-
公开(公告)号：US08851853B2
公开(公告)日：2014-10-07
申请号：US13116199
申请日：2011-05-26
Applicant: Ioannis Alvanos , Gabriel L. Suciu , Christopher M. Dye , Glenn Levasseur
Inventor： Ioannis Alvanos , Gabriel L. Suciu , Christopher M. Dye , Glenn Levasseur
CPC classification number: F01D5/3046 , F01D5/225 , F01D5/282 , F01D5/284 , F05D2300/6033
Abstract: A rotor disk assembly for a gas turbine engine includes a rotor hub defined about an axis of rotation, the rotor hub includes a blade mount section with a first radial flange having a multiple of first apertures and a second radial flange with a multiple of second apertures.
Abstract translation: 用于燃气涡轮发动机的转子盘组件包括围绕旋转轴限定的转子毂，转子毂包括具有第一径向凸缘的叶片安装部分，第一径向凸缘具有多个第一孔，第二径向凸缘具有多个第二孔 。
-
42.发明授权Hybrid rotor disk assembly with a ceramic matrix composite airfoil for a gas turbine engine 有权具有用于燃气涡轮发动机的陶瓷基体复合翼型的混合转子盘组件公开(公告)号：US08834125B2
公开(公告)日：2014-09-16
申请号：US13116188
申请日：2011-05-26
Applicant: Ioannis Alvanos , Gabriel L. Suciu , Christopher M. Dye , Glenn Levasseur
Inventor： Ioannis Alvanos , Gabriel L. Suciu , Christopher M. Dye , Glenn Levasseur
CPC classification number: F01D5/3046 , C04B37/00 , C04B2235/5244 , C04B2237/365 , C04B2237/38 , C04B2237/76 , F01D5/225 , F01D5/282 , F01D5/284 , F05D2240/12 , F05D2300/6033
Abstract: A Ceramic Matrix Composite (CMC) airfoil for a gas turbine engine includes a CMC root section which extends to form a CMC airfoil section, the CMC root section defines a bore along a non-linear axis.
Abstract translation: 用于燃气涡轮发动机的陶瓷基体复合材料（CMC）翼型件包括延伸以形成CMC翼型部分的CMC根部，CMC根部沿着非线性轴线限定孔。
-
公开(公告)号：US20130287565A1
公开(公告)日：2013-10-31
申请号：US13456436
申请日：2012-04-26
Applicant: Gabriel L. Suciu , Ioannis Alvanos
Inventor： Gabriel L. Suciu , Ioannis Alvanos
IPC: F02C7/20
CPC classification number: F02C7/20 , B64D27/26 , B64D2027/264
Abstract: A mounting apparatus for a turbine exhaust case (TEC) is provided. The mounting apparatus may include a neck, support links and a plurality of fastening pins. The neck may include an upper portion that is receivable within a pylon associated with the TEC and at least one neck aperture extending therethrough. The support links may downwardly extend from a lower portion of the neck. The support links may be configured to at least partially receive a section of the TEC. Each support link may include at least one link aperture extending therethrough. The fastening pins may include at least one neck pin extending through the neck aperture and at least one link pin extending through the link aperture of each support link.
Abstract translation: 提供了一种用于涡轮机排气箱（TEC）的安装装置。 安装设备可以包括颈部，支撑连杆和多个紧固销。 颈部可以包括可接收在与TEC相关联的挂架内的上部和延伸穿过其的至少一个颈孔。 支撑连杆可以从颈部的下部向下延伸。 支持链路可以被配置为至少部分地接收TEC的一部分。 每个支撑连杆可以包括延伸穿过其中的至少一个连杆孔。 紧固销可以包括延伸穿过颈部孔的至少一个颈销和延伸穿过每个支撑连杆的连杆孔的至少一个连杆销。
-
公开(公告)号：US20130233997A1
公开(公告)日：2013-09-12
申请号：US13417606
申请日：2012-03-12
Applicant: Gabriel L. Suciu , Ioannis Alvanos , Brian D. Merry
Inventor： Gabriel L. Suciu , Ioannis Alvanos , Brian D. Merry
IPC: F16M13/00
Abstract: A mount for a turbine engine has a semi-circular yoke with a first leg and a second leg. The mount also has a stanchion with a cylindrical section attached to the yoke, and a conical section attached to the cylindrical section. A mounting bracket is attached to the conical section.
Abstract translation: 用于涡轮发动机的安装座具有带有第一腿和第二腿的半圆形轭。 安装座还具有支柱，其具有附接到轭的圆柱形部分，以及附接到圆柱形部分的锥形部分。 安装支架连接到锥形部分。
-
公开(公告)号：US20130219920A1
公开(公告)日：2013-08-29
申请号：US13405527
申请日：2012-02-27
Applicant: Gabriel L. Suciu , Ioannis Alvanos
Inventor： Gabriel L. Suciu , Ioannis Alvanos
IPC: F02C6/08
Abstract: A gas turbine engine includes a heat exchanger, a diffuser case, a passageway and a nozzle assembly. The heat exchanger exchanges heat with a bleed airflow to provide a conditioned airflow. The diffuser case includes a plenum that receives the conditioned airflow. The passageway is fluidly connected between the heat exchanger and the diffuser case, and the conditioned airflow is communicated through the passageway and into the plenum. The nozzle assembly is in fluid communication with the plenum of the diffuser case to receive the conditioned airflow from the plenum.
