公开(公告)号：US08714918B2

公开(公告)日：2014-05-06

申请号：US13177151

申请日：2011-07-06

申请人： Ian Tibbott ,  Peter Ireland ,  Anthony J Rawlinson ,  Lynne H Turner

发明人： Ian Tibbott ,  Peter Ireland ,  Anthony J Rawlinson ,  Lynne H Turner

IPC分类号： F01D11/10

CPC分类号： F01D11/08 ,  F01D11/10 ,  F01D11/24 ,  F01D25/12 ,  F05D2240/11 ,  F05D2250/313 ,  F05D2250/314 ,  F05D2260/202 ,  Y02T50/676 ,  Y10T29/49323

摘要： A shroud segment for a turbine stage of a gas turbine engine forms an endwall for the working gas annulus of the stage. The segment also provides a close clearance to the tips of a row of turbine blades which sweep across the segment. In use a leakage flow of the working gas passes through the clearance gap between the blade tips and the segment. The segment has a plurality of cooling holes and respective air feed passages for the cooling holes. The cooling holes are distributed over that part of the gas-washed surface of the segment which is swept by the blade tips. The cooling holes deliver, in use, cooling air which spreads over the gas-washed surface. The feed passages are configured such that the delivered air opposes the leakage flow of the working gas.

摘要翻译： 用于燃气涡轮发动机的涡轮级的护罩段形成用于工作台的工作气体环的端壁。 该段还提供了跨越段的一排涡轮机叶片的尖端的紧密间隙。 在使用中，工作气体的泄漏流通过叶片尖端和段之间的间隙。 该段具有用于冷却孔的多个冷却孔和各自的空气供给通道。 冷却孔分布在由叶片尖端扫过的段的气体洗涤表面的那部分上。 冷却孔在使用中提供散布在气洗表面上的冷却空气。 供给通道构造成使得所输送的空气与工作气体的泄漏流相反。

公开(公告)号：US09068472B2

公开(公告)日：2015-06-30

申请号：US13368718

申请日：2012-02-08

申请人： Anthony J. Rawlinson ,  Peter Ireland ,  Lynne H. Turner ,  Ian Tibbott

发明人： Anthony J. Rawlinson ,  Peter Ireland ,  Lynne H. Turner ,  Ian Tibbott

IPC分类号： F01D5/18 ,  F01D9/06 ,  F01D11/08 ,  F01D25/12 ,  F01D11/12

CPC分类号： F01D25/12 ,  F01D5/186 ,  F01D5/187 ,  F01D9/06 ,  F01D11/08 ,  F01D11/122 ,  F05D2240/11 ,  F05D2240/81 ,  F05D2260/20 ,  F05D2260/202

摘要： A component of a turbine stage of a gas turbine engine is provided, the component forming an endwall for the working gas annulus of the stage. The component has one or more internal plena behind the endwall which, in use, contain a flow of cooling air. The component further has a plurality of exhaust holes in the endwall. The holes connect the plena to a gas-washed surface of the endwall such that the cooling air effuses through the holes to form a cooling film over the gas-washed surface. Each exhaust hole has a flow cross-sectional area which is greater at an intermediate position between the entrance of the hole from the respective plenum and the exit of the hole to the gas-washed surface than it is at said exit.

摘要翻译： 提供了一种燃气涡轮发动机的涡轮级的部件，该部件形成了用于工作台的工作气体环的端壁。 该组件在端壁后面具有一个或多个内部斑点，其在使用中包含冷却空气流。 该部件还在端壁中具有多个排气孔。 这些孔将绦虫连接到端壁的气体洗涤表面，使得冷却空气通过孔流出，以在气洗表面上形成冷却膜。 每个排气孔的流动横截面面积在从相应的压力室的孔的入口与孔的出口到气体洗涤表面之间的中间位置处比在所述出口处更大。

公开(公告)号：US20140050581A1

公开(公告)日：2014-02-20

申请号：US13940241

申请日：2013-07-11

申请人： Peter Ireland

发明人： Peter Ireland

IPC分类号： F01D5/28

CPC分类号： F01D5/286 ,  B64C3/26 ,  B64C11/205 ,  B64C27/473 ,  F03D1/0675 ,  Y02E10/721 ,  Y02T50/673

摘要： An erosion protection system and method applicable to foils or aerodynamic surfaces. Single element erosion protective elements having joggles are provided, each single element being alignable with the next to provide a contiguous erosion protection layer.

