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1. 发明授权

US4555901A Combustion chamber construction 失效
标题翻译：燃烧室施工
公开(公告)号：US4555901A
公开(公告)日：1985-12-03
申请号：US316532
申请日：1972-12-19
申请人： Thomas G. Wakeman , Harvey M. Maclin
发明人： Thomas G. Wakeman , Harvey M. Maclin
IPC分类号： F23R3/00 , F23R3/08 , F02C7/20
CPC分类号： F23R3/08 , F23R3/002 , F05B2230/70 , F05B2230/80
摘要： A combustion chamber for use in gas turbine engines is provided with a liner formed of a high temperature material. The liner includes a plurality of panels of material mounted by means of a slideable, frictional mounting arrangement upon a high strength structural frame. As a result of this mounting arrangement, the liner is substantially isolated from structural forces associated with the combustion chamber, while the frame is substantially isolated from thermal stresses associated with the liner. Means are provided for positioning and securing individual panel members axially relative to the frame. The panels may be continuous annular bodies, or may be circumferentially segmented. In the latter case, means are provided for mounting individual panels in a slideable, frictional cooperation with laterally adjacent panels, as well as for sealing the abutting junctions. The individual liner panels may be easily removed for repair or replacement without disassembling the frame and associated components.
摘要翻译：用于燃气涡轮发动机的燃烧室设置有由高温材料形成的衬套。衬套包括通过可滑动的摩擦安装装置安装在高强度结构框架上的多个材料面板。作为这种安装结构的结果，衬套基本上与与燃烧室相关联的结构力隔离，而框架基本上与衬套相关联的热应力隔离。提供了用于相对于框架轴向地定位和固定单个面板构件的装置。面板可以是连续的环形体，或者可以是圆周分段的。在后一种情况下，提供了用于将单独的面板安装在与横向相邻的面板可滑动，摩擦协作以及用于密封邻接结的装置。单独的衬板可以容易地移除用于修理或更换，而不拆卸框架和相关组件。

2. 发明授权

US4796423A Sheet metal panel 失效
标题翻译：钣金面板
公开(公告)号：US4796423A
公开(公告)日：1989-01-10
申请号：US4827
申请日：1987-01-12
申请人： Louis Lievestro , James S. Kelm , Arthur L. Ludwig , Harvey M. Maclin , Thomas G. Wakeman
发明人： Louis Lievestro , James S. Kelm , Arthur L. Ludwig , Harvey M. Maclin , Thomas G. Wakeman
IPC分类号： F01D9/04 , F02G1/00 , F02G3/00
CPC分类号： F01D9/04 , Y10T403/4327 , Y10T403/7016
摘要： A sheet metal panel comprising a bent region is disclosed. The region defines a first arc of intersection with a first plane and a second arc of intersection with a second plane. The second arc has a radius of less than twice the thickness of the panel.
摘要翻译：公开了一种包括弯曲区域的金属板。该区域定义与第一平面和第二平面相交的第一弧线的第一交叉圆弧。第二弧的半径小于面板厚度的两倍。

3. 发明授权

US4679400A Variable turbine vane support 失效
标题翻译：可变涡轮叶片支架
公开(公告)号：US4679400A
公开(公告)日：1987-07-14
申请号：US754678
申请日：1985-07-12
申请人： James S. Kelm , Harvey M. Maclin , Edward C. Vickers , Thomas G. Wakeman
发明人： James S. Kelm , Harvey M. Maclin , Edward C. Vickers , Thomas G. Wakeman
IPC分类号： F01D17/16 , F23R3/60 , F02C1/00
CPC分类号： F01D17/162 , F23R3/60
摘要： Means for axially attaching a variable turbine vane array to a combustor in a gas turbine engine is disclosed. The attachment means are configured so that substantially all of the axial load on the array is transmitted through the walls of the combustor.
摘要翻译：公开了用于将可变涡轮叶片阵列轴向附接到燃气涡轮发动机中的燃烧器的装置。附接装置被构造成使得阵列上的基本上所有的轴向负载都通过燃烧器的壁传递。

