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. 发明公开

CN105026734A 发动机燃油供给回路的定量装置失效
公开(公告)号：CN105026734A
公开(公告)日：2015-11-04
申请号：CN201480012982.4
申请日：2014-03-07
申请人：涡轮梅坎公司
发明人：史蒂芬·兰福德 , 菲利普·让·雷内·玛丽·本尼扎克 , 皮埃尔·斯盖尔 , 拉斐尔·萨姆森
IPC分类号： F02C9/26 , F02C9/46
CPC分类号： F02C9/263 , F02C9/46 , F05D2200/221 , Y02T50/671
摘要：一种发动机燃油供应回路的计量装置，包括计量阀(21)，以及压力控制装置，该压力控制装置在该计量阀(21)的下游与上游之间保持一的恒定的压力差，其中，该计量阀(21)包括一个设置有进口孔(31e)和出口孔(31s)的底座(31)，被布置在该底座(31)内的开闭器(32)，以及控制该开闭器(32)的位置的致动器，该开闭器(32)在该进口孔(31e)与该出口孔(31s)之间限定一通道，该通道的最小截面基于该开闭器(32)沿在下止点与上止点之间延伸并经过一阈值位置的一个通道的位置是可变的。根据本发明，该开闭器(32)的设置方式使得该通道的最小截面，继而穿过该阀(21)的燃油的流速，基于在该下止点与该阈值位置之间的该开闭器的位置的坐标而线性地增加，该通道的最小截面，继而燃油的流速，基于在该阈值位置与该上止点之间的该开闭器的位置的坐标而平方地或更快地增加。

2. 发明授权

CN100557201C 燃气轮机的可变喷嘴有权转让
公开(公告)号：CN100557201C
公开(公告)日：2009-11-04
申请号：CN200480035996.4
申请日：2004-11-30
申请人：诺沃皮尼奥内控股有限公司
发明人： G·萨萨内利
IPC分类号： F01D17/16 , F01D5/14
CPC分类号： F01D17/162 , F01D5/14 , F01D5/141 , F05D2200/22 , F05D2200/221 , F05D2200/222 , F05D2200/24 , F05D2200/25 , F05D2240/128 , F05D2240/301 , F05D2250/16 , F05D2250/17 , F05D2250/70 , F05D2250/71 , F05D2250/711 , F05D2250/712 , F05D2260/74
摘要：一种固定到轴(11)上的燃气轮机的可变喷嘴(10)，所述喷嘴(10)具有上压力面(12)和与上表面(12)相对的下负压面，可变喷嘴包括一系列大致呈“C”形的剖面，每一剖面具有第一修圆端和第二修圆端，所述系列剖面中的每一剖面还具有带有向上正对着底部(90)的凹部，并且每一剖面沿着曲线(60)在轴(11)的轴线方向上彼此连续布置，至少为二次的曲线(60)位于表面(70)上，其中所述表面(70)的轴线与轴(11)的轴线正交，并且所述表面(70)还以一个角度(80)相对于底部(90)倾斜布置。

3. 发明公开

CN1890455A 燃气轮机的可变喷嘴有权转让
公开(公告)号：CN1890455A
公开(公告)日：2007-01-03
申请号：CN200480035996.4
申请日：2004-11-30
申请人：诺沃皮尼奥内控股有限公司
发明人： G·萨萨内利
IPC分类号： F01D17/16 , F01D5/14
CPC分类号： F01D17/162 , F01D5/14 , F01D5/141 , F05D2200/22 , F05D2200/221 , F05D2200/222 , F05D2200/24 , F05D2200/25 , F05D2240/128 , F05D2240/301 , F05D2250/16 , F05D2250/17 , F05D2250/70 , F05D2250/71 , F05D2250/711 , F05D2250/712 , F05D2260/74
摘要：一种固定到轴(11)上的燃气轮机的可变喷嘴(10)，所述喷嘴(10)具有上压力面(12)和与上表面(12)相对的下负压面，可变喷嘴包括一系列大致呈“C”形的剖面，每一剖面具有第一修圆端和第二修圆端，所述系列剖面中的每一剖面还具有带有向上正对着底部(90)的凹部，并且每一剖面沿着曲线(60)在轴(11)的轴线方向上彼此连续布置，至少为二次的曲线(60)位于表面(70)上，其中所述表面(70)的轴线与轴(11)的轴线正交，并且所述表面(70)还以一个角度(80)相对于底部(90)倾斜布置。

