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41. 发明专利

JPS63212725A BIAXIAL GAS TURBINE CONTROL SYSTEM 失效
公开(公告)号：JPS63212725A
公开(公告)日：1988-09-05
申请号：JP3541888
申请日：1988-02-19
申请人： NUOVO PIGNONE SPA
发明人： ERIO BENBENUUCHI , BURUUNO INNOCHIENCHI
IPC分类号： F02C7/057 , F01D17/06 , F01D17/08 , F01D17/16 , F02C9/22 , F02C9/28 , F02C9/54

42. 发明专利

JPS6343569B2 失效
公开(公告)号：JPS6343569B2
公开(公告)日：1988-08-31
申请号：JP16003585
申请日：1985-07-19
申请人： YUNAITETSUDO TEKUNOROJIIZU CORP
发明人： CHAARUZU FUREDERITSUKU SUTAANSU
IPC分类号： F02C9/28 , F02C9/26 , F02C9/32 , F02C9/38 , F02C9/54

43. 发明专利

JPS6258021A FUEL SYSTEM OF GAS TURBINE ENGINE 失效
公开(公告)号：JPS6258021A
公开(公告)日：1987-03-13
申请号：JP18836086
申请日：1986-08-11
申请人： ROLLS ROYCE PLC
发明人： JIYON BOOGAN RUTSUKUSU , RATSUSERU ARAN ROTSUKUSUREI
IPC分类号： F02C9/36 , F02C7/22 , F02C9/54 , F04C2/18

44. 发明专利

JPS6130142B2 失效
公开(公告)号：JPS6130142B2
公开(公告)日：1986-07-11
申请号：JP15059178
申请日：1978-12-07
申请人： GEN ELECTRIC
发明人： JATSUKU EDOWAADO KOONETSUTO , RARUFU KONNAA KOORII , TOOMASU ORISON FUREIRII , ANDORYUU AKUSERU SANDAASU JUNIA
IPC分类号： F02C9/20 , F02C9/54 , F02K3/04

45. 发明专利

JPS6193235A Fuel controller 失效
公开(公告)号：JPS6193235A
公开(公告)日：1986-05-12
申请号：JP16003585
申请日：1985-07-19
申请人： United Technologies Corp
发明人： CHIYAARUZU FUREDERITSUKU SUTAA
IPC分类号： F02C9/28 , F02C9/26 , F02C9/32 , F02C9/38 , F02C9/54
CPC分类号： F02C9/38 , F02C9/26 , F02C9/54

46. 发明专利

JPS6143223A Gas turbine with measure to counter environment 失效
标题翻译：气体涡轮计量环境
公开(公告)号：JPS6143223A
公开(公告)日：1986-03-01
申请号：JP16292784
申请日：1984-08-03
申请人： Hitachi Ltd
发明人： TERANISHI MITSUO , HIROSE FUMIYUKI , INOSE HIROSHI
IPC分类号： F02C7/057 , F02C9/54
CPC分类号： F02C9/54
摘要： PURPOSE:To reduce a harmful component in exhaust gas from a turbine when it is partly loaded, by changing a mounting angle of a variable stationary blade in a compressor so that a flow proportion of fuel to air may be controlled to a fixed range. CONSTITUTION:A flow of fuel F fed to a combustor 4 is measured by a detector 7, and its signal 8 is fed to a control device 9. Here a mounting angle control signal 10 for a variable stationary blade 2 provided in an axial compressor 1 is calculated being fed to a variable stationary blade driving gear 3 so that fuel-air ratio F/A may be controlled to a fixed value. In this way, a turbine, even when it is partly loaded, enables a harmful component in exhaust gas to be reduced by controlling the fuel-air ratio within a fixed range.
摘要翻译：目的：通过改变压缩机中的可变静止叶片的安装角度，可以将燃料对空气的流量比例控制在一定范围内，从而减少来自涡轮机的部分负荷的废气中的有害成分。构成：通过检测器7测量供给燃烧器4的燃料F的流动，其信号8被送入控制装置9.这里，设置在轴向压缩机1中的可变静止叶片2的安装角度控制信号10 被计算为可变的固定叶片驱动齿轮3，从而燃料 - 空气比F / A可以被控制到固定值。以这种方式，即使在部分负载的情况下，涡轮也能够通过将燃料空气比控制在固定范围内来减少废气中的有害成分。