摘要翻译： 适用于箔片或空气动力学表面的侵蚀保护系统和方法。 提供具有滑块的单元侵蚀保护元件，每个单个元件可与下一个元件对准，以提供连续的侵蚀保护层。

公开(公告)号：US20070010947A1

公开(公告)日：2007-01-11

申请号：US11176042

申请日：2005-07-07

申请人： Peter Ireland ,  James Thornton ,  Gregory Wibben ,  Kamran Waheed ,  Stephen Reski

发明人： Peter Ireland ,  James Thornton ,  Gregory Wibben ,  Kamran Waheed ,  Stephen Reski

IPC分类号： G01V1/40

CPC分类号： G01V1/40

摘要： Techniques for generating deliverable files from well logging data include obtaining the well logging data, wherein the well logging data is associated with a unique identifier; outputting a graphical deliverable file based on the well logging data, one or more templates, and a set of graphical deliverable attributes that specify how the graphical deliverable file is to be generated; and outputting an electronic data file comprising the set of graphical deliverable attributes such that the graphical deliverable file can be regenerated from the electronic data file. The well logging data may include all information necessary to recalculate the computed outputs from the raw data (e.g., computational parameters). Other methods include techniques for uniquely associating data and for making the outputs tamper-proof so that a user can compare two different types of outputs (e.g., digital and graphical deliverables) and be confident whether they are from the same source data.

摘要翻译： 从测井数据生成可交付文件的技术包括获得测井数据，其中测井数据与唯一标识符相关联; 基于测井数据，一个或多个模板以及指定如何生成图形可交付文件的一组图形可交付属性输出图形可交付文件; 以及输出包括所述一组图形可交付属性的电子数据文件，使得可以从电子数据文件再生图形可交付文件。 测井数据可以包括从原始数据重新计算计算的输出所需的所有信息（例如，计算参数）。 其他方法包括用于唯一地关联数据和使输出防篡改的技术，使得用户可以比较两种不同类型的输出（例如，数字和图形可交付物），并且确定它们是否来自相同的源数据。

公开(公告)号：US20170137116A1

公开(公告)日：2017-05-18

申请号：US15319807

申请日：2014-06-24

申请人： Peter Ireland ,  Anthony Ireland

发明人： Peter Ireland ,  Anthony Ireland

IPC分类号： B64C23/06 ,  B64C21/10 ,  F04D29/32 ,  F01D9/02 ,  F23R3/00 ,  F04D27/00 ,  F01D5/14 ,  B64F5/60 ,  F04D29/54

CPC分类号： B64C23/06 ,  B64C21/10 ,  B64C2230/26 ,  F01D5/145 ,  F01D5/147 ,  F04D29/324 ,  F04D29/542 ,  F04D29/681 ,  F05D2240/127 ,  F05D2250/182 ,  F05D2250/183 ,  F15D1/003 ,  F15D1/12 ,  F23R3/002 ,  Y02T50/162 ,  Y02T50/166 ,  Y02T50/672 ,  Y02T50/673

摘要： Methods and related apparatus embodiments are disclosed that allow novel Conformal Vortex Generator and/or Elastomeric Vortex Generator art to improve energy efficiency and control capabilities at many surface points of a body or object moving at speed in aero/hydrodynamic Newtonian fluids, by reducing; shock energy losses, surface flow turbulence, and/or momentum layer thicknesses.

