专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

WO2005016748A2 DUAL ACTION INLET DOOR AND METHOD FOR USE THEREOF 审中-公开
标题翻译：双作用入口门及其使用方法
公开(公告)号：WO2005016748A2
公开(公告)日：2005-02-24
申请号：PCT/US2004/023220
申请日：2004-07-19
申请人： HONEYWELL INTERNATIONAL, INC. , HEIN, Jeffrey, M. , BROWN, Daniel , SELLAHEWA RAVISHA, Pramod , PEDUCHI, Andrew, Stephen , HIGUERA, Benjamen, Kurt , COWANS, Ora, Morency , LAM, Cecilia, S. , SHEORAN, Yogendra, Y. , WILLIAMS, Nicholas, A.
发明人： HEIN, Jeffrey, M. , BROWN, Daniel , SELLAHEWA RAVISHA, Pramod , PEDUCHI, Andrew, Stephen , HIGUERA, Benjamen, Kurt , COWANS, Ora, Morency , LAM, Cecilia, S. , SHEORAN, Yogendra, Y. , WILLIAMS, Nicholas, A.
IPC分类号： B64D
CPC分类号： F02C7/04 , B64D33/02 , B64D41/00 , B64D2033/0213 , B64D2041/002 , F02C7/045 , F02C7/32 , F05D2220/50 , F05D2260/96
摘要： An inlet door assembly and method for reducing noise from an auxiliary power unit (APU) contained within an aircraft housing is provided. The inlet assembly includes an inlet duct, an and a door. The inlet duct is configured to extend from the auxiliary power unit to the aircraft housing and has a sidewall that defines a flow passage through which APU noise propagates. The actuator is disposed at least partially within the inlet duct. The door coupled to the actuator. The actuator is also configured to selectively rotate the door between at least a first position, in which at least a portion of the door deflects APU noise in a first direction, and a second position, in which at least a portion of the door deflects the APU noise in a second direction.
摘要翻译：提供了一种用于降低包含在飞行器壳体内的辅助动力单元（APU）的噪声的入口门组件和方法。入口组件包括入口管道和门。入口管道被构造成从辅助动力单元延伸到飞行器壳体并且具有限定APU噪声通过其传播的流动通道的侧壁。致动器至少部分地设置在入口管道内。门连接到执行机构。致动器还构造成在至少第一位置之间选择性地旋转门，其中门的至少一部分在第一方向上偏转APU噪声和第二位置，其中门的至少一部分偏转 APU噪声在第二个方向。

2. 发明申请

WO2006034462A2 QUIET CHEVRON/TAB EXHAUST EDUCTOR SYSTEM 审中-公开
标题翻译： QUIET CHEVRON / TAB排气教育系统
公开(公告)号：WO2006034462A2
公开(公告)日：2006-03-30
申请号：PCT/US2005/034194
申请日：2005-09-23
申请人： HONEYWELL INTERNATIONAL INC. , SHEORAN, Yogendra, Y. , JUDD, Zedic, D. , BROWN, Daniel, V.
发明人： SHEORAN, Yogendra, Y. , JUDD, Zedic, D. , BROWN, Daniel, V.
CPC分类号： F02K1/48 , B64D41/00 , B64D2041/002 , F02K1/386 , F05D2220/50 , F05D2260/601 , Y02T50/671
摘要： The present invention provides a means for inducing (educting) a "passive" secondary flow stream (122) using an exhaust eductor system (110) including a primary exhaust nozzle (112) designed to transport an active flow stream (120) and a plurality of tabs (118) extending from a rear perimeter of the primary exhaust nozzle (112). Each of the tabs (118) is designed to be bent at an angle in relation to the primary exhaust nozzle (112). An exhaust mixing duct (114) is positioned around the primary exhaust nozzle (112) that is designed to transport a passive flow stream (122) to the active flow stream (120) where the plurality of tabs (118) create a streamwise vorticity to enhance the mixing of the active flow stream (120) and the passive flow stream (122).
摘要翻译：本发明提供了一种用于使用排气喷射器系统（110）诱导（排出）“无源”二次流（122）的装置，该排气喷射器系统（110）包括设计成输送主动流体流（120）和多个从主排气喷嘴（112）的后周边延伸的突片（118）。每个突片（118）设计成相对于主排气喷嘴（112）以一定角度弯曲。排气混合管道（114）围绕主排气喷嘴（112）定位，其被设计成将被动流动流（122）输送到主动流动流（120），其中多个翼片（118）产生流向涡度增强主流流（120）和被动流流（122）的混合。

