叶片的径向和轴向夹紧。

5. 发明授权

US5675873A Clamping ring with slanted clamping surfaces for securing flanged components to each other 失效
标题翻译：夹紧环带有倾斜的夹紧面，用于将法兰部件固定在一起
公开(公告)号：US5675873A
公开(公告)日：1997-10-14
申请号：US761853
申请日：1996-12-09
申请人： Helmut Groess
发明人： Helmut Groess
IPC分类号： F16L23/036 , F16L23/04 , B65D63/00 , F16L35/00
CPC分类号： F16L23/08 , Y10T24/1441 , Y10T24/1451
摘要： Two components such as pipes having radial end flanges with conical flange clamping surfaces are clamped together by a clamping ring having at least two ring sections with conical ring clamping surfaces engaging said conical flange clamping surfaces when clamping screws passing through section ends are tightened. The ring sections have an inner ring radius (RR) slightly larger than a respective flange radius (FR) for providing a positive but gradual engagement between said conical surfaces when said ring sections are clamped together for example by threaded bolts or screws at ring section ends.
摘要翻译：两个部件，例如具有带锥形凸缘夹紧表面的径向端部凸缘的管道通过具有至少两个环形部分的夹紧环夹紧在一起，当夹紧通过截面端部的螺钉被拧紧时，锥形环夹紧表面接合所述圆锥形凸缘夹紧表面。环形部分具有比相应的凸缘半径（FR）稍大的内环半径（RR），用于当所述环形部分被夹紧在一起时提供所述圆锥形表面之间的正但逐渐的接合，例如通过环形部分端部处的螺栓或螺钉。

6. 发明授权

US5593282A Turbomachine rotor construction including a serrated root section and a rounded terminal portion on a blade root, especially for an axial-flow turbine of a gas turbine engine 失效
标题翻译：涡轮机转子结构包括锯齿状根部部分和叶片根部上的圆形终端部分，特别是用于燃气涡轮发动机的轴流涡轮机
公开(公告)号：US5593282A
公开(公告)日：1997-01-14
申请号：US527876
申请日：1995-09-14
申请人： Wolfgang Krueger
发明人： Wolfgang Krueger
IPC分类号： F01D5/28 , F01D5/30 , F01D5/20
CPC分类号： F01D5/225 , F01D5/3007 , F01D5/3084 , Y02T50/671
摘要： A rotor of a turbomachine includes blades having an improved blade root configuration for anchoring and centering the blade roots in axial slots of the rotor disk. Each blade root includes two portions or sections, namely a serrated section that has a single bilaterally uniformly shaped serration, and a terminal portion that has rounded surfaces and a narrower cross-section than the serrated root section. The serrated section provides anchoring against centrifugal forces. The terminal portion provides the predominant centering effect, for which it is radially movably received and located in a recess provided in the bottom of the slot. The special root configuration substantially avoids misfit and centering problems associated with manufacturing variances, whereby the blades and blade roots can be made of lightweight engineering materials.
摘要翻译：涡轮机的转子包括具有改进的叶片根部构造的叶片，用于将叶片根部固定和定心在转子盘的轴向槽中。每个叶片根部包括两个部分或部分，即具有单个双边均匀形状的锯齿状的锯齿状部分，以及具有圆形表面和比锯齿状根部部分更窄的横截面的端部部分。锯齿部分提供了抵抗离心力的锚定。端子部分提供主要的定心作用，其可径向移动地容纳并位于设置在槽底部的凹槽中。特殊的根结构基本上避免了与制造方差有关的失配和对中问题，由此叶片和叶片根部可以由轻质工程材料制成。

7. 发明授权

US5557846A Blank for the manufacturing of fiber reinforced coatings or metal components 失效
标题翻译：用于制造纤维增强涂层或金属部件的空白
公开(公告)号：US5557846A
公开(公告)日：1996-09-24
申请号：US474959
申请日：1995-06-07
申请人： William Wei , Thomas Stoll
发明人： William Wei , Thomas Stoll
IPC分类号： B22F3/00 , B23P17/06 , B29C70/22 , C22C47/20 , D04B1/00 , D04B1/14 , B23P15/02
CPC分类号： B29C70/22 , B22F3/002 , B23P17/06 , C22C47/20 , D04B1/00 , D04B1/123 , D04B1/14 , B22F2998/00 , B29K2305/00 , B29K2309/04 , B29L2031/7504 , D10B2403/02411 , D10B2505/02 , Y10S428/902 , Y10T29/4932 , Y10T29/49801 , Y10T428/2918 , Y10T442/109 , Y10T442/11
摘要： A blank material for manufacturing fiber-reinforced coatings or metal components comprising fibers made of a high-strength material and metals or metal alloys, and a process for manufacturing the blank, and for manufacturing coatings and components made therefrom. The fibers are aligned in the blank in parallel to its axis, and metal wire meshes are knitted around them, with the fibers embedded at a distance from one another. By means of high-temperature isostatic pressing, metal components can be made, through which the reinforcing fibers extend at a uniform distance.
摘要翻译：用于制造包含由高强度材料和金属或金属合金制成的纤维的纤维增强涂层或金属部件的坯料，以及用于制造坯料的方法以及用于制造由其制成的涂层和部件。纤维在坯料中平行于其轴线对齐，金属丝网围绕它们编织，纤维彼此间隔一定距离。通过高温等静压，可以制造金属部件，增强纤维通过该部件以均匀的距离延伸。

