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1. 发明授权

US08826637B2 Arrangement for the discharge of oil-venting air on a gas-turbine engine 有权
标题翻译：用于在燃气涡轮发动机上排放排油空气的布置
公开(公告)号：US08826637B2
公开(公告)日：2014-09-09
申请号：US12973114
申请日：2010-12-20
申请人： Robert Thies
发明人： Robert Thies
IPC分类号： F01D11/00 , F04D29/06 , F16J15/00 , F01D25/18 , F01D25/22 , F02C7/28 , F02K1/78 , F01D25/00 , F02C7/06 , F01M13/04
CPC分类号： F02C7/06 , F01D25/002 , F01D25/18 , F01M2013/0433 , F05D2260/607 , Y02T50/675
摘要： In an arrangement for discharging oil-venting air (oil air) separated by a lubricating oil de-aeration system, kinetic energy of the oil-venting air (O) is increased to a static pressure which exceeds the exhaust-gas flow (A) pressure by a diffuser and the oil-venting air is then mixed with the exhaust-gas flow and discharged with the latter. The venting line (10) coming from the lubricating oil de-aeration system issues into a diffuser (13) which is integrated into the exhaust cone (9) enveloped by the exhaust-gas flow of the engine and whose oil-air outlet opening (14) is connected to the exhaust-gas flow either directly or via an attenuation chamber (18) provided in the exhaust cone. Provision is such made for discharging oil air from the engine to the atmosphere without contaminating visible engine parts and for obtaining a weight reduction due to the reduced length of the venting line.
摘要翻译：在通过润滑油除气系统分离出的排油空气（油空气）的排出装置中，排油空气（O）的动能增加到超过排气流量（A）的静压力，然后通过扩散器施加压力，然后将排油空气与排气流混合并与其排出。来自润滑油去气系统的排气管线（10）发生到一个扩散器（13），该扩散器（13）集成到由发动机的废气流包围的排气锥体（9）中，并且其排气口 14）直接或经由设置在排气锥体中的衰减室（18）连接到废气流。这样做是为了将油空气从发动机排放到大气中而不污染可见的发动机部件，并且由于排气管线的长度减小而获得重量减轻。

2. 发明申请

US20110146223A1 ARRANGEMENT FOR THE DISCHARGE OF EXHAUST AIR SEPARATED FROM THE LUBRICATING OIL DE-AERATION SYSTEM OF A GAS-TURBINE ENGINE 有权
标题翻译：从气体涡轮发动机润滑油去除系统分离的排放空气排放的安排
公开(公告)号：US20110146223A1
公开(公告)日：2011-06-23
申请号：US12968792
申请日：2010-12-15
申请人： Robert THIES
发明人： Robert THIES
IPC分类号： F02C7/00
CPC分类号： F01D25/002 , B64C1/1453 , F01D25/18 , F01D25/30 , F01M13/021 , F02C7/06 , F05D2260/607 , F16N39/002 , Y02T50/671 , Y02T50/675
摘要： With an arrangement for the discharge of oil-contaminated exhaust air separated from the lubricating oil de-aeration system of a gas-turbine engine and led to the atmosphere via a venting line, the venting line (13) issues into an attenuation chamber (12) formed within the exhaust cone (9) of the gas-turbine engine and connected to a Venturi nozzle (14) via a discharge tube (17) for drawing off the oil-contaminated exhaust air and blowing it into the exhaust-gas flow, with the Venturi nozzle (14) being arranged in the exhaust gas-flow of the gas-turbine engine and oriented in a flow direction. The oil-contaminated exhaust air is completely discharged with the exhaust-gas flow without contacting visible engine parts.
摘要翻译：通过排出与燃气涡轮发动机的润滑油除气系统分离并经由排气管路引导到大气的排出油的废气的布置，通气管线（13）发射到衰减室（12））形成在燃气涡轮发动机的排气锥（9）内并且经由排放管（17）连接到文丘里喷嘴（14），用于抽出被油污染的废气并将其吹入排气流中，文丘里喷嘴（14）布置在燃气涡轮发动机的排气流中并沿流动方向定向。受油污染的废气与废气流完全排放而不接触可见的发动机部件。