3. 发明申请

WO2002074621A1 PLENUM ENTRY BULK SWIRL GENERATOR 审中-公开
标题翻译： PLENUM进入大容量SWIRL发电机
公开(公告)号：WO2002074621A1
公开(公告)日：2002-09-26
申请号：PCT/US2002/008031
申请日：2002-03-14
申请人： HONEYWELL INTERNATIONAL INC.
发明人： SHEORAN, Yogendra, Y. , BOULDIN, Bruce, D.
IPC分类号： B64D41/00
CPC分类号： B64D41/00 , B64D33/02 , B64D2033/0213 , F02C7/04 , F05D2220/50 , F15D1/04
摘要： A swirl generator for creating bulk swirl in a compressor plenum (22) in the opposite direction to the direction of rotation of the compressor rotor (12). The generator includes a continuous flow pasageway formed by an inlet duct (40) and a compressor (12) forming an angle in the range of about 0°-180° to one another. A non-uniform velocity gradient (30) forming an angle in the range of about 0°-180° to one another. A non-uniform velocity gradient (30) is created by forming an area of non-uniform cross-sectional area within the flow passageway. The non-uniform area may comprise a ramp with a tapered end line, a rounded line of intersection, a fillet or by lengthening one side wall of the inlet duct relative to the opposite side wall. Preferably, the non-uniform cross sectional area uniformly tapers from ones sidewall of the flow passageway to the opposite sidewall.
摘要翻译：一种涡旋发生器，用于在与压缩机转子（12）的旋转方向相反的方向上在压缩机室（22）中产生大量涡流。发电机包括由入口管道（40）和形成在约0°-180°范围内的角度的压缩机（12）形成的连续流动通道。不均匀的速度梯度（30）形成在约0°-180°范围内的角度。通过在流动通道内形成不均匀的横截面积的区域来产生非均匀的速度梯度（30）。不均匀区域可以包括具有锥形端线，圆角线，圆角或通过相对于相对侧壁延长入口管道的一个侧壁的斜面。优选地，不均匀的横截面积从流动通道的侧壁到相对的侧壁均匀地逐渐变细。