4. 发明授权

CN105026734B 发动机燃油供给回路的定量装置失效
公开(公告)号：CN105026734B
公开(公告)日：2017-04-05
申请号：CN201480012982.4
申请日：2014-03-07
申请人：涡轮梅坎公司
发明人：史蒂芬·兰福德 , 菲利普·让·雷内·玛丽·本尼扎克 , 皮埃尔·斯盖尔 , 拉斐尔·萨姆森
IPC分类号： F02C9/26 , F02C9/46
CPC分类号： F02C9/263 , F02C9/46 , F05D2200/221 , Y02T50/671
摘要：一种发动机燃油供应回路的计量装置，包括计量阀(21)，以及压力控制装置，该压力控制装置在该计量阀(21)的下游与上游之间保持一的恒定的压力差，其中，该计量阀(21)包括一个设置有进口孔(31e)和出口孔(31s)的底座(31)，被布置在该底座(31)内的开闭器(32)，以及控制该开闭器(32)的位置的致动器，该开闭器(32)在该进口孔(31e)与该出口孔(31s)之间限定一通道，该通道的最小截面基于该开闭器(32)沿在下止点与上止点之间延伸并经过一阈值位置的一个通道的位置是可变的。根据本发明，该开闭器(32)的设置方式使得该通道的最小截面，继而穿过该阀(21)的燃油的流速，基于在该下止点与该阈值位置之间的该开闭器的位置的坐标而线性地增加，该通道的最小截面，继而燃油的流速，基于在该阈值位置与该上止点之间的该开闭器的位置的坐标而平方地或更快地增加。

5. 发明申请

US20160017817A1 METERING DEVICE FOR A FUEL FEED CIRCUIT OF AN ENGINE 审中-公开
标题翻译：用于发动机燃油进给电路的计量装置
公开(公告)号：US20160017817A1
公开(公告)日：2016-01-21
申请号：US14773569
申请日：2014-03-07
申请人： TURBOMECA
发明人： Stephen LANGFORD , Philippe Jean, Rene, Marie BENEZECH , Pierre SICAIRE , Rafael SAMSON
IPC分类号： F02C9/26
CPC分类号： F02C9/263 , F02C9/46 , F05D2200/221 , Y02T50/671
摘要： A metering device for an engine fuel feed circuit, the device including a metering valve, and a pressure regulator device maintaining a constant pressure difference from downstream to upstream across the metering valve, wherein the metering valve includes a seat provided with an inlet orifice and an outlet orifice, a shutter arranged within the seat, and an actuator controlling the position of the shutter, and wherein, between the inlet orifice and the outlet orifice the shutter defines a passage of minimum section that is variable as a function of the position of the shutter along a stroke extending between a bottom abutment and a top abutment and passing via a threshold position.
摘要翻译：一种用于发动机燃料供给回路的计量装置，该装置包括一个计量阀和一个压力调节装置，该压力调节装置在整个计量阀上保持从下游到上游恒定的压力差，其中计量阀包括设置有入口孔和出口孔，布置在座内的快门以及控制快门位置的致动器，并且其中，在入口孔和出口孔之间，快门限定最小部分的通道，该最小部分可根据快门沿着在底部支座和顶部支座之间延伸并经过阈值位置的行程。

6. 发明授权

US4566273A Pneumatic servomotor 失效
标题翻译：气动伺服电机
公开(公告)号：US4566273A
公开(公告)日：1986-01-28
申请号：US474285
申请日：1983-03-11
申请人： Markus Baumeler
发明人： Markus Baumeler
IPC分类号： F16K31/12 , F01D17/14 , F16K31/122 , F16K31/42 , F16K47/00 , F15B11/06
CPC分类号： F16K31/122 , F01D17/145 , F16K47/00 , F05D2200/221
摘要： The servomotor is constructed in one embodiment with a partition which forms a constriction through which air is throttled during an emergency closing of the valve. The constriction is formed with a flow resistance equivalent to a free cross-sectional area of not more than 0.02D.sup.2 ; D being the inside diameter of the cylinder. In addition, the chamber defined between the piston and the partition is not more than 10% of the combined volume of this chamber and a pressurized chamber below the partition.In another embodiment, the pressurized chamber may be formed by a pressure tank which is connected via a line which forms a constriction to the chamber below the piston. In still another embodiment, a spherical pressure tank may be secured about a cup-shaped cylinder to form the pressurized chamber while radial grooves in a flange of the cylinder form a constriction with a cover secured to the cylinder and spherical tank.
摘要翻译：伺服电动机在一个实施例中被构造成具有形成收缩部的隔板，在阀的紧急关闭期间空气被节流。收缩部形成有相当于0.02D2以下的自由截面积的流动阻力; D是气缸的内径。另外，在活塞和分隔件之间限定的腔室不超过该腔室的组合体积的10％以及隔板下方的加压室。在另一个实施例中，加压室可以由压力罐形成，该压力罐经由形成收缩部的管线连接到活塞下方的室。在另一个实施例中，球形压力罐可以围绕杯形圆柱体固定以形成加压室，而圆柱形凸缘中的径向槽形成与固定到圆柱体和球形罐的盖的收缩。