Abstract translation: 燃气涡轮发动机包括热交换器，扩散器壳体，通道和喷嘴组件。 热交换器与放气气流交换热量以提供调节气流。 扩散器壳体包括容纳调节气流的增压室。 通道流体地连接在热交换器和扩散器壳体之间，并且经调节的气流通过通道连通并进入通风室。 喷嘴组件与扩散器壳体的气室流体连通以接收来自气室的经调节的气流。
-
Patent Agency Ranking
公开(公告)号：US20130004314A1
公开(公告)日：2013-01-03
申请号：US13172279
申请日：2011-06-29
Applicant: Ioannis Alvanos , Gabriel L. Suciu
Inventor： Ioannis Alvanos , Gabriel L. Suciu
CPC classification number: F01D25/246 , Y10T29/49321
Abstract: A full hoop stator vane cluster includes an inner hoop and an outer hoop both being substantially cylindrical and coaxial. A plurality of airfoils extend radially between the hoops, and a plurality of vane splines extend radially outward from the outer hoop for attaching the vane cluster to a gas turbine engine.
Abstract translation: 一个完整的环形定子叶片组包括一个内圈和一个外圈，它们都是大致圆柱形和同轴的。 多个翼型件在环之间径向延伸，并且多个叶片花键从外环径向向外延伸，用于将叶片簇附接到燃气涡轮发动机。
-
公开(公告)号：US20120301315A1
公开(公告)日：2012-11-29
申请号：US13116246
申请日：2011-05-26
Applicant: Ioannis Alvanos , Gabriel L. Suciu , Douglas M. Berczik , John D. Riehl , Kevin L. Rugg
Inventor： Ioannis Alvanos , Gabriel L. Suciu , Douglas M. Berczik , John D. Riehl , Kevin L. Rugg
CPC classification number: F01D5/284 , F01D5/282 , F01D5/34 , F01D9/041 , F01D11/001 , F01D25/246 , F05D2240/12 , F05D2300/6033
Abstract: A Ceramic Matrix Composites (CMC) airfoil for a gas turbine engine includes a first multiple of CMC plies which define a suction side, a first airfoil portion of the first multiple of CMC plies at least partially parallel to an airfoil axis. A second multiple of CMC plies define a pressure side, a second airfoil portion of the second multiple of CMC plies at least partially parallel to the airfoil axis and bonded to the first airfoil portion.
Abstract translation: 用于燃气涡轮发动机的陶瓷基体复合材料（CMC）翼型件包括限定吸力侧的CMC层的第一倍数，至少部分平行于翼型轴线的CMC层的第一倍数的第一翼型部分。 CMC层的第二倍数限定了压力侧，CMC层的第二倍数的第二翼型部分至少部分地平行于翼型轴线并结合到第一翼型部分。
-
公开(公告)号：US08899924B2
公开(公告)日：2014-12-02
申请号：US13164234
申请日：2011-06-20
Applicant: Ioannis Alvanos
Inventor： Ioannis Alvanos
CPC classification number: F01D5/081 , F02C7/18 , F05D2260/30 , Y02T50/676 , Y10T29/49327
Abstract: A high pressure turbine includes a stator, a rotor, a tangential on-board injector, and a heat shield. The rotor is located downstream of the stator and the tangential on-board injector directs cooling air to the rotor. The heat shield is retained by abutment with the stator and the tangential on-board injector.
Abstract translation: 高压涡轮机包括定子，转子，切向的车载喷射器和隔热罩。 转子位于定子的下游，切向的车载喷射器将冷却空气引导到转子。 隔热板通过与定子和切向机载喷射器的邻接保持。
-
公开(公告)号：US07708520B2
公开(公告)日：2010-05-04
申请号：US11605678
申请日：2006-11-29
Applicant: Roger E. Paolillo , Ioannis Alvanos , Cheng-Zhang Wang
Inventor： Roger E. Paolillo , Ioannis Alvanos , Cheng-Zhang Wang
IPC: F01D11/02
CPC classification number: F01D11/001 , F01D11/02 , F05D2250/712
Abstract: A gas turbine engine is provided with turbine sealing structures including knife edge seals which extend at an angle relative to an axial center line of the engine. Each knife edge seal is associated with a concave pocket defined between a radially inner surface and a spaced radially outer surface. The concave pockets and their associated knife edge seals create a pair of vortices which prevent leakage into radially inner portions of the turbine section.
Abstract translation: 燃气涡轮发动机设置有涡轮机密封结构，其包括相对于发动机的轴向中心线以一定角度延伸的刀刃密封件。 每个刀刃密封件与限定在径向内表面和间隔开的径向外表面之间的凹槽相关联。 凹口袋及其相关的刀刃密封件产生一对涡流，防止泄漏到涡轮部分的径向内部。
-
公开(公告)号：US20090257877A1
公开(公告)日：2009-10-15
申请号：US12103673
申请日：2008-04-15
Applicant: Ioannis Alvanos , John J. OConnor
Inventor： Ioannis Alvanos , John J. OConnor
CPC classification number: F01D5/3007
Abstract: A rotor blade for a gas turbine engine includes an asymmetric attachment section received within a rotor disk rim with an asymmetric slot.
Abstract translation: 用于燃气涡轮发动机的转子叶片包括容纳在具有不对称槽的转子盘形边缘内的非对称附接部分。
-
-
-
-
-
-
-
-
-
Search Results
72
records
(took 0.031 seconds)