4. 发明申请

WO2002079631A1 TORTUOUS PATH EXHAUST EDUCTOR SYSTEM 审中-公开
标题翻译： TORTUOUS路径排气教育系统
公开(公告)号：WO2002079631A1
公开(公告)日：2002-10-10
申请号：PCT/US2002/009387
申请日：2002-03-26
申请人： HONEYWELL INTERNATIONAL INC.
发明人： SHEORAN, Yogendra, Y. , EDMONDS, David, H. , BROWN, Daniel, V.
IPC分类号： F02K1/82
CPC分类号： B64D33/06 , B64D41/00 , B64D2041/002 , F02C7/14 , F02K1/36 , F02K1/827 , F05D2220/50 , F05D2250/314 , F05D2260/601 , F05D2260/96 , Y02T50/44 , Y02T50/671 , Y02T50/675
摘要： A tortuous path quiet exhaust eductor system may be mounted to a gas turbine engine, such as commercial aircraft APU. The system includes an oil cooler, eductor primary nozzle, oil cooler nozzle, and surge air dump nozzle. The primary nozzle, oil cooler air nozzle, and surge air dump nozzle direct exhaust flow to entrain APU compartment cooling air, oil cooling air and surge air in a direction having both radial and axial components with respect to the APU centerline axis. The exhaust flow is directed into an eductor mixing duct angled away from the centerline axis and then is turned to enter an exit duct angled toward the centerline axis so that direct line of sight acoustic paths from the tail pipe exit to the turbine exit are blocked, suppressing core noise. The tail pipe ducts may be acoustically treated, further enhancing noise suppresion.
摘要翻译：曲折路径安静的排气喷射器系统可以安装在诸如商用飞机APU的燃气涡轮发动机上。该系统包括油冷却器，喷射器主喷嘴，油冷却器喷嘴和浪涌空气倾倒喷嘴。主喷嘴，油冷却器空气喷嘴和浪涌空气倾倒喷嘴直接排出流动，以相对于APU中心线轴线沿径向和轴向分量的方向夹带APU室冷却空气，油冷却空气和浪涌空气。排气流被引导到远离中心线轴线成角度的喷射器混合管道中，然后被转动以进入朝向中心线轴线成角度的出口管道，使得从尾管出口到涡轮机出口的直接视线声学路径被阻挡，抑制核心噪声。尾管可以进行声学处理，进一步增强噪音抑制。

5. 发明授权

EP1646560B1 DUAL ACTION INLET DOOR AND METHOD FOR USE THEREOF 有权
标题翻译：双效进气门及其使用方法
公开(公告)号：EP1646560B1
公开(公告)日：2007-03-07
申请号：EP04786085.3
申请日：2004-07-19
申请人： Honeywell International Inc.
发明人： HEIN, Jeffrey, M. , BROWN, Daniel , SELLAHEWA RAVISHA, Pramod , PEDUCHI, Andrew, Stephen , HIGUERA, Benjamen, Kurt , COWANS, Ora, Morency , LAM, Cecilia, S. , SHEORAN, Yogendra, Y. , WILLIAMS, Nicholas, A.
IPC分类号： B64D1/00
CPC分类号： F02C7/04 , B64D33/02 , B64D41/00 , B64D2033/0213 , B64D2041/002 , F02C7/045 , F02C7/32 , F05D2220/50 , F05D2260/96
摘要： An inlet door assembly and method for reducing noise from an auxiliary power unit (APU) (10) contained within an aircraft housing (12) is provided. The inlet assembly includes an inlet duct (21), an actuator (46) and a door (44). The inlet duct (21) is configured to extend from the auxiliary power unit (10) to the aircraft housing (12) and has a sidewall (38) that defines a flow passage (40) through which APU noise propagates. The actuator (46) is disposed at least partially within the inlet duct (21). The door (44) coupled to the actuator (46). The actuator (46) is also configured to selectively rotate the door (44) between at least a first position, in which at least a portion of the door (44) deflects APU noise in a first direction, and a second position, in which at least a portion of the door (44) deflects the APU noise in a second direction.