47. 发明专利

JPS6073017A CONTROLLER FOR REHEAT GAS TURBINE 失效
公开(公告)号：JPS6073017A
公开(公告)日：1985-04-25
申请号：JP17937983
申请日：1983-09-29
申请人： KOGYO GIJUTSUIN
发明人： TANAKA MASARU , YASUI HAJIME , TAKEYA KAZUO
IPC分类号： F02C9/28 , F02C7/26 , F02C9/50 , F02C9/52 , F02C9/54
摘要： PURPOSE:To permit smooth and rapid starting operation by igniting a high-pressure combustor and a low-pressure combustor in succession and controlling a low-pressure shaft towards speed increase, after a high-pressure shaft is controlled towards speed increase. CONSTITUTION:When a high-pressure turbine 5 and a low-pressure turbine 8 are started separately and a prescribed ignition revolution number is reached, an ignition signal is sent into the fuel control valve 14 of a high-pressure combustor 4. Then, an ignition signal is sent into the fuel control valve 15 of a low-pressure combustor 7. After ignition, each opening degree of the fuel control valves 14 and 15 is throttled to the min. value, and after the lapse of a prescribed time, a high-pressure shaft is controlled towards the increase of speed according to the acceleration setting schedule, and then a low-pressure shaft is controlled towards speed increase, aiming at the turbine outlet temp. When a prescribed speed is obtained, incorporation with a power generator 9 system is performed. Therefore, starting operation can be preformed smoothly and rapidly.

48. 发明专利

JPS5949413B2 JPS5949413B2 - 失效
公开(公告)号：JPS5949413B2
公开(公告)日：1984-12-03
申请号：JP5145579
申请日：1979-04-27
申请人： Mitsubishi Jukogyo Kk , Mitsubishi Jidosha Kogyo Kk
发明人： MYATA TERUO , OKAMOTO NOBUICHI , KINO ETSUJI , SUMINOE ARATA , FUJII NOBORU
IPC分类号： F02C9/28 , F02C9/00 , F02C9/54

49. 发明专利

JPS59122730A Controller of gas turbine engine 失效
标题翻译：气动涡轮发动机控制器
公开(公告)号：JPS59122730A
公开(公告)日：1984-07-16
申请号：JP22764582
申请日：1982-12-28
申请人： Nissan Motor Co Ltd
发明人： YOSHIDA KENICHI
IPC分类号： F02C9/20 , F02C3/10 , F02C9/28 , F02C9/54 , F04D27/02
CPC分类号： F04D27/0261 , F05D2270/101
摘要： PURPOSE:To prevent a surge controller from overrunning by comparing the output from a surge detecting means with a specified reference value to detect any unusual operation of a surge detecting means and constantly restraining creation of any surge. CONSTITUTION:If surging may occur, the target value of the inlet temperature of a turbine is reduced and then gradually returned to the original value. If a surging detecting means may fail, the malfunction of the surge sensor 16 is detected by comparing the output of the means with the reference value which corresponds to the signal value of the surge sensor 16 and fail-safe control is performed so as to restrain the target value of the inlet temperature of a turbine under the specified value. The occurrence of the surging may be thereby forcedly restrained so that the damage of an engine may be prevented.
摘要翻译：目的：通过将浪涌检测装置的输出与指定的参考值相比较来防止浪涌控制器超驰，以检测浪涌检测装置的任何异常操作，并持续抑制任何浪涌的产生。构成：如果可能发生浪涌，则涡轮机入口温度的目标值减小，然后逐渐恢复到原始值。如果浪涌检测装置可能失败，则通过将装置的输出与对应于浪涌传感器16的信号值的参考值进行比较来检测浪涌传感器16的故障，并执行故障安全控制以便抑制涡轮机入口温度的目标值在规定值以下。因此可以强制地抑制浪涌的发生，从而可以防止发动机的损坏。

50. 实用新型

JPS5924943U JPS5924943U - 失效
公开(公告)号：JPS5924943U
公开(公告)日：1984-02-16
申请号：JP12056282
申请日：1982-08-10
IPC分类号： F02C9/22 , F02C6/00 , F02C9/28 , F02C9/48 , F02C9/54 , F23N5/20

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