3. 发明申请

US20120067025A1 BLOOM MIXER FOR A TURBOFAN ENGINE 有权
标题翻译：用于涡轮发动机的BLOOM混合器
公开(公告)号：US20120067025A1
公开(公告)日：2012-03-22
申请号：US13231409
申请日：2011-09-13
申请人： Robert THIES
发明人： Robert THIES
IPC分类号： F02K3/075
CPC分类号： F02K1/386 , F02K1/383 , F02K1/48 , F02K3/075 , F05D2240/126
摘要： An adjustable bloom mixer for a turbofan engine for setting a mixing ratio, adapted to the respective flight condition, between cold airflow in the bypass duct and hot airflow in the core flow duct includes an air-guiding element (13) arranged upstream of a thin-walled, corrugated part (6b) of the bloom mixer (6) for branching off a cold partial airflow and/or a hot partial airflow from the bypass duct and from the core flow duct of the engine. An air control device (14) is assigned to the air-guiding element (13) for leading the branched-off cold airflow or hot airflow along the inner surface and/or the outer surface of the bloom mixer (6) in order to deflect its corrugated part (6b) radially inwards or outwards on the basis of a temperature difference between an inner and an outer surface effected by the hot and/or cold partial airflow.
摘要翻译：一种用于涡轮风扇发动机的可调节的起重混合器，用于设置适于各个飞行状态的混合比，在旁路管道中的冷气流与芯流道中的热气流之间包括空气引导元件（13），其布置在薄的用于将冷部分空气流和/或来自旁路管道和来自发动机的核心流动管道的热部分气流分流出来的，用于分配出来的混合器（6）的壁的波纹部分（6b）。空气控制装置（14）被分配到空气引导元件（13），用于引导分流冷气流或沿着盛油混合器（6）的内表面和/或外表面的热气流，以便偏转其波纹部分（6b）基于由热和/或冷部分气流影响的内表面和外表面之间的温度差径向向内或向外径向。

4. 发明申请

US20110173990A1 INTERMEDIATE CASING FOR A GAS-TURBINE ENGINE 有权
标题翻译：气动涡轮发动机中间油箱
公开(公告)号：US20110173990A1
公开(公告)日：2011-07-21
申请号：US13009060
申请日：2011-01-19
申请人： Robert THIES
发明人： Robert THIES
IPC分类号： F02C7/20
CPC分类号： F01D25/28 , F01D25/162 , F01D25/34 , F02C7/20 , F02C7/275 , F02C7/32 , Y02T50/671
摘要： An intermediate casing for a gas-turbine engine has an outer ring (3), an inner ring (1) and an intermediate ring (2) mutually supported by mutually aligned outer and inner supporting struts (4, 5). A radial drive shaft (6), positioned through inner and outer supporting struts (4.1, 5.1) aligned at a 6-o′ clock position, connects to an auxiliary gear drive (7). Four additional outer supporting struts (5.2, 5.3, 5.4, 5.5) are spaced apart 72° . A mounting bracket connects to the outer ring at a side facing an aircraft fuselage in areas of two of the additional outer supporting struts. The arrangement of supporting struts and type of mounting bracket attachment, saves weight, improves flow in the bypass duct and increase maintenance and installation access at the bottom side of the engine to nearly 144° .
摘要翻译：用于燃气涡轮发动机的中间壳体具有由相互对准的外支撑支柱（4,5）相互支撑的外环（3），内圈（1）和中间环（2）。通过在6点钟位置对准的内部和外部支撑支柱（4.1,5.1）定位的径向驱动轴（6）连接到辅助齿轮传动装置（7）。四个额外的外支撑支柱（5.2,5.3,5.4,5.5）间隔开72°。一个安装支架在两个额外的外部支撑支柱的区域中的面向飞机机身的一侧连接到外圈。支撑支架和安装支架附件类型的布置，节省重量，改善旁路管道中的流量，并将发动机底部的维护和安装通道增加到接近144°。

