CN200950088Y - Novel device for testing temperature field of combustion chamber - Google Patents

Novel device for testing temperature field of combustion chamber Download PDF

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Publication number
CN200950088Y
CN200950088Y CN200620092990.7U CN200620092990U CN200950088Y CN 200950088 Y CN200950088 Y CN 200950088Y CN 200620092990 U CN200620092990 U CN 200620092990U CN 200950088 Y CN200950088 Y CN 200950088Y
Authority
CN
China
Prior art keywords
whirligig
cone section
cover plate
sleeve
thermopair
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
CN200620092990.7U
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Chinese (zh)
Inventor
金成海
赵强
赵鹏
杨志民
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AVIC Shenyang Engine Design and Research Institute
Original Assignee
AVIC Shenyang Engine Design and Research Institute
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
Application filed by AVIC Shenyang Engine Design and Research Institute filed Critical AVIC Shenyang Engine Design and Research Institute
Priority to CN200620092990.7U priority Critical patent/CN200950088Y/en
Application granted granted Critical
Publication of CN200950088Y publication Critical patent/CN200950088Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model provides a burning room temperature field testing device with a gas channel formed from an external and an inner sleeves 1, 3, and an external and an internal cone sections 2, 4; a thermal couple 5 is arranged at the entrance, a revolving device 14 is positioned in the inner sleeve 3. The thermal couple 5 is inserted into the revolving device 14 and fixed by a screw and connected with a compensation lead wire by a pin; the revolving device 14 is driven by the motor mechanism 6 on the outer sleeve 1 through the drive mechanism; the drive mechanism 7 goes through the cooling channel 8, the outside end is provided with a position display device 9 and an angle sensor 10, the inside end is provided with a pressed limiting device 11, the outer and inner sleeves 1, 3, the external and internal cone sections 2, 4 and the revolving device 14 having a cooling channel; the cooling air is filled into the inner sleeve 3 and the internal cone section 4, the device is characterized in that the vertical pipe of the revolving device 14 has an arc chute 15 and a cover plate 16, the arch chute 15 and the cover plate 16 form a cooling air channel and the cooling water channel is arranged outside the arc chute 15. The device has the advantages of easy removal, energy saving and relief of labor intensity.

