专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

11. 发明授权

US07070391B2 Hollow fan blade for gas turbine engine 有权
标题翻译：用于燃气轮机的中空风扇叶片
公开(公告)号：US07070391B2
公开(公告)日：2006-07-04
申请号：US10765741
申请日：2004-01-26
申请人： Michael A. Weisse
发明人： Michael A. Weisse
IPC分类号： F01D5/18
CPC分类号： F01D5/18 , B23P15/04 , F01D5/147 , F04D29/324 , F05D2220/324 , F05D2220/36 , F05D2230/10 , F05D2230/60 , Y02T50/671 , Y02T50/676
摘要： Hollow fan blades for turbo fan gas turbine engines are formed of two separate detail halves. Each detail half has a plurality of cavities and ribs machined out to reduce weight. These detail halves are subsequently bonded and given an airfoil shape in the forming operation. In the present invention, the ribs are oriented biased to provide stiffness as needed in different sections of the fan blade with smooth transitions between regions. The ribs and cavities do not run solely radially or chordwise, but curve and change direction. The path of each cavity is curved sufficiently to eliminate any regions with long, straight cavities, which would have low inertia in cross sections through the cavity parallel to the rib. Preferably, cavities do not continue straight in any direction for lengths greater than half the blade chord (e.g. leading edge to trailing edge) before curvature causes the rib to intersect cross section.
摘要翻译：用于涡轮风扇燃气涡轮发动机的空心风扇叶片由两个独立的细节一半形成。每个细节一半具有加工成多个空腔和肋，以减轻重量。随后在成型操作中结合这些细部半部并给予翼型形状。在本发明中，肋被定向偏置以根据需要在风扇叶片的不同部分中提供刚度，并且在区域之间具有平滑的过渡。肋骨和空腔不能径向或弦向，而是曲线并改变方向。每个腔的路径足够弯曲，以消除任何具有长而直的空腔的区域，这些区域通过平行于肋的空腔的横截面具有较低的惯性。优选地，在弯曲导致肋与横截面相交之前，空腔不会在任何方向上持续直线长度大于叶片弦（例如前缘到后缘）的长度。

12. 发明授权

US07052238B2 Hollow fan blade for gas turbine engine 有权
标题翻译：用于燃气轮机的中空风扇叶片
公开(公告)号：US07052238B2
公开(公告)日：2006-05-30
申请号：US10765593
申请日：2004-01-26
申请人： Daniel J. Whitesell , Michael A. Weisse , Christopher Mark Palazzini
发明人： Daniel J. Whitesell , Michael A. Weisse , Christopher Mark Palazzini
IPC分类号： F01D5/18
CPC分类号： B23P15/04 , F01D5/147 , F01D5/18 , F04D29/324 , F05D2220/324 , F05D2220/36 , F05D2230/10 , Y02T50/671 , Y02T50/676 , Y10T29/49339
摘要： A hollow fan blade for turbo fan gas turbine engines is formed of two separate detail halves. Each detail half has a plurality of cavities and ribs machined out to reduce weight. These detail halves are subsequently bonded and given an airfoil shape in the forming operation. The present invention provides a hollow fan blade with internal cavity and rib geometry with improved durability that permits the bonding and forming to be performed without the need for gas pressurization. The ability to form the hollow fan blade of the present invention without gas pressurization is a result of the cavity and rib geometry and the orientation of the ribs. The ribs are tapered and transition into a compound radius of the floor that simulates the classical arch design element. The orientation of the ribs is generally in a parallel plane with the load vector that results from forming loads during the pre-form and final form operations. This orientation provides compressive stress transfer into the ribs and away from the concave and convex skins. The rib spacing is controlled where ribs can not be held in a parallel plane with the load vector.
摘要翻译：用于涡轮风扇燃气涡轮发动机的中空风扇叶片由两个单独的细节半部形成。每个细节一半具有加工成多个空腔和肋，以减轻重量。随后在成型操作中结合这些细部半部并给予翼型形状。本发明提供一种具有内腔和肋几何结构的中空风扇叶片，其具有改进的耐久性，其允许在不需要气体加压的情况下执行粘结和成形。在没有气体加压的情况下形成本发明的中空风扇叶片的能力是肋和肋的几何形状和取向。肋骨是渐缩的，并转变成模拟古典拱形设计元素的地板的复合半径。肋的取向通常在与预成型和最终成型操作期间形成载荷的负载向量平行的平面中。该方向提供压缩应力传递到肋中并远离凹凸表皮。肋条间距被控制，其中肋不能与负载矢量保持在平行的平面中。