4. 发明授权

US4628694A Fabricated liner article and method 失效
公开(公告)号：US4628694A
公开(公告)日：1986-12-16
申请号：US562959
申请日：1983-12-19
申请人： James S. Kelm , Arthur L. Ludwig , Harvey M. Maclin , Steven K. Roggenkamp , Thomas G. Wakeman
发明人： James S. Kelm , Arthur L. Ludwig , Harvey M. Maclin , Steven K. Roggenkamp , Thomas G. Wakeman
IPC分类号： B21D35/00 , F23R3/00 , F02C7/00
CPC分类号： F23R3/002 , B21D35/00 , F05B2260/201 , F23R2900/00018
摘要： A method of fabricating sheet metal panels and the article produced thereby. According to one form, the method of fabrication includes the steps of providing a panel of sheet metal, perforating the panel to provide a plurality of holes, forming the panel into a preselected curve about a longitudinal centerline, forming the leading edge portion of the panel into a front flange, forming a shoulder in the panel centered on the holes and extending perpendicularly from a surface thereof, bending an outer portion of the shoulder into a lip, and bonding the portions of the panel comprising the shoulder and lip.

5. 发明授权

US5181379A Gas turbine engine multi-hole film cooled combustor liner and method of manufacture 失效
标题翻译：气体涡轮发动机多孔薄膜冷却COMBUSTOR内胆及其制造方法
公开(公告)号：US5181379A
公开(公告)日：1993-01-26
申请号：US614418
申请日：1990-11-15
申请人： Thomas G. Wakeman , Alan Walker , Harvey M. Maclin
发明人： Thomas G. Wakeman , Alan Walker , Harvey M. Maclin
IPC分类号： F02K3/10 , B23K26/38 , F02K1/82 , F23R3/00 , F23R3/06
CPC分类号： F23R3/002 , B23K26/389 , F02K1/822 , F05D2260/202 , Y02T50/67 , Y02T50/671 , Y02T50/676
摘要： A gas turbine engine combustor is provided, having a single wall sheet metal liner which is generally annular in shape which may be corrugated and a multi-hole film cooling means which includes at least one pattern of a great many small closely spaced sharply downstream angled film cooling holes disposed essentially along portion of the liner to be cooled. Another embodiment provided a corrugated aircraft engine afterburner sheet metal liner having at least one pattern of great many small closely spaced sharply downstream angled film cooling holes disposed essentially along the entire surface of the liner.

6. 发明授权

US4688310A Fabricated liner article and method 失效
标题翻译：制造衬管制品和方法
公开(公告)号：US4688310A
公开(公告)日：1987-08-25
申请号：US897941
申请日：1986-08-19
申请人： James S. Kelm , Arthur L. Ludwig , Harvey M. Maclin , Steven K. Roggenkamp , Thomas G. Wakeman
发明人： James S. Kelm , Arthur L. Ludwig , Harvey M. Maclin , Steven K. Roggenkamp , Thomas G. Wakeman
IPC分类号： B21D35/00 , F23R3/00 , B21K3/04 , B21D53/00
CPC分类号： F23R3/002 , B21D35/00 , F05B2260/201 , Y10T29/49323
摘要： A method of fabricating sheet metal panels and the article produced thereby. According to one form, the method of fabrication includes the steps of providing a panel of sheet metal, perforating the panel to provide a plurality of holes, forming the panel into a preselected curve about a longitudinal centerline, forming the leading edge portion of the panel into a front flange, forming a shoulder in the panel centered on the holes and extending perpendicularly from a surface thereof, bending an outer portion of the shoulder into a lip, and bonding the portions of the panel comprising the shoulder and lip.
摘要翻译：一种制造金属板的方法和由此制造的制品。根据一种形式，制造方法包括以下步骤：提供一块金属板，穿孔面板以提供多个孔，将面板形成围绕纵向中心线的预选曲线，形成面板的前缘部分形成前凸缘，在面板的中心形成一个肩部并从其表面垂直延伸，将肩部的外部部分弯曲成唇部，并且将包括肩部和唇部的面板的部分粘结。

