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1.发明申请METHOD FOR PROTECTING A GAS TURBINE ENGINE AGAINST HIGH DYNAMICAL PROCESS VALUES AND GAS TURBINE ENGINE FOR CONDUCTING THE METHOD 有权用于保护气体涡轮发动机的高动态过程值和气体涡轮发动机的方法，用于驱动该方法公开(公告)号：US20120279229A1
公开(公告)日：2012-11-08
申请号：US13462920
申请日：2012-05-03
IPC分类号： F02C9/00
CPC分类号： F02C9/28 , F02C7/057 , F02C9/48 , F05D2260/80 , F05D2260/96 , F05D2270/11 , F05D2270/14 , F23N5/16 , F23N5/242 , F23R2900/00013
摘要： A method can protect a gas turbine engine (10), which includes a compressor (11), a combustor (13), and a turbine (12), against high dynamical process values, especially in combustor/flame pulsations. Effective protection against high dynamical process values, especially in combustor/flame pulsations, can be achieved by: a) measuring the pulsations of the combustor (13) with a suitable sensor (18), b) dividing the frequency spectrum of the measured pulsation signal up into pre-defined band pass sections, c) computing the rms (root mean square) of the signal for each band, d) weighting the computed frequency/frequency band rms with predetermined weighting factors, e) cumulating the weighted frequency/frequency band rms values to get a Pulsation Limit Criterion (PLC) value, f) comparing the PLC value with at least one reference value (23), and g) operating the gas turbine engine (10) according to the result of the comparison.
摘要翻译： 一种方法可以防止包括压缩机（11），燃烧器（13）和涡轮（12）的燃气涡轮发动机（10），抵抗高动力学过程值，特别是在燃烧器/火焰脉动中。 可以通过以下方式来实现对高动力过程值的有效保护，特别是在燃烧器/火焰脉动中：a）用合适的传感器（18）测量燃烧器（13）的脉动，b）将所测量的脉动信号的频谱 c）计算每个频带的信号的均方根（均方根），d）用预定的加权因子对所计算的频率/频带rms进行加权，e）累积加权的频率/频带 rms值以获得脉冲限制标准（PLC）值，f）将PLC值与至少一个参考值（23）进行比较，以及g）根据比较结果来操作燃气涡轮发动机（10）。
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公开(公告)号：US07751943B2
公开(公告)日：2010-07-06
申请号：US11275858
申请日：2006-02-01
IPC分类号： G05D3/12 , G05D5/00 , G05D9/00 , G05D11/00 , G05D17/00 , F02C3/00 , F02C9/00 , F02C7/36 , F02G3/00 , G05D13/00
CPC分类号： F23N5/242 , F23N5/16 , F23N2025/04 , F23N2041/20 , F23R2900/00013 , Y10T477/40
摘要： In a process for protection of a gas turbine (1) from damage caused by pressure pulsations (P), pressure pulsations (P) occurring during the operation of the gas turbine (1) are measured, from the measured pressure pulsations (P), a pulsation-time signal (PZS) is generated, the pulsation-time signal (PZS) is transformed into a pulsation-frequency signal (PFS), from the pulsation-frequency signal (PFS), a pulsation level (PL) is determined for at least one specified monitoring frequency band (12), the pulsation level (PL) is monitored for the occurrence of at least one specified trigger condition, and, when the at least one trigger condition occurs, a specified protective action (16) is carried out.