13. 发明授权

US5419040A Hollow fan blade fabrication 失效
标题翻译：中空风扇叶片制造
公开(公告)号：US5419040A
公开(公告)日：1995-05-30
申请号：US237436
申请日：1994-04-29
申请人： Michael A. Weisse , David B. Carter
发明人： Michael A. Weisse , David B. Carter
IPC分类号： B23P15/04 , F01D5/14 , F01D5/18 , B23P15/00
CPC分类号： F01D5/147 , B23P15/04 , Y02T50/671 , Y10T29/49336 , Y10T29/49339 , Y10T29/49893
摘要： Purge flow openings through chordwise ribs in hollow fan blades are formed by making partial circular cuts at the rib edges before diffusion bonding the blade halves. A full semi-circular section is used on the pressure side, but only a segment of a semicircular section is used on the suction side.
摘要翻译：在中空风扇叶片之间吹扫通过弦肋的流动开口通过在扩散接合叶片半部之前在肋边缘处进行部分圆形切割而形成。在压力侧使用完整的半圆形截面，但在吸力侧仅使用半圆形截面。

14. 发明申请

US20130319010A1 AIRFOIL COVER SYSTEM 有权
标题翻译：气翼罩系统
公开(公告)号：US20130319010A1
公开(公告)日：2013-12-05
申请号：US13488556
申请日：2012-06-05
申请人： Kwan Hui , Michael A. Weisse
发明人： Kwan Hui , Michael A. Weisse
IPC分类号： F01D5/14 , B23P15/00 , F02C3/04 , F01D5/18 , F01D1/04
CPC分类号： F01D5/141 , B23P15/04 , F01D5/147 , F01D5/282 , F04D29/023 , F04D29/324 , F05D2220/36 , F05D2230/23 , F05D2260/941 , F05D2300/50212 , F05D2300/603 , F05D2300/615 , Y02T50/672 , Y02T50/673 , Y10T29/49236
摘要： An example airfoil for a gas turbine engine includes a body having a first surface extending from a first edge to a second edge and a cavity disposed in the body. A first cover is at least partially disposed within the cavity. The first cover includes a first portion cooperates with a corresponding second portion. A second cover covers the first cover and forms at least a portion of the first surface with the body. The first cover is disposed between the body and the second cover. The first cover and the second cover have a different coefficient of thermal expansion than the body.
摘要翻译：用于燃气涡轮发动机的示例性翼型件包括具有从第一边缘延伸到第二边缘的第一表面的主体和设置在主体中的空腔。第一盖至少部分地设置在腔内。第一盖包括与对应的第二部分配合的第一部分。第二盖覆盖第一盖并且与主体形成第一表面的至少一部分。第一盖设置在主体和第二盖之间。第一盖和第二盖具有与身体不同的热膨胀系数。

15. 发明申请

US20130108470A1 ROTOR BLADE WITH BONDED COVER 有权
公开(公告)号：US20130108470A1
公开(公告)日：2013-05-02
申请号：US13286371
申请日：2011-11-01
申请人： Michael A. Weisse
发明人： Michael A. Weisse
IPC分类号： F01D5/18
CPC分类号： F01D5/147 , B23P15/04 , F01D5/16 , F04D29/324 , F05D2230/23 , F05D2240/301 , F05D2250/61 , Y02T50/672 , Y02T50/673
摘要： An airfoil comprises an airfoil body with an internal cavity and inner and outer covers. The airfoil body defines a first major surface of the airfoil, and a rib extends along the internal cavity. The inner cover is bonded to the airfoil body over the internal cavity, and includes a coupling element extending along the internal cavity in cooperative engagement with the rib. The outer cover is bonded to the airfoil body over the inner cover, and defines a second major surface of the airfoil.