5. 发明授权

US08857193B2 Intermediate casing for a gas-turbine engine 有权
标题翻译：用于燃气涡轮发动机的中间套管
公开(公告)号：US08857193B2
公开(公告)日：2014-10-14
申请号：US13009060
申请日：2011-01-19
申请人： Robert Thies
发明人： Robert Thies
IPC分类号： F02C7/20 , F02C7/32 , F01D25/28 , F01D25/34 , F01D25/16 , F02C7/275
CPC分类号： F01D25/28 , F01D25/162 , F01D25/34 , F02C7/20 , F02C7/275 , F02C7/32 , Y02T50/671
摘要： An intermediate casing for a gas-turbine engine has an outer ring (3), an inner ring (1) and an intermediate ring (2) mutually supported by mutually aligned outer and inner supporting struts (4, 5). A radial drive shaft (6), positioned through inner and outer supporting struts (4.1, 5.1) aligned at a 6-o′ clock position, connects to an auxiliary gear drive (7). Four additional outer supporting struts (5.2, 5.3, 5.4, 5.5) are spaced apart 72°. A mounting bracket connects to the outer ring at a side facing an aircraft fuselage in areas of two of the additional outer supporting struts. The arrangement of supporting struts and type of mounting bracket attachment, saves weight, improves flow in the bypass duct and increase maintenance and installation access at the bottom side of the engine to nearly 144°.
摘要翻译：用于燃气涡轮发动机的中间壳体具有由相互对准的外支撑支柱（4,5）相互支撑的外环（3），内圈（1）和中间环（2）。通过在6点钟位置对准的内部和外部支撑支柱（4.1,5.1）定位的径向驱动轴（6）连接到辅助齿轮传动装置（7）。四个额外的外支撑支柱（5.2,5.3,5.4,5.5）间隔开72°。一个安装支架在两个额外的外部支撑支柱的区域中的面向飞机机身的一侧连接到外圈。支撑支架和安装支架附件类型的布置，节省重量，改善旁路管道中的流量，并将发动机底部的维护和安装通道增加到接近144°。

6. 发明授权

US08640436B2 Arrangement for the discharge of exhaust air separated from the lubricating oil de-aeration system of a gas-turbine engine 有权
标题翻译：用于排出与燃气轮机的润滑油除气系统分离的废气的排列
公开(公告)号：US08640436B2
公开(公告)日：2014-02-04
申请号：US12968792
申请日：2010-12-15
申请人： Robert Thies
发明人： Robert Thies
IPC分类号： F02G3/00
CPC分类号： F01D25/002 , B64C1/1453 , F01D25/18 , F01D25/30 , F01M13/021 , F02C7/06 , F05D2260/607 , F16N39/002 , Y02T50/671 , Y02T50/675
摘要： With an arrangement for the discharge of oil-contaminated exhaust air separated from the lubricating oil de-aeration system of a gas-turbine engine and led to the atmosphere via a venting line, the venting line (13) issues into an attenuation chamber (12) formed within the exhaust cone (9) of the gas-turbine engine and connected to a Venturi nozzle (14) via a discharge tube (17) for drawing off the oil-contaminated exhaust air and blowing it into the exhaust-gas flow, with the Venturi nozzle (14) being arranged in the exhaust gas-flow of the gas-turbine engine and oriented in a flow direction. The oil-contaminated exhaust air is completely discharged with the exhaust-gas flow without contacting visible engine parts.
摘要翻译：通过排出与燃气涡轮发动机的润滑油除气系统分离并经由排气管路引导到大气的排出油的废气的布置，通气管线（13）发射到衰减室（12））形成在燃气涡轮发动机的排气锥（9）内并且经由排放管（17）连接到文丘里喷嘴（14），用于抽出被油污染的废气并将其吹入排气流中，文丘里喷嘴（14）布置在燃气涡轮发动机的排气流中并沿流动方向定向。受油污染的废气与废气流完全排放而不接触可见的发动机部件。

7. 发明申请

US20110146224A1 ARRANGEMENT FOR THE DISCHARGE OF OIL-VENTING AIR ON A GAS-TURBINE ENGINE 有权
标题翻译：在燃气发动机上排放空气的装置的安排
公开(公告)号：US20110146224A1
公开(公告)日：2011-06-23
申请号：US12973114
申请日：2010-12-20
申请人： Robert THIES
发明人： Robert THIES
IPC分类号： F02C7/06
CPC分类号： F02C7/06 , F01D25/002 , F01D25/18 , F01M2013/0433 , F05D2260/607 , Y02T50/675
摘要： In an arrangement for discharging oil-venting air (oil air) separated by a lubricating oil de-aeration system, kinetic energy of the oil-venting air (O) is increased to a static pressure which exceeds the exhaust-gas flow (A) pressure by a diffuser and the oil-venting air is then mixed with the exhaust-gas flow and discharged with the latter. The venting line (10) coming from the lubricating oil de-aeration system issues into a diffuser (13) which is integrated into the exhaust cone (9) enveloped by the exhaust-gas flow of the engine and whose oil-air outlet opening (14) is connected to the exhaust-gas flow either directly or via an attenuation chamber (18) provided in the exhaust cone. Provision is such made for discharging oil air from the engine to the atmosphere without contaminating visible engine parts and for obtaining a weight reduction due to the reduced length of the venting line.
摘要翻译：在通过润滑油除气系统分离出的排油空气（油空气）的排出装置中，排油空气（O）的动能增加到超过排气流量（A）的静压力，然后通过扩散器施加压力，然后将排油空气与排气流混合并与其排出。来自润滑油去气系统的排气管线（10）发生到一个扩散器（13），该扩散器（13）集成到由发动机的废气流包围的排气锥体（9）中，并且其排气口 14）直接或经由设置在排气锥体中的衰减室（18）连接到废气流。这样做是为了将油空气从发动机排放到大气中而不污染可见的发动机部件，并且由于排气管线的长度减小而获得重量减轻。

