RU2002124800A - ANTI-CONDENSATE DEVICE FOR COMBUSTION CHAMBER FLAME SENSOR - Google Patents

ANTI-CONDENSATE DEVICE FOR COMBUSTION CHAMBER FLAME SENSOR

Info

Publication number
RU2002124800A
RU2002124800A RU2002124800/06A RU2002124800A RU2002124800A RU 2002124800 A RU2002124800 A RU 2002124800A RU 2002124800/06 A RU2002124800/06 A RU 2002124800/06A RU 2002124800 A RU2002124800 A RU 2002124800A RU 2002124800 A RU2002124800 A RU 2002124800A
Authority
RU
Russia
Prior art keywords
combustion chamber
sensor
tubular structures
flame
flame sensor
Prior art date
Application number
RU2002124800/06A
Other languages
Russian (ru)
Other versions
RU2318161C2 (en
Inventor
Алессио МИЛИАНИ
Андреа СИНЬОРИ
Original Assignee
Нуово Пиньоне Холдинг С.П.А.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from IT2001MI001948A external-priority patent/ITMI20011948A1/en
Application filed by Нуово Пиньоне Холдинг С.П.А. filed Critical Нуово Пиньоне Холдинг С.П.А.
Publication of RU2002124800A publication Critical patent/RU2002124800A/en
Application granted granted Critical
Publication of RU2318161C2 publication Critical patent/RU2318161C2/en

Links

Claims (5)

1. Противоконденсатное устройство для датчика (10) пламени камеры (12) сгорания, в котором датчик (10) расположен снаружи от камеры (12) сгорания и определяет наличие пламени при сгорании при помощи отверстия (14), выполненного в стенке указанной камеры (12), отличающееся тем, что устройство содержит, по меньшей мере, две трубчатые конструкции (22, 24), одна из которых (24) окружает другую (22) по меньшей мере частично, причем между указанными двумя конструкциями (22, 24) образовано кольцевое пространство, в котором протекает воздух.1. An anti-condensation device for the sensor (10) of the flame of the combustion chamber (12), in which the sensor (10) is located outside of the combustion chamber (12) and detects the presence of flame during combustion by means of an opening (14) made in the wall of said chamber (12) ), characterized in that the device contains at least two tubular structures (22, 24), one of which (24) surrounds the other (22) at least partially, and an annular ring is formed between the two structures (22, 24) the space in which air flows. 2. Устройство по п.1, отличающееся тем, что первая (22) из указанных трубчатых структур (22, 24) соединена с указанным отверстием (14) в камере (12) сгорания и проходит в направлении датчика (10), при этом вторая (24) из указанных трубчатых конструкций (22, 24) соединена с датчиком (10) пламени, указанная вторая конструкция (24) окружает первую конструкцию (22) вдоль большей части ее длины, за исключением района (А) вблизи отверстия (14) и района (В) вблизи датчика (10).2. The device according to claim 1, characterized in that the first (22) of these tubular structures (22, 24) is connected to the specified hole (14) in the combustion chamber (12) and passes in the direction of the sensor (10), while the second (24) of these tubular structures (22, 24) is connected to a flame sensor (10), said second structure (24) surrounds the first structure (22) along most of its length, with the exception of area (A) near the hole (14) and area (B) near the sensor (10). 3. Устройство по п.1, отличающееся тем, что указанные трубчатые конструкции (22, 24) соосны и направлены прямо в направлении пламени в камере (12) сгорания.3. The device according to claim 1, characterized in that said tubular structures (22, 24) are aligned and directed directly in the direction of the flame in the combustion chamber (12). 4. Устройство по п.1, отличающееся тем, что трубчатые конструкции (22, 24) имеют кольцевое поперечное сечение.4. The device according to claim 1, characterized in that the tubular structures (22, 24) have an annular cross section. 5. Устройство по п.1, отличающееся тем, что указанное устройство используется для камер (12) сгорания газовых турбин.5. The device according to claim 1, characterized in that the specified device is used for chambers (12) of combustion of gas turbines.
RU2002124800/06A 2001-09-18 2002-09-17 Device for protecting flame pickup of combustion chamber against formation of condensate RU2318161C2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT2001MI001948A ITMI20011948A1 (en) 2001-09-18 2001-09-18 ANTI-CONDENSATE DEVICE FOR A FLAME SENSOR OF A COMBUSTION CHAMBER
ITMI2001A001948 2001-09-18

Publications (2)

Publication Number Publication Date
RU2002124800A true RU2002124800A (en) 2004-04-10
RU2318161C2 RU2318161C2 (en) 2008-02-27

Family

ID=11448392

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2002124800/06A RU2318161C2 (en) 2001-09-18 2002-09-17 Device for protecting flame pickup of combustion chamber against formation of condensate

Country Status (9)

Country Link
US (1) US6766648B2 (en)
EP (1) EP1293729B1 (en)
JP (1) JP4105508B2 (en)
KR (1) KR100924858B1 (en)
CA (1) CA2403723C (en)
DE (1) DE60215738T2 (en)
IT (1) ITMI20011948A1 (en)
RU (1) RU2318161C2 (en)
TW (1) TWI223050B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4099665B2 (en) * 2003-09-26 2008-06-11 株式会社Ｉｈｉ Purge air flow path structure
US20070079357A1 (en) * 2005-10-04 2007-04-05 Disney Enterprises, Inc. System and/or method for role-based authorization
US10697815B2 (en) 2018-06-09 2020-06-30 Honeywell International Inc. System and methods for mitigating condensation in a sensor module
CN115199407A (en) * 2022-06-08 2022-10-18 惠州深能源丰达电力有限公司 Method for eliminating hidden danger of flame flicker of gas turbine by automatic heating

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2156035A1 (en) * 1971-11-11 1973-05-17 Fluggeraetetechnik Gmbh FLAME DETECTOR FOR DETECTING A FLAME ACCORDING TO THE PRINCIPLE OF IONIZATION OF GASES BY A FLAME
US4648711A (en) * 1984-06-08 1987-03-10 The Dow Chemical Company Sight tube assembly and sensing instrument for controlling a gas turbine
US4786188A (en) * 1986-02-27 1988-11-22 Rosemont Inc. Purge air system for a combustion instrument
US4934137A (en) * 1988-12-14 1990-06-19 Allied-Signal Inc. Temperature measurement in turbine engines
US4981088A (en) * 1990-05-14 1991-01-01 Diamond Electronics, Inc. Slag eliminator for furnace viewing system
US5226731A (en) * 1992-05-28 1993-07-13 Electric Power Research Institute Apparatus for measuring rotor exhaust gas bulk temperature in a combustion turbine and method therefor
US5421652A (en) * 1993-12-21 1995-06-06 General Electric Company Pyrometer adapter
DE19729712C1 (en) * 1997-07-11 1999-03-04 Krupp Uhde Gmbh Device for holding a probe in a thermally highly stressed apparatus
US6354733B2 (en) * 1999-01-15 2002-03-12 Ametex, Inc. System and method for determining combustion temperature using infrared emissions
ES2166312B1 (en) * 2000-02-16 2003-04-01 Invest Y Cooperacion Ind De An SYSTEM FOR OPTIMIZATION OF COMBUSTION PROCESSES BY DIRECT MEASURES INSIDE THE HOME.

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