8. 发明授权

US5480160A Shaft seal with in-line sealing rings 失效
标题翻译：带密封环的轴封
公开(公告)号：US5480160A
公开(公告)日：1996-01-02
申请号：US236376
申请日：1994-05-02
申请人： Axel Harms
发明人： Axel Harms
IPC分类号： F16J15/00 , F16J15/26 , F16J15/16 , F16J15/40
CPC分类号： F16J15/006 , F16J15/26
摘要： A shaft seal (5) for circumferential shaft speeds in excess of 30 m/s and for sealing a differential pressure between two chambers to be sealed, in excess of 100 kP, has several in-line sealing rings (12A, 12B, 20, 22). Preferably, at least two of the high-pressure side seal rings are constructed as slide seal rings (12A, 12B) that are urged against the shaft by a tension spring (17) surrounding the outer circumferential surface of the slide seal rings. One low-pressure side sealing ring is a brush seal (20). A compressed air seal ring (22) is arranged between this brush seal (20) and the slide seal rings (12A, 12B). The air seal ring (22) forms a radial air gap (24) around the shaft (1). In operation of the seal the pressure in the air gap (24) is lower than the pressure in the high-pressure chamber (HD) and higher than the pressure in the low-pressure chamber (ND), whereby a high sealing integrity and resistance to abrasive wear at very high circumferential shaft speeds in excess of 100 m/s and at high differential pressures are maintained.
摘要翻译：用于圆周轴速度超过30m / s并用于密封待密封的两个室之间的压差超过100kP的轴密封件（5）具有几个直列密封环（12A，12B，20， 22）。优选地，至少两个高压侧密封环被构造为滑动密封环（12A，12B），其通过围绕滑动密封环的外周表面的拉伸弹簧（17）而被推靠在轴上。一个低压侧密封环是刷密封件（20）。在该刷子密封件（20）和滑动密封环（12A，12B）之间布置有压缩空气密封环（22）。空气密封环（22）围绕轴（1）形成径向气隙（24）。在密封操作中，气隙（24）中的压力低于高压室（HD）中的压力并且高于低压室（ND）中的压力，由此高密封完整性和电阻在非常高的周向轴速度超过100m / s并且在高压差下保持磨损。

9. 发明授权

US5344686A Tension strained fiber structure component 失效
标题翻译：拉伸应变纤维结构部件
公开(公告)号：US5344686A
公开(公告)日：1994-09-06
申请号：US861808
申请日：1992-08-18
申请人： Horst Heubert
发明人： Horst Heubert
IPC分类号： B29C70/68 , B29C70/02 , F01D5/28 , F16C7/00 , B32B1/04
CPC分类号： F16C7/026 , B29C70/023 , F01D5/282 , Y10S428/902 , Y10T428/238 , Y10T428/24132 , Y10T428/24777
摘要： A tension strained fiber structure component comprises a plurality of mutually connected structural elements which each consists of a fiber strand plate aligned in the tension direction and of a pressure plate extending at an acute angle with respect to the tension direction, which are both connected with one another. As a result, a favorable introduction of the tension forces into a separate supporting component can be achieved.
摘要翻译： PCT No.PCT / DE90 / 00979 Sec。 371日期：1992年8月18日 102（e）日期1992年8月18日PCT 1990年12月20日PCT PCT。公开号WO91 / 08893 1991年6月27日。张力应变纤维结构部件包括多个相互连接的结构元件，每个结构元件由沿张力方向排列的纤维绞线板和相对于张力方向以锐角延伸的压板，它们都相互连接。结果，可以实现将张力有利地引入单独的支撑部件中。

10. 发明授权

US5232789A Structural component with a protective coating having a nickel or cobalt basis and method for making such a coating 失效
标题翻译：具有镍或钴基保护层的结构部件和制造这种涂层的方法
公开(公告)号：US5232789A
公开(公告)日：1993-08-03
申请号：US845763
申请日：1992-03-02
申请人： Albin Platz , Klaus Schweitzer , Peter Adam
发明人： Albin Platz , Klaus Schweitzer , Peter Adam
IPC分类号： C23C4/10 , C23C4/18 , C23C30/00 , F01D5/28
CPC分类号： F01D5/288 , C23C30/00 , C23C4/10 , C23C4/18 , Y10S428/937 , Y10T428/12646 , Y10T428/12931
摘要： A structural component made of a base metal composition on a nickel or cobalt basis is provided with a protective coating against oxidation, corrosion, and thermal fatigue. The protective coating and the base metal are made of chemically the same or identical material, whereby the bonding of the protective coating is increased, the tendency to crack is reduced, and the resistance to thermal fatigue is improved. The grain size of the coating is substantially smaller than the grain size of the base metal composition.
摘要翻译：由基于镍或钴的贱金属组合物制成的结构部件具有防氧化，腐蚀和热疲劳的保护涂层。保护涂层和母材由化学相同或相同的材料制成，由此保护涂层的粘结增加，裂纹的倾向减小，耐热疲劳性得到改善。涂层的晶粒尺寸显着小于贱金属组合物的晶粒尺寸。

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