7. 发明授权

US5370427A Expansion joint for fluid piping with rotation prevention member 失效
标题翻译：带旋转防止件的流体管道膨胀节
公开(公告)号：US5370427A
公开(公告)日：1994-12-06
申请号：US179286
申请日：1994-01-10
申请人： James S. Hoelle , Ivan H. Peterson , Thomas G. Wakeman , Michael R. Storage , Michael A. Umney , Mark K. Meyer
发明人： James S. Hoelle , Ivan H. Peterson , Thomas G. Wakeman , Michael R. Storage , Michael A. Umney , Mark K. Meyer
IPC分类号： F02C7/18 , F16L27/11 , F16L27/12
CPC分类号： F16L27/11 , F16L27/026
摘要： An expansion joint for connecting first and second fluid-carrying pipes comprising first and second annular couplings which are operably affixable to respective ones of the pipes. In a preferred embodiment the couplings include cylindrical bores of substantially the same diameter disposed relative to one another to form a passage for providing flow communication between the pipes. An annular bellows extends between the couplings for accommodating relative axial movement and angular misalignment between the pipes and is disposed radially outward of the passage to capture any fluid leaking between the interfacing surfaces of the couplings. A second cylindrical bore of a first one of the couplings engages an outer spherical surface of the second coupling to allow the second coupling to pivot in a manner which accommodates angular misalignment between the pipes. Means are provided for limiting the pivoting of the second coupling and for preventing the first coupling from rotating about a centerline of the joint, thereby avoiding unacceptable bending and torsional loading of the bellows. The expansion joint further includes means for limiting the axial compression and axial extension of the bellows.
摘要翻译：一种用于连接第一和第二流体输送管的膨胀接头，包括第一和第二环形联接器，其可操作地固定在相应的管道中。在优选实施例中，联接器包括相对于彼此设置的基本上相同直径的圆柱形孔，以形成用于在管之间提供流动连通的通道。环形波纹管在耦合器之间延伸，用于容纳管道之间的相对轴向运动和角度偏移，并且设置在通道的径向外侧，以捕获在联接器的接口表面之间泄漏的任何流体。联接器中的第一联接器的第二圆柱形孔接合第二联接器的外球面，以允许第二联接器以容纳管之间的角度偏移的方式枢转。提供了用于限制第二联接器的枢转并且用于防止第一联接件围绕接头的中心线旋转的装置，从而避免波纹管的不可接受的弯曲和扭转负载。膨胀接头还包括用于限制波纹管的轴向压缩和轴向延伸的装置。

8. 发明授权

US5127793A Turbine shroud clearance control assembly 失效
标题翻译：涡轮机清洁控制组件
公开(公告)号：US5127793A
公开(公告)日：1992-07-07
申请号：US531288
申请日：1990-05-31
申请人： Alan Walker , Thomas G. Wakeman , Dean T. Lenahan , Larry W. Plemmons , Andrew P. Elovic
发明人： Alan Walker , Thomas G. Wakeman , Dean T. Lenahan , Larry W. Plemmons , Andrew P. Elovic
IPC分类号： F01D11/10 , F01D11/08 , F01D25/24 , F02C7/00 , F02C7/20 , F02C7/28
CPC分类号： F01D25/246 , F01D11/08 , F05D2240/11
摘要： The clearances between an array of high pressure turbine blades and its surrounding high pressure turbine shroud as well as the clearances between an array of low pressure turbine blades and its associated low pressure turbine shroud are carefully controlled by a support structure which provides for evenly controlled circumferential cooling of the shroud support structure. Radial loads on the shroud support structure are reduced by counterbalancing loads imposed on the support structure by the shroud with predetermined pressure loads controlled and set through a series of cooling air cavities. The high pressure turbine shroud and low pressure turbine shroud are formed as integral segments in a segmented shroud design. Forward and aft shroud hanger members interconnect the shroud with its support so as to facilitate assembly and disassembly of the shroud segments to and from their support structure.
摘要翻译：高压涡轮机叶片阵列及其周围的高压涡轮机罩之间的间隙以及低压涡轮叶片阵列与其相关联的低压涡轮机罩之间的间隙由支撑结构小心地控制，所述支撑结构提供均匀控制的圆周护罩支撑结构的冷却。护罩支撑结构上的径向载荷通过由具有通过一系列冷却空气腔控制和设定的预定压力负载的护罩平衡负载施加在支撑结构上而减小。高压涡轮机护罩和低压涡轮机护罩在分段护罩设计中形成为整体段。前部和后部护罩悬挂构件将护罩与其支撑件互连，以便于护罩段与其支撑结构的组装和拆卸。