8. 发明授权

US09027323B2 Bloom mixer for a turbofan engine 有权
标题翻译：用于涡轮风扇发动机的布鲁姆搅拌机
公开(公告)号：US09027323B2
公开(公告)日：2015-05-12
申请号：US13231409
申请日：2011-09-13
申请人： Robert Thies
发明人： Robert Thies
IPC分类号： F02K1/48 , F02K1/38 , F02K3/075
CPC分类号： F02K1/386 , F02K1/383 , F02K1/48 , F02K3/075 , F05D2240/126
摘要： An adjustable bloom mixer for a turbofan engine for setting a mixing ratio, adapted to the respective flight condition, between cold airflow in the bypass duct and hot airflow in the core flow duct includes an air-guiding element (13) arranged upstream of a thin-walled, corrugated part (6b) of the bloom mixer (6) for branching off a cold partial airflow and/or a hot partial airflow from the bypass duct and from the core flow duct of the engine. An air control device (14) is assigned to the air-guiding element (13) for leading the branched-off cold airflow or hot airflow along the inner surface and/or the outer surface of the bloom mixer (6) in order to deflect its corrugated part (6b) radially inwards or outwards on the basis of a temperature difference between an inner and an outer surface effected by the hot and/or cold partial airflow.
摘要翻译：一种用于涡轮风扇发动机的可调节的起重混合器，用于设置适于各个飞行状态的混合比，在旁路管道中的冷气流与芯流道中的热气流之间包括空气引导元件（13），其布置在薄的用于将冷部分空气流和/或来自旁路管道和来自发动机的核心流动管道的热部分气流分流出来的，用于分配出来的混合器（6）的壁的波纹部分（6b）。空气控制装置（14）被分配到空气引导元件（13），用于引导分流冷气流或沿着盛油混合器（6）的内表面和/或外表面的热气流，以便偏转其波纹部分（6b）基于由热和/或冷部分气流影响的内表面和外表面之间的温度差径向向内或向外径向。

9. 发明申请

US20110116908A1 GAS TURBINE ENGINE WITH AN ARRANGEMENT FOR MEASURING THE SHAFT ROTATION SPEED 审中-公开
标题翻译：气体涡轮发动机具有用于测量轴转速的装置
公开(公告)号：US20110116908A1
公开(公告)日：2011-05-19
申请号：US12947236
申请日：2010-11-16
申请人： Robert THIES
发明人： Robert THIES
IPC分类号： F01D25/00
CPC分类号： G01P3/486 , F01D17/06 , F05D2220/36 , F05D2270/02 , F05D2270/023 , F05D2270/304
摘要： A gas turbine engine includes an arrangement for measuring shaft rotation speed, including a laser source (10) for directing a laser beam (11) onto portions of rotor blades to either be reflected from or interrupted by the rotor blades to create light impulses as a function of the rotor rotation rate. A receiver diode (12) receives the light impulses and generates voltage impulses corresponding to the rotor or shaft rotation rate. An evaluation unit associated with the receiver diode measures the number of the voltage impulses generated per unit of time and calculates therefrom the rotation speed of the engine shaft connected to the rotor. The measurement arrangement is arranged in the engine housing to be easily accessible for mounting, maintenance and adjustment, is functionally reliable under robust engine operation and can detect the rotation of a low pressure shaft and connected fan.
摘要翻译：燃气涡轮发动机包括用于测量轴转速的装置，其包括用于将激光束（11）引导到转子叶片的部分上以被转子叶片反射或被转子叶片中断的激光源（10），以产生作为转子转速的函数。接收器二极管（12）接收光脉冲并产生对应于转子或轴转速的电压脉冲。与接收二极管相关联的评估单元测量每单位时间产生的电压脉冲的数量，并从其计算连接到转子的发动机轴的转速。测量装置布置在发动机壳体中，易于安装，维护和调节，在发动机运行稳定的情况下功能可靠，可以检测低压轴和连接的风扇的旋转。

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