7. 发明申请

US20190186357A1 GAS TURBINE ENGINE WITH FAN TIED COMPRESSOR 审中-公开
公开(公告)号：US20190186357A1
公开(公告)日：2019-06-20
申请号：US16282891
申请日：2019-02-22
申请人： United Technologies Corporation
发明人： Gabriel L. Suciu , Frederick M. Schwarz , William K. Ackermann , Daniel Bernard Kupratis
IPC分类号： F02C3/113 , F02K3/072 , F02C9/16 , F02K3/06 , F02C3/06 , F02C7/36
CPC分类号： F02C3/113 , F02C3/06 , F02C7/36 , F02C9/16 , F02K3/06 , F02K3/072 , F05D2200/221 , F05D2220/3215 , F05D2220/323 , F05D2260/40311 , F05D2270/20
摘要： A turbofan engine according to an example of the present disclosure includes, among other things, a fan including fan blades, an outer housing that surrounds the fan to define a bypass flow path, a compressor section in fluid communication with the fan, the compressor section including a low pressure compressor section and a high pressure compressor section, a turbine section including a fan drive turbine section driving the fan and the low pressure compressor section and a high pressure turbine section driving the high pressure compressor section. A gear reduction including an epicyclic gear train is between the fan drive turbine section and the low pressure compressor section such that the low pressure compressor section and the fan are rotatable at a common speed and such that the fan is rotatable at a lower speed than the fan drive turbine section. The fan drive turbine section has a first exit area at a first exit point and is rotatable at a first speed, the high pressure turbine section has a second exit area at a second exit point and is rotatable at a second speed, which is higher than the first speed. A first performance quantity is defined as a product of the first speed squared and the first area, a second performance quantity is defined as a product of the second speed squared and the second exit area and a performance ratio of the first performance quantity to the second performance quantity is between 0.2 and 0.8.

8. 发明公开

EP1096122A4 METHOD FOR DETECTING SENSOR FAILURES AND FOR CONTROLLING THE OPERATION CONDITIONS OF AN OBJECT 审中-公开
标题翻译：一种确定传感器故障和一些控制对象的工作条件
公开(公告)号：EP1096122A4
公开(公告)日：2001-10-31
申请号：EP99927001
申请日：1999-06-03
申请人： OTKRITOE AKTSIONERNOE OBSCHEST
发明人： ZAZULOV VIKTOR IVANOVICH , BONDAREV LEONID YAKOVLEVICH , ZELIKIN JURY MARKOVICH , DOBRYNIN ANDREI ALEXSANDROVICH , KLEPIKOV VLADIMIR IVANOVICH
IPC分类号： F02C9/46 , F01D17/20 , F01D21/00 , G05B9/02 , G05B9/03 , F02C9/00 , G05B23/00
CPC分类号： G05B9/03 , F01D17/20 , F01D21/003 , F05D2200/11 , F05D2200/221 , F05D2270/01 , F05D2270/30 , G05B9/02
摘要： The present invention relates to control systems intended for use in complex technical objects that operate in a wide range of modes and loads, wherein said invention can be used in the control systems of jet engines, power-plant turbines, etc. The method of the present invention involves connecting sensors (3) to the condition monitoring units which are designed according the model of the engine (object) (1), and connecting all sensors but one to the remaining monitoring units. The method involves calculating the weighted sum of the square values of the offsets between all condition monitoring units, and comparing the values of the weighted sum of the square values of the offsets in a first unit with the values of the weighted sums of the square values of the offsets in each of the remaining monitoring units. The maximal value among the values of the difference signals obtained is compared with a threshold value and, in case said value exceeds the threshold value, a failure signal is generated for that sensor (3) whose parameters are not used in the operation monitoring unit. The method further involves determining for each monitoring unit the potential location area of the offsets due to parametering errors of the object model, and determining those monitoring units whose offsets exceed the limits of a predetermined area.