6. 发明公开

EP1797311A2 QUIET CHEVRON/TAB EXHAUST EDUCTOR SYSTEM 有权
标题翻译：安静的CHEVRON / TAB排气喷雾系统
公开(公告)号：EP1797311A2
公开(公告)日：2007-06-20
申请号：EP05817301.4
申请日：2005-09-23
申请人： Honeywell International, Inc.
发明人： SHEORAN, Yogendra, Y. , JUDD, Zedic, D. , BROWN, Daniel, V.
IPC分类号： F02K1/82 , F02K1/38 , F02K1/36 , B64D33/04
CPC分类号： F02K1/48 , B64D41/00 , B64D2041/002 , F02K1/386 , F05D2220/50 , F05D2260/601 , Y02T50/671
摘要： The present invention provides a means for inducing (educting) a 'passive' secondary flow stream (122) using an exhaust eductor system (110) including a primary exhaust nozzle (112) designed to transport an active flow stream (120) and a plurality of tabs (118) extending from a rear perimeter of the primary exhaust nozzle (112). Each of the tabs (118) is designed to be bent at an angle in relation to the primary exhaust nozzle (112). An exhaust mixing duct (114) is positioned around the primary exhaust nozzle (112) that is designed to transport a passive flow stream (122) to the active flow stream (120) where the plurality of tabs (118) create a streamwise vorticity to enhance the mixing of the active flow stream (120) and the passive flow stream (122).
摘要翻译：本发明提供了一种用于使用排气喷射器系统（110）来诱导（导出）“被动”二次流动流（122）的装置，所述排气喷射器系统包括设计成输送活动流动流（120）的主排气喷嘴（112）从主排气喷嘴（112）的后周边延伸的接片（118）。每个接片（118）被设计成相对于主排气喷嘴（112）以一定角度弯曲。围绕主排气喷嘴（112）设置排气混合管道（114），所述排气混合管道被设计为将被动流动流（122）输送到主动流动流（120），其中多个翼片（118）产生流动涡旋至增强活性流动流（120）和被动流动流（122）的混合。

7. 发明授权

EP1368228B1 PLENUM ENTRY BULK SWIRL GENERATOR 有权
标题翻译：室入口MASSENWIRBELUNGSGENERATOR
公开(公告)号：EP1368228B1
公开(公告)日：2005-07-27
申请号：EP02721438.6
申请日：2002-03-14
申请人： Honeywell International Inc.
发明人： SHEORAN, Yogendra, Y. , BOULDIN, Bruce, D.
IPC分类号： B64D41/00 , B64D33/02 , F02C7/04 , F15D1/04
CPC分类号： B64D41/00 , B64D33/02 , B64D2033/0213 , F02C7/04 , F05D2220/50 , F15D1/04
摘要： A swirl generator for creating bulk swirl in a compressor plenum (22) in the opposite direction to the direction of rotation of the compressor rotor (12). The generator includes a continuous flow pasageway formed by an inlet duct (40) and a compressor (12) forming an angle in the range of about 0°-180° to one another. A non-uniform velocity gradient (30) forming an angle in the range of about 0°-180° to one another. A non-uniform velocity gradient (30) is created by forming an area of non-uniform cross-sectional area within the flow passageway. The non-uniform area may comprise a ramp with a tapered end line, a rounded line of intersection, a fillet or by lengthening one side wall of the inlet duct relative to the opposite side wall. Preferably, the non-uniform cross sectional area uniformly tapers from ones sidewall of the flow passageway to the opposite sidewall.

8. 发明授权

EP1257468B1 INLET VORTEX BUSTOR AND ICE PROTECTOR FOR AUXILIARY POWER UNITS 失效
标题翻译：进气口和涡流DÄMPFER防冰辅助发动机
公开(公告)号：EP1257468B1
公开(公告)日：2004-12-08
申请号：EP01911137.6
申请日：2001-02-21
申请人： Honeywell International Inc.
发明人： SHEORAN, Yogendra, Y.
IPC分类号： B64D33/02
CPC分类号： F02C3/32 , B64D33/02 , B64D41/00 , B64D2033/0213 , B64D2041/002 , F05D2220/40 , F05D2260/601
摘要： An air inlet assembly for bringing air to an auxiliary power unit (10) mounted in the APU compartment (12) of an aircraft (14). The assembly includes a duct (30) extending from an intake (32) contoured to conform to the aircraft fuselage (16) to an exit coupled to the inlet plenum of the auxiliary power unit. A first door (33) hingeably mounted to the aft side of said intake and moveable from an open position to a closed position where said first door lies flush against intake, said first door having a closing wall (90) and two side walls (92,94) and a deflector (100,200) mounted to the forward end of said intake, said deflector having a plate (102,202) with two inwardly extending walls (104,106,204,206), each of said inwardly extending walls hinged to one of said side walls so that the second door rotates with said first door. During ground operation air that would have swirled around the side walls of the first door thus generating inlet corner vortices are now blocked by the side walls of the deflector.