16. 发明授权

US06994524B2 Hollow fan blade for gas turbine engine 有权
标题翻译：用于燃气轮机的中空风扇叶片
公开(公告)号：US06994524B2
公开(公告)日：2006-02-07
申请号：US10765347
申请日：2004-01-26
申请人： William D. Owen , Michael A. Weisse , Daniel J. Whitesell
发明人： William D. Owen , Michael A. Weisse , Daniel J. Whitesell
IPC分类号： F01D5/18
CPC分类号： B23P15/04 , F01D5/147 , F01D5/18 , F04D29/324 , F05D2220/324 , F05D2220/36 , F05D2230/10 , F05D2230/60 , Y02T50/671 , Y02T50/676
摘要： Hollow fan blades for turbo fan gas turbine engines are formed of two separate detail halves. Each detail half has a plurality of cavities and ribs machined out to reduce weight. These detail halves are subsequently bonded and given an airfoil shape in the forming operation. In the present invention, the ribs are oriented biased to provide stiffness as needed in different sections of the fan blade with smooth transitions between regions. The result is a blade with good protection from a wide spectrum of external threats.
摘要翻译：用于涡轮风扇燃气涡轮发动机的空心风扇叶片由两个独立的细节一半形成。每个细节一半具有加工成多个空腔和肋，以减轻重量。随后在成型操作中结合这些细部半部并给予翼型形状。在本发明中，肋被定向偏置以根据需要在风扇叶片的不同部分中提供刚度，并且在区域之间具有平滑的过渡。结果是一个刀片具有良好的保护，不受广泛的外部威胁。

17. 发明授权

US5584660A Increased impact resistance in hollow airfoils 失效
标题翻译：中空翼型的抗冲击性提高
公开(公告)号：US5584660A
公开(公告)日：1996-12-17
申请号：US430948
申请日：1995-04-28
申请人： David B. Carter , Michael A. Weisse
发明人： David B. Carter , Michael A. Weisse
IPC分类号： B23P15/04 , F01D5/14 , F01D5/18
CPC分类号： F01D5/147 , B23P15/04 , F05D2200/23 , Y02T50/671 , Y10S416/02 , Y10T29/49339
摘要： A hollow airfoil (10) for a gas turbine engine having a leading edge (12), a trailing edge (14), a pressure side (20), and a suction side (22) includes a plurality of internal spanwise stiffening ribs (31-35) that are arranged in a logarithmic pattern. The particular arrangement of internal fibs (31-35) optimizes stiffness of the airfoil (10) without significantly increasing the weight thereof.
摘要翻译：一种用于具有前缘（12），后缘（14），压力侧（20）和吸力侧（22）的燃气涡轮发动机的中空翼片（10）包括多个内翼展加强筋 -35），它们以对数模式排列。内部纤维（31-35）的特定布置优化翼型件（10）的刚度，而不显着增加其重量。

18. 发明授权

US5443367A Hollow fan blade dovetail 失效
标题翻译：空心扇叶燕尾榫
公开(公告)号：US5443367A
公开(公告)日：1995-08-22
申请号：US200128
申请日：1994-02-22
申请人： Marc Samit , Michael A. Weisse
发明人： Marc Samit , Michael A. Weisse
IPC分类号： F01D5/14 , F01D5/30 , F04D29/32
CPC分类号： F01D5/3007 , F01D5/147 , F04D29/324 , Y02T50/671 , Y02T50/673
摘要： A gas turbine engine fan blade having an airfoil portion and a dovetail root portion is enhanced by having spaced apart supporting ribs extend into the dovetail root portion. The supporting ribs define a plurality of hollow cavities extending into the dovetail root portion of the fan blade. The extended cavities reduce the weight of each blade and also improve the integrity of each blade.
摘要翻译：具有翼型部分和燕尾根部的燃气涡轮发动机风扇叶片通过具有间隔开的支撑肋延伸到燕尾根部而被增强。支撑肋限定延伸到风扇叶片的燕尾根部的多个中空腔。延长的空腔减少每个叶片的重量并且还提高每个叶片的完整性。