公开(公告)号：US20160357182A1

公开(公告)日：2016-12-08

申请号：US15175030

申请日：2016-06-06

申请人： Peter Ireland

发明人： Peter Ireland

IPC分类号： G05D1/00 ,  B64D43/02

CPC分类号： G05D1/0005 ,  B64D43/02

摘要： An aircraft planning control system and method. According to one embodiment, a flight management computer and remote server system are communicably coupled to a plurality of sensors, the plurality of sensors recording data associated with an aircraft in operation. The data is used by the remote server system and flight management computer to generate real-time performance data for the aircraft, and to optimize a speed schedule for the aircraft.

摘要翻译： 飞机规划控制系统及方法。 根据一个实施例，飞行管理计算机和远程服务器系统可通信地耦合到多个传感器，所述多个传感器记录与正在运行的飞行器相关联的数据。 数据由远程服务器系统和飞行管理计算机用于生成飞机的实时性能数据，并优化飞机的速度计划。

公开(公告)号：US08721271B2

公开(公告)日：2014-05-13

申请号：US12956501

申请日：2010-11-30

申请人： Yi Wang ,  Miles T Trumper ,  Mark J Wilson ,  Peter Ireland ,  Robert C Chambers

发明人： Yi Wang ,  Miles T Trumper ,  Mark J Wilson ,  Peter Ireland ,  Robert C Chambers

IPC分类号： F01D5/08

CPC分类号： F01D25/12 ,  F01D25/18 ,  F02C7/14 ,  F02C7/18 ,  F02K3/115 ,  F05D2260/22141

摘要： An air-cooled oil cooler for the wall of an air flow passage of a gas turbine engine is provided, the oil cooler allowing improved heat exchange performance to be obtained. This is achieved by: (I) diverting air flow from the inner side of the oil cooler towards the outer side of the oil cooler, (ii) enhancing heat exchange performance at the leading edge of the cooler, and/or (iii) suppressing airflow wake at the trailing edge of the cooler.

摘要翻译： 提供了一种用于燃气涡轮发动机的空气流动通道的壁的风冷式油冷却器，能够获得改善的热交换性能的油冷却器。 这通过以下方式实现：（I）将空气流从油冷却器的内侧转向油冷却器的外侧，（ii）提高冷却器前缘处的热交换性能，和/或（iii）抑制 气流在冷却器的后缘处醒来。

公开(公告)号：US20110008174A1

公开(公告)日：2011-01-13

申请号：US12832966

申请日：2010-07-08

申请人： Peter Ireland

发明人： Peter Ireland

IPC分类号： F04D29/38

CPC分类号： B64C23/06 ,  B64C23/065 ,  B64C2003/147 ,  Y02T50/12 ,  Y02T50/162 ,  Y02T50/164

摘要： A method of improving aerodynamic performance of foils by the application of conformal, elastomeric vortex generators. The novel use of elastomers allows the application of various forms of vortex generators to sections that have been problematic from engineering and cost considerations. A novel and efficient vortex generator profile is identified, which develops an additional co rotating vortex at low energy expenditure. The mechanisms allow for the application of transverse vortex generators, or Gurney Flaps/Lift Enhancement Tabs/Divergent Trailing Edges, to propellers, rotorblades, and to wings/flaps/control trailing edges. Cove Tabs are additionally described using an elastomeric transverse vortex generator to achieve performance improvements of a high lift device.

摘要翻译： 通过应用保形弹性涡流发生器来改善箔的空气动力学性能的方法。 弹性体的新颖使用允许将各种形式的涡流发生器应用于从工程和成本考虑问题的部分。 确定了一种新颖有效的涡流发生器轮廓，其在低能量消耗下产生额外的共旋转涡流。 这些机构允许将横向涡流发生器或Gurney襟翼/升力增强翼片/发散尾翼边缘应用于螺旋桨，转子叶片以及翼/翼/控制后缘。 使用弹性体横向涡流发生器另外描述了小翼片，以实现高提升装置的性能改进。