9. 发明授权

EP1797311B1 QUIET CHEVRON/TAB EXHAUST EDUCTOR SYSTEM 有权
标题翻译： SILENT CHEVRON / TAB ABFALLEDUKTORSYSTEM
公开(公告)号：EP1797311B1
公开(公告)日：2008-12-24
申请号：EP05817301.4
申请日：2005-09-23
申请人： Honeywell International Inc.
发明人： SHEORAN, Yogendra, Y. , JUDD, Zedic, D. , BROWN, Daniel, V.
IPC分类号： F02K1/82 , F02K1/38 , F02K1/36 , B64D33/04
CPC分类号： F02K1/48 , B64D41/00 , B64D2041/002 , F02K1/386 , F05D2220/50 , F05D2260/601 , Y02T50/671
摘要： The present invention provides a means for inducing (educting) a 'passive' secondary flow stream (122) using an exhaust eductor system (110) including a primary exhaust nozzle (112) designed to transport an active flow stream (120) and a plurality of tabs (118) extending from a rear perimeter of the primary exhaust nozzle (112). Each of the tabs (118) is designed to be bent at an angle in relation to the primary exhaust nozzle (112). An exhaust mixing duct (114) is positioned around the primary exhaust nozzle (112) that is designed to transport a passive flow stream (122) to the active flow stream (120) where the plurality of tabs (118) create a streamwise vorticity to enhance the mixing of the active flow stream (120) and the passive flow stream (122).

10. 发明公开

EP1368228A1 PLENUM ENTRY BULK SWIRL GENERATOR 有权
标题翻译：入口散装涡旋发生器
公开(公告)号：EP1368228A1
公开(公告)日：2003-12-10
申请号：EP02721438.6
申请日：2002-03-14
申请人： Honeywell International Inc.
发明人： SHEORAN, Yogendra, Y. , BOULDIN, Bruce, D.
IPC分类号： B64D41/00 , B64D33/02 , F02C7/04 , F15D1/04
CPC分类号： B64D41/00 , B64D33/02 , B64D2033/0213 , F02C7/04 , F05D2220/50 , F15D1/04
摘要： A swirl generator for creating bulk swirl in a compressor plenum (22) in the opposite direction to the direction of rotation of the compressor rotor (12). The generator includes a continuous flow pasageway formed by an inlet duct (40) and a compressor (12) forming an angle in the range of about 0°-180° to one another. A non-uniform velocity gradient (30) forming an angle in the range of about 0°-180° to one another. A non-uniform velocity gradient (30) is created by forming an area of non-uniform cross-sectional area within the flow passageway. The non-uniform area may comprise a ramp with a tapered end line, a rounded line of intersection, a fillet or by lengthening one side wall of the inlet duct relative to the opposite side wall. Preferably, the non-uniform cross sectional area uniformly tapers from ones sidewall of the flow passageway to the opposite sidewall.
摘要翻译：一种涡旋发生器，用于在与压缩机转子（12）的旋转方向相反的方向上在压缩机增压室（22）中产生大量涡流。发电机包括由进口管道（40）和压缩机（12）形成的连续流动的通道，该进口通道与压缩机（12）形成彼此处于约0°至180°范围内的角度。一个非均匀的速度梯度（30）形成一个彼此相差约0°-180°的角度。通过在流动通道内形成不均匀的横截面积的区域来产生不均匀的速度梯度（30）。非均匀区域可以包括具有锥形端线，圆形交线，斜角或通过相对于相对侧壁延长入口管道的一个侧壁的斜坡。优选地，不均匀横截面从流动通道的侧壁到相对侧壁均匀地渐缩。

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