19. 发明申请

US20130167555A1 ALUMINUM FAN BLADE CONSTRUCTION WITH WELDED COVER 有权
标题翻译：铝合金风扇叶片结构与焊接盖
公开(公告)号：US20130167555A1
公开(公告)日：2013-07-04
申请号：US13343025
申请日：2012-01-04
申请人： Frederick M. Schwarz , Michael A. Weisse
发明人： Frederick M. Schwarz , Michael A. Weisse
IPC分类号： F01D5/14 , B23K20/12 , B23K31/02 , F02C3/04 , F01D5/28
CPC分类号： B23K20/1265 , B23K2101/001 , F01D5/147 , F01D5/28 , F05D2220/36 , F05D2230/232 , F05D2300/121
摘要： An airfoil includes, among other possible things, a main body extending between a leading edge and a trailing edge. Channels are formed into the main body, with a plurality of ribs extending intermediate the channels. A cover skin is attached to the main body. The cover skin is welded to the main body at outer edges. An adhesive is placed between inner surfaces of the cover skin and the main body. The adhesive is deposited inwardly of the outer edges of the cover skin.
摘要翻译：除了其他可能的事情之外，翼型件还包括在前缘和后缘之间延伸的主体。通道形成在主体中，多个肋在通道之间延伸。覆盖皮肤附着在主体上。覆盖皮肤在外边缘焊接到主体。将粘合剂放置在覆盖皮肤和主体的内表面之间。粘合剂沉积在覆盖皮肤的外边缘的内侧。

20. 发明授权

US07334333B2 Method for making a hollow fan blade with machined internal cavities 有权
标题翻译：制造具有加工内腔的中空风扇叶片的方法
公开(公告)号：US07334333B2
公开(公告)日：2008-02-26
申请号：US10765591
申请日：2004-01-26
申请人： Christopher Mark Palazzini , Michael A. Weisse , Douglas A. Senecal
发明人： Christopher Mark Palazzini , Michael A. Weisse , Douglas A. Senecal
IPC分类号： B21K3/04 , B21D53/78 , B23P15/08
CPC分类号： F01D5/147 , B23P15/04 , F01D5/18 , F04D29/324 , F05D2220/324 , F05D2220/36 , F05D2230/10 , F05D2230/60 , Y02T50/671 , Y02T50/676 , Y10T29/49336 , Y10T29/49339 , Y10T29/49341 , Y10T29/49893 , Y10T29/49995 , Y10T409/303752
摘要： Hollow fan blades for turbo fan gas turbine engines are formed of two separate detail halves. Each detail half has a plurality of cavities and ribs machined out to reduce weight. The floor and opposite interior walls of each cavity are machined simultaneously. The configuration minimizes the number of cutter plunge cuts for the internal cavities, and maximizes cutter size, in order to minimize the time required to machine them. These detail halves are subsequently bonded and given an airfoil shape in the forming operation.
摘要翻译：用于涡轮风扇燃气涡轮发动机的空心风扇叶片由两个独立的细节一半形成。每个细节一半具有加工成多个空腔和肋，以减轻重量。每个腔体的地板和相对的内壁都被同时加工。该配置最大限度地减少了内部空腔的切割刀片切割次数，并最大化了刀具尺寸，以最大限度地减少加工刀具所需的时间。随后在成型操作中结合这些细部半部并给予翼型形状。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式