摘要翻译： 在保护燃气轮机（1）免受压力脉动（P）引起的损害的过程中，从测量的压力脉动（P），测量在燃气轮机（1）的运行期间发生的压力脉动（P） 产生脉动时间信号（PZS），脉动时间信号（PZS）从脉动频率信号（PFS）变换为脉动频率信号（PFS），确定脉动水平（PL）为 监视至少一个指定的监视频带（12），脉动水平（PL）发生至少一个指定的触发条件，并且当发生至少一个触发条件时，承载指定的保护动作（16） 出来
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公开(公告)号：US20090297698A1
公开(公告)日：2009-12-03
申请号：US12472801
申请日：2009-05-27
IPC分类号： B05D5/12
摘要： A method for forming an oxygen resistant aluminum oxide layer on an outer surface of a thermocouple sheath composed of a nickel alloy containing between 1% to 7% aluminium comprises removing a pre-formed oxide layer from the outer surface so as to create a prepared sheath; performing a controlled oxidation by subjecting the prepared sheath to atmospheric conditions at a temperature between 1000° C. and 1250° C. so as to form the oxygen resistant layer on the thermocouple sheath and to thus form an oxidised sheath; and cooling the oxidised sheath so as to prepare the oxidized sheath for service.
摘要翻译： 在由包含1％至7％的铝的镍合金构成的热电偶护套的外表面上形成氧化铝氧化物层的方法包括从外表面去除预先形成的氧化物层，以形成制备的护套 ; 通过在1000℃至1250℃的温度下对所制备的护套进行大气条件进行受控氧化，以在热电偶护套上形成耐氧层，从而形成氧化护套; 并冷却氧化的护套，以制备用于使用的氧化护套。
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公开(公告)号：US20060088075A1
公开(公告)日：2006-04-27
申请号：US11256719
申请日：2005-10-24
申请人： Paolo Ruffino , Hanspeter Zinn
发明人： Paolo Ruffino , Hanspeter Zinn
IPC分类号： G01K1/00
摘要： An apparatus for a rapid measurement of temperatures in a hot gas flow, in particular in a gas turbine. The apparatus includes a sensor having two two-dimensional, electrically conductive heating elements, which are attached to the surface of a common, electrically insulating sensor body.
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公开(公告)号：US20100021338A1
公开(公告)日：2010-01-28
申请号：US12509076
申请日：2009-07-24
CPC分类号： C22C38/26 , C22C38/002 , C22C38/005 , C22C38/22 , C22C38/28 , C22C38/32
摘要： An iron-based high-temperature alloy is disclosed which contains the following chemical composition: 20% by weight Cr; 5 to 6% by weight Al; 4% by weight Ta; 4% by weight Mo; 3 to 4% by weight Re; 0.2% by weight Zr; 0.05% by weight B; 0.1% by weight Y; 0.1% by weight Hf; 0 to 0.05% by weight C; and remainder Fe and unavoidable impurities. The alloy can be produced at low cost and can possess outstanding oxidation resistance and good mechanical properties at temperatures up to 1200° C.
摘要翻译： 公开了一种铁基高温合金，其含有以下化学组成：20重量％的Cr; 5〜6重量％的Al; 4重量％Ta; 4％（重量）Mo; 3〜4重量％Re; 0.2重量％Zr; 0.05重量％B; 0.1重量％Y; 0.1重量％Hf; 0〜0.05重量％C; 余量为Fe和不可避免的杂质。 该合金可以低成本生产，并且可以在高达1200℃的温度下具有优异的抗氧化性和良好的机械性能。
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6.发明申请Method for operating a gas turbine installation, and gas turbine installation 失效操作燃气轮机安装的方法，以及燃气轮机的安装公开(公告)号：US20060075755A1
公开(公告)日：2006-04-13
申请号：US11009131
申请日：2004-12-13
申请人： Carlos Haertel , Sasha Savic , Hanspeter Zinn
发明人： Carlos Haertel , Sasha Savic , Hanspeter Zinn
IPC分类号： F02C3/30
CPC分类号： F01K21/047 , F02C3/30 , F02C7/1435 , F04D29/5846
摘要： A method for operating a gas turbine installation (1) includes sucking in a gaseous medium (2) by the compressor (3) and compressed in the compressor space, a liquid medium (10) being injected into the gaseous medium (2), so that a two-phase flow comprising a gaseous phase and a liquid phase is formed at least in a subregion of the compressor (3). The gaseous medium (2) is then burnt with fuel (5) in a combustion chamber (6) to form hot gases (7), and the hot gases (7) are expanded in a turbine (8), the hot components of the gas turbine installation (1) being cooled by cooling air (14) of a cooling air system. A measurement is carried out to determine whether a liquid phase is present in a region of the compressor (3) and/or of the cooling air system.