公开(公告)号：US20050074325A1

公开(公告)日：2005-04-07

申请号：US10946105

申请日：2004-09-22

申请人： Andrew Chambers ,  Geoffrey Dailey ,  David Gillespie ,  Peter Ireland

发明人： Andrew Chambers ,  Geoffrey Dailey ,  David Gillespie ,  Peter Ireland

IPC分类号： F01D5/08 ,  F01D5/18 ,  F01D25/12 ,  F02C7/12 ,  F28D7/02

CPC分类号： F01D5/18 ,  F05D2260/201 ,  F05D2260/221 ,  F23R3/04 ,  F23R2900/03041 ,  F23R2900/03042 ,  F23R2900/03044

摘要： Cooling jets 1 are provided with a longitudinal aspect 2 greater than width 3. Thus, the coolant flow through the jet 1 is less susceptible to deflection by lateral or cross flows presented to that coolant flow such that cooling by impingement of the coolant flow upon a surface 7 to be cooled is improved. Typically, a plurality of jets 1 are provided in a housing wall 8. These jets 1 will be arranged in an appropriate pattern to achieve cooling by flow impingement upon the surface 7 to be cooled. Possibly, a plurality of jets 1 in an appropriate pattern may be arranged upstream of conventional circular coolant jets in order to provide some protection for those circular coolant jets from lateral or cross flow.

摘要翻译： 冷却喷嘴1设置有大于宽度3的纵向方面2.因此，流过喷嘴1的冷却剂流不易受到呈现给该冷却剂流的横向或横向流动的偏转，使得冷却剂的冷却剂流动到 要冷却的表面7得到改善。 通常，多个喷射器1设置在壳体壁8中。这些喷射器1将被布置成适当的图案，以通过流动冲击来冷却待冷却的表面7上的冷却。 可能地，可以将多个适当图案的喷嘴1布置在传统的圆形冷却剂喷流的上游，以便为这些圆形冷却剂喷嘴提供一些保护以防止横向或横向流动。

公开(公告)号：US08861015B2

公开(公告)日：2014-10-14

申请号：US11963288

申请日：2007-12-21

申请人： Peter Ireland

发明人： Peter Ireland

IPC分类号： G06K15/00 ,  G06F3/12 ,  G06F17/21

CPC分类号： G06F3/1285 ,  G06F3/1208 ,  G06F3/1242 ,  G06F3/125 ,  G06F17/211

摘要： An approach that prepares an electronic document of continuous information for document exchange that simultaneously supports continuous and page-by-page printing is described. In one embodiment, there is an electronic document generator tool for document exchange that includes an input component configured to receive input with respect to preparing the electronic document of continuous information for continuous and page-by-page printing. The input comprises an indication to represent the electronic document of continuous information in a page-based file format for document exchange and an indication of target page sizes with respective unprintable margins that are desired for printing the electronic document of continuous information. A printable area customization component is configured to customize the electronic document of continuous information into a page-by-page electronic document that is suitable for both continuous and page-by-page printing without loss of information, scale changes and/or gaps of continuity. The printable area customization component is configured to determine a custom page size that represents the continuous information and prints to the target page sizes without loss of information, scale changes and/or gaps of continuity.

摘要翻译： 描述了一种准备用于文档交换的连续信息的电子文档的方法，该文档交换同时支持连续和逐页打印。 在一个实施例中，存在用于文件交换的电子文档生成工具，其包括被配置为接收关于准备用于连续和逐页打印的连续信息的电子文档的输入的输入部件。 输入包括用于表示用于文档交换的基于页面的文件格式的连续信息的电子文档的指示以及用于打印连续信息的电子文档所需的各自不可打印边距的目标页面大小的指示。 可打印区域定制组件被配置为将连续信息的电子文档定制成逐页电子文档，其适合于连续和逐页打印，而不会丢失信息，缩放变化和/或连续性差距 。 可打印区域定制组件被配置为确定表示连续信息的自定义页面大小，并打印到目标页面大小，而不会丢失信息，缩放更改和/或连续性间隔。