9. 发明授权

US4657484A Blade pitch varying means 失效
标题翻译：叶片间距变化手段
公开(公告)号：US4657484A
公开(公告)日：1987-04-14
申请号：US647283
申请日：1984-09-04
申请人： Thomas G. Wakeman , Neil Walker
发明人： Thomas G. Wakeman , Neil Walker
IPC分类号： B64C11/30 , B64C11/38 , B64C11/48
CPC分类号： B64C11/38 , B64C11/306 , B64D2027/005 , Y02T50/66
摘要： Blade pitch varying means for use in a gas turbine engine are disclosed. The blade pitch varying means may be used on an engine with a single row or two counterrotating rows of variable pitch blades which are disposed outwardly from an annular gas flowpath and which are connected with a rotating airfoil within the flowpath. The blade pitch varying means comprise actuation means, bearing means, and gearing means. The actuation means are in a nonrotating reference frame disposed inwardly from the flowpath and deliver an axial force. The bearing means transmit the axial force from the nonrotating into a rotating reference frame which contains both the propulsor blade and the airfoil in the gas flowpath. The gearing means are located in the rotating reference frame and convert the axial force into a force for varying the blade pitch.
摘要翻译：公开了一种用于燃气涡轮发动机的叶片间距变化装置。叶片桨距变化装置可以用于具有单排或两排可变桨距叶片的发动机，该排或两个可逆桨叶叶片从环形气体流路向外设置并且与流路内的旋转翼型件连接。叶片间距变化装置包括致动装置，轴承装置和传动装置。致动装置位于从流动路径向内设置并提供轴向力的非旋转基准框架中。轴承装置将来自非旋转的轴向力传递到在气体流动路径中包含推进器叶片和翼型的旋转参考框架。传动装置位于旋转的参考系中，并将轴向力转换成用于改变叶片间距的力。

10. 发明授权

US4187675A Compact air-to-air heat exchanger for jet engine application 失效
标题翻译：用于喷气发动机应用的紧凑型空气 - 空气热交换器
公开(公告)号：US4187675A
公开(公告)日：1980-02-12
申请号：US842139
申请日：1977-10-14
申请人： Thomas G. Wakeman
发明人： Thomas G. Wakeman
IPC分类号： F02C7/18 , F28D21/00
CPC分类号： F02C7/185 , F28D21/0014 , F28D2021/0021 , Y02T50/675
摘要： A structurally compact air-to-air heat exchanger, for a gas turbine engine of the fan bypass type, that permits a lower percentage of cooling air, than is presently needed in the art, to cool effectively the hot turbine, and its parts, of the engine. This goal is achieved, in part, by using a portion of the cool flow of fan air as a heat sink, without disturbing the flow of the fan air stream. The heat exchanger is disposed internal of the engine, and, it includes a plurality of flow tubes through which flows the hot cooling air, with the flow tubes positioned in a crossflow relationship with and to a portion of the cool flow of fan air. Three (3) variations of the preferred embodiment of the heat exchanger also are taught.
摘要翻译：用于风扇旁路式燃气涡轮发动机的结构紧凑的空气 - 空气热交换器，其允许比本领域目前需要的更低的冷却空气百分比来有效地冷却热涡轮机及其部件，的发动机。该目标部分地通过使用一部分冷却风扇的风扇作为散热器，而不会干扰风扇空气流的流动。热交换器设置在发动机的内部，并且其包括多个流管，流动管通过该多个流管与流动的管道以与风扇空气的冷却流的一部分交叉流动的关系流动。还教导了热交换器的优选实施例的三（3）变型。

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