摘要翻译： 用于操作燃气轮机装置（1）的方法包括：通过压缩机（3）吸入气体介质（2）并在压缩机空间中被压缩，将液体介质（10）注入到气体介质（2）中，因此 至少在压缩机（3）的一个分区中形成包含气相和液相的两相流。 然后气体介质（2）在燃烧室（6）中用燃料（5）燃烧以形成热气体（7），并且热气体（7）在涡轮机（8）中膨胀，热气体 燃气轮机安装（1）由冷却空气系统的冷却空气（14）冷却。 进行测量以确定压缩机（3）和/或冷却空气系统的区域中是否存在液相。
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7.发明授权Method for protecting a gas turbine engine against high dynamical process values and gas turbine engine for conducting the method 有权用于保护燃气涡轮发动机免受高动力过程值和用于进行该方法的燃气涡轮发动机的方法公开(公告)号：US09068512B2
公开(公告)日：2015-06-30
申请号：US13462920
申请日：2012-05-03
CPC分类号： F02C9/28 , F02C7/057 , F02C9/48 , F05D2260/80 , F05D2260/96 , F05D2270/11 , F05D2270/14 , F23N5/16 , F23N5/242 , F23R2900/00013
摘要： A method can protect a gas turbine engine (10), which includes a compressor (11), a combustor (13), and a turbine (12), against high dynamical process values, especially in combustor/flame pulsations. Effective protection against high dynamical process values, especially in combustor/flame pulsations, can be achieved by: a) measuring the pulsations of the combustor (13) with a suitable sensor (18), b) dividing the frequency spectrum of the measured pulsation signal up into pre-defined band pass sections, c) computing the rms (root mean square) of the signal for each band, d) weighting the computed frequency/frequency band rms with predetermined weighting factors, e) cumulating the weighted frequency/frequency band rms values to get a Pulsation Limit Criterion (PLC) value, f) comparing the PLC value with at least one reference value (23), and g) operating the gas turbine engine (10) according to the result of the comparison.
摘要翻译： 一种方法可以防止包括压缩机（11），燃烧器（13）和涡轮（12）的燃气涡轮发动机（10），抵抗高动力学过程值，特别是在燃烧器/火焰脉动中。 可以通过以下方式来实现对高动力过程值的有效保护，特别是在燃烧器/火焰脉动中：a）用合适的传感器（18）测量燃烧器（13）的脉动，b）将所测量的脉动信号 c）计算每个频带的信号的均方根（均方根），d）用预定的加权因子对所计算的频率/频带rms进行加权，e）累积加权的频率/频带 rms值以获得脉冲限制标准（PLC）值，f）将PLC值与至少一个参考值（23）进行比较，以及g）根据比较结果来操作燃气涡轮发动机（10）。
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公开(公告)号：US08153054B2
公开(公告)日：2012-04-10
申请号：US12509076
申请日：2009-07-24
CPC分类号： C22C38/26 , C22C38/002 , C22C38/005 , C22C38/22 , C22C38/28 , C22C38/32
摘要： An iron-based high-temperature alloy is disclosed which contains the following chemical composition: 20% by weight Cr; 5 to 6% by weight Al; 4% by weight Ta; 4% by weight Mo; 3 to 4% by weight Re; 0.2% by weight Zr; 0.05% by weight B; 0.1% by weight Y; 0.1% by weight Hf; 0 to 0.05% by weight C; and remainder Fe and unavoidable impurities. The alloy can be produced at low cost and can possess outstanding oxidation resistance and good mechanical properties at temperatures up to 1200° C.