9. 发明申请

WO2005054633A1 VARIABLE NOZZLE FOR A GAS TURBINE 审中-公开
标题翻译：用于气体涡轮的可变喷嘴
公开(公告)号：WO2005054633A1
公开(公告)日：2005-06-16
申请号：PCT/EP2004/013657
申请日：2004-11-30
申请人： NUOVO PIGNONE HOLDING S.p.A. , SASSANELLI, Giuseppe
发明人： SASSANELLI, Giuseppe
IPC分类号： F01D17/16
CPC分类号： F01D17/162 , F01D5/14 , F01D5/141 , F05D2200/22 , F05D2200/221 , F05D2200/222 , F05D2200/24 , F05D2200/25 , F05D2240/128 , F05D2240/301 , F05D2250/16 , F05D2250/17 , F05D2250/70 , F05D2250/71 , F05D2250/711 , F05D2250/712 , F05D2260/74
摘要： Variable nozzle (10) for a gas turbine fixed to a shaft (11) equipped with a pressurized upper surface (12) and a depressurized lower surface opposite to the upper surface (12), the variable nozzle comprises a series of substantially "C"-shaped sections, each having a first rounded end and a second rounded end each section of the series of sections also having the concavity facing upwards with respect to a base (90) and arranged one after another continuously, in the direction of an axis of the shaft (11) along a curved line (60), the at least second degree curved line (60) lies on a surface (70) having an axis orthogonal to the axis of the shaft (11) and also tilted with respect to the base (90) by an angle (80).
摘要翻译：固定在具有加压上表面（12）的轴（11）和与上表面（12）相对的减压下表面的燃气轮机的可变喷嘴（10），所述可变喷嘴包括一系列基本上“C” 每个部分具有第一圆形端部和第二圆形端部，所述一系列部分的每个部分还具有相对于基部（90）面向上的凹部，并且沿着轴线方向连续布置所述轴（11）沿着曲线（60），所述至少第二度曲线（60）位于具有与所述轴（11）的轴线正交的轴线的表面（70）上，并且还相对于所述轴线基座（90）角度（80）。

10. 发明公开

EP2971703A1 DISPOSITIF DE DOSAGE D'UN CIRCUIT D'ALIMENTATION EN CARBURANT D'UN MOTEUR 审中-公开
标题翻译：配料装置用于电动机的燃料供应回路
公开(公告)号：EP2971703A1
公开(公告)日：2016-01-20
申请号：EP14715344.9
申请日：2014-03-07
申请人： Turbomeca
发明人： LANGFORD, Stephen , BENEZECH, Philippe, Jean, René, Marie , SICAIRE, Pierre , SAMSON, Rafaël
IPC分类号： F02C9/26 , F02C9/46
CPC分类号： F02C9/263 , F02C9/46 , F05D2200/221 , Y02T50/671
摘要： A dosing device for an engine fuel supply circuit comprising a dosing valve (21), and a pressure control device keeping a constant pressure differential between the downstream and upstream of the dosing valve (21), in which the dosing valve (21) comprises a seat (31), provided with an inlet opening (31e) and an outlet opening (31s), a shutter (32), disposed within the seat (31), and an actuator, controlling the position of the shutter (32), and in which the shutter (32) defines a passage between the inlet opening (31e) and the outlet opening (31s) of which the minimum cross-section is variable on the basis of the position of the shutter (32) along a path extending between a lower stop and an upper stop and passing through a threshold position. According to the invention, the shutter (32) is configured in such a way that the minimum cross-section of said passage, and therefore the flow of fuel passing through the valve (21), increases linearly on the basis of the coordinate of the position of the shutter between the lower stop and the threshold position, and that the minimum cross-section of said passage, and therefore the flow of fuel, increases quadratically, or more quickly, on the basis of the coordinate of the position of the shutter between the threshold position and the upper stop.

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