摘要翻译： 公开了一种铁基高温合金，其含有以下化学组成：20重量％的Cr; 5〜6重量％的Al; 4重量％Ta; 4％（重量）Mo; 3〜4重量％Re; 0.2重量％Zr; 0.05重量％B; 0.1重量％Y; 0.1重量％Hf; 0〜0.05重量％C; 余量为Fe和不可避免的杂质。 该合金可以低成本生产，并且可以在高达1200℃的温度下具有优异的抗氧化性和良好的机械性能。
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9.发明授权Method for operating a gas turbine installation, and gas turbine installation 失效操作燃气轮机安装的方法，以及燃气轮机的安装公开(公告)号：US07269954B2
公开(公告)日：2007-09-18
申请号：US11009131
申请日：2004-12-13
CPC分类号： F01K21/047 , F02C3/30 , F02C7/1435 , F04D29/5846
摘要： A method for operating a gas turbine installation (1) includes sucking in a gaseous medium (2) by the compressor (3) and compressed in the compressor space, a liquid medium (10) being injected into the gaseous medium (2), so that a two-phase flow comprising a gaseous phase and a liquid phase is formed at least in a subregion of the compressor (3). The gaseous medium (2) is then burnt with fuel (5) in a combustion chamber (6) to form hot gases (7), and the hot gases (7) are expanded in a turbine (8), the hot components of the gas turbine installation (1) being cooled by cooling air (14) of a cooling air system. A measurement is carried out to determine whether a liquid phase is present in a region of the compressor (3) and/or of the cooling air system.
摘要翻译： 用于操作燃气轮机装置（1）的方法包括：通过压缩机（3）吸入气体介质（2）并在压缩机空间中被压缩，将液体介质（10）注入到气体介质（2）中，因此 至少在压缩机（3）的一个分区中形成包含气相和液相的两相流。 然后气体介质（2）在燃烧室（6）中用燃料（5）燃烧以形成热气体（7），并且热气体（7）在涡轮机（8）中膨胀，热气体 燃气轮机安装（1）由冷却空气系统的冷却空气（14）冷却。 进行测量以确定压缩机（3）和/或冷却空气系统的区域中是否存在液相。
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公开(公告)号：US07216486B2
公开(公告)日：2007-05-15
申请号：US10894031
申请日：2004-07-20
CPC分类号： G01N21/359 , F02C3/22 , F02C9/40 , F23N5/003 , F23N2021/10 , G01N21/3504 , G01N33/225
摘要： Relevant fuel-gas properties (XG) are measured on an ongoing basis while a gas turbine group is operating. The C2+alkane content of the fuel gas is of particular interest in this context, since it has a significant influence on the ignitability of the fuel gas in the combustion chamber. The operating parameters of the gas turbine group are acted on directly as a function of the measured fuel-gas properties. In particular, in the case of the example of a gas turbine group with sequential combustion, the distribution of the fuel mass flows ({dot over (m)}EV, {dot over (m)}SEV) between the combustion chambers (4, 8) of the gas turbine group is varied. Furthermore, if there is provision for inert media, such as water or steam, to be introduced, it is possible for the mass flow of inert media ({dot over (m)}ST) to be controlled as a function of the measured fuel properties.
摘要翻译： 在燃气轮机组运行的同时，持续地测量相关的燃料气体性质（X N G）。 在这种情况下，燃料气体的C 2 + C 2烷烃含量是特别有意义的，因为它对燃烧室中的燃料气体的可燃性具有显着的影响。 燃气轮机组的操作参数作为测量的燃料 - 气体性质的函数直接作用。 特别地，在具有顺序燃烧的燃气轮机组的示例的情况下，燃料质量的分布流动（{dot over（m）EV，{dot over（m SEV < 燃气轮机组的燃烧室（4,8）之间的距离变化，此外，如果设置要引入的惰性介质，例如水或蒸汽，则惰性物质流可能 作为测量的燃料性质的函数来控制介质（{dot over（m ST ST ））。
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