Description

A kind of new combustion chamber temperature field test device
Technical field
The utility model relates to the temperature field test technology.
Background technology
Chamber temperature field measurement thermopair is the main survey instrument that is used for checking the temperature field functional reliability, because the measuring section structure is very complicated, adopted gas, water dual-cooled mode, also comprise complicated rotation and gear train, make the installation difficulty of detector probe thermopair bigger, need be with the big decomposition of measuring section, progressively remove the outer cone section, the inner cone section, motor drive mechanism, gear train, after compressing parts such as stop means, after whirligig moved forward to correct position along horizontal axis, back out screw, open the cover plate of whirligig front end, pull up the contact pin of thermopair, could extract thermopair out from compensating wire.Generally speaking, 4 thermopairs are installed on the whirligig.The order that thermopair is installed is just in time opposite, the mounting or dismounting working time is longer, each approximately 3 hours times spent, make the workload of changing thermopair in the test heavy, and per hour 10,000 kilowatts of power consumptions in the process of the test, cause very big energy dissipation, in the period of test mission anxiety, even the scheduling of influence test.
Summary of the invention
The purpose of this utility model is to provide a kind of chamber temperature field test device of being convenient to install thermopair.
The utility model provides a kind of new combustion chamber temperature field test device, by outer sleeve 1, outer cone section 2, inner sleeve 3 and inner cone section 4 constitute blast tube, thermopair 5 is settled in the blast tube porch, inner sleeve is equipped with whirligig 14 for 3 li, thermopair 5 is inserted in 14 li of whirligigs, be screwed, and be connected with compensating wire with contact pin at the axle center part of whirligig 14, whirligig 14 is driven through gear train 7 by the motor drive mechanism 6 that is contained on the outer sleeve 1, gear train 7 passes measurement, cooling, transmission cavity 8, lever position indicator 9 and angular transducer 10 are equipped with in gear train 7 outer ends, gear train 7 inner ends are equipped with and are compressed stop means 11, outer sleeve 1, outer cone section 2, inner sleeve 3, inner cone section 4 and whirligig 14 all are provided with cooling water channel, inner sleeve 3 and inner cone section are connected with cold gas for 4 li, outer sleeve 1 front end has joint flange, it is characterized in that: the standpipe of described whirligig 14 front portions partly is provided with arc-shaped partition 15 and cover plate 16, arc-shaped partition 15 forms the cold gas cavity that detector probe is installed with cover plate 16, is the chilled water cavity outside the arc-shaped partition 15.During work, the thermopower that thermopair records is exported by transfer wire through compensating wire.Change at needs under the situation of thermopair 5 and back out screw, open cover plate 16, open the closing disk 13 of whirligig 14 front ends, pull up the contact pin of thermopair, just can take out thermopair 5, and not need measuring section is decomposed greatly from compensating wire.
The new combustion chamber temperature field test device that the utility model provides, its arc-shaped partition 15 can be circular with the cold gas cavity that cover plate 16 forms, air-flow is unobstructed.
The new combustion chamber temperature field test device that the utility model provides, its advantage is: be convenient to dismounting, the dismounting time of thermopair 5 is reduced to 1 hour from original 3 hours, saved a large amount of energy (per hour power saving is 10,000 kilowatts), alleviated tradesman's labour intensity.
Description of drawings
Fig. 1 is the structural representation of this chamber temperature field test device,
Fig. 2 is the structural representation of this chamber temperature field test device whirligig,
Fig. 3 is the structural representation (side view) of this chamber temperature field test device whirligig,
Fig. 4 is the M-M sectional view of this chamber temperature field test device whirligig.
Embodiment
Embodiment 1
New combustion chamber temperature field test device, its structure as shown in Figure 1, by outer sleeve 1, outer cone section 2, inner sleeve 3 and inner cone section 4 constitute blast tube, thermopair 5 is settled in the blast tube porch, inner sleeve is equipped with whirligig 14 for 3 li, the standpipe of whirligig 14 front portions partly is provided with arc-shaped partition 15 and cover plate 16 (seeing Fig. 2~4), arc-shaped partition 15 forms the circular cold gas cavity that thermopair is installed with cover plate 16, outside the arc-shaped partition 15 is the chilled water cavity, thermopair 5 is inserted in 14 li of whirligigs, be screwed on whirligig 14 and cover plate 16, and be connected with compensating wire with contact pin at the axle center part of whirligig 14, whirligig 14 thermopairs 5 are inserted in the detector probe of whirligig 14, and fix with contact pin, whirligig 14 is contained in 3 li of inner sleeves, drive through gear train 7 by the motor drive mechanism 6 that is contained on the outer sleeve 1, gear train 7 passes measurement, cooling, transmission cavity 8, lever position indicator 9 and angular transducer 10 are equipped with in gear train 7 outer ends, gear train 7 inner ends are equipped with and are compressed stop means 11, outer sleeve 1, outer cone section 2, inner sleeve 3, inner cone section 4 and whirligig 14 all are provided with cooling water channel, and inner sleeve 3 and inner cone section are connected with cold gas for 4 li.
During work, the thermopower that thermopair records is exported by transfer wire through compensating wire.
Change at needs under the situation of thermopair 5, back out screw, pull down cover plate 16, open the cover plate 13 of whirligig 14 front ends, pull up the contact pin of thermopair, just can take out thermopair 5, and not need measuring section is decomposed greatly from compensating wire.

Claims (2)

1, a kind of new combustion chamber temperature field test device, by outer sleeve (1), outer cone section (2), inner sleeve (3) and inner cone section (4) constitute blast tube, thermopair (5) is settled in the blast tube porch, whirligig (14) is equipped with in inner sleeve (3) lining, thermopair (5) is inserted in whirligig (14) lining, be screwed, and be connected with compensating wire with contact pin at the axle center part of whirligig (14), whirligig (14) is driven through gear train (7) by the motor drive mechanism (6) that is contained on the outer sleeve (1), gear train (7) passes measurement, cooling, transmission cavity (8), lever position indicator (9) and angular transducer (10) are equipped with in gear train (7) outer end, gear train (7) inner end is equipped with and is compressed stop means (11), outer sleeve (1), outer cone section (2), inner sleeve (3), inner cone section (4) and whirligig (14) all are provided with cooling water channel, inner sleeve (3) and inner cone section (4) lining are connected with cold gas, outer sleeve (1) front end has joint flange, it is characterized in that: the anterior standpipe of described whirligig (14) partly is provided with arc-shaped partition (15) and cover plate (16), arc-shaped partition (15) forms the cold gas cavity that thermopair is installed with cover plate (16), and arc-shaped partition (15) is outer to be the chilled water cavity.
2, according to the described new combustion chamber temperature field test of claim 1 device, it is characterized in that: described arc-shaped partition (15) is circular with the cold gas cavity that cover plate (16) forms.
CN200620092990.7U 2006-08-30 2006-08-30 Novel device for testing temperature field of combustion chamber Expired - Fee Related CN200950088Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN200620092990.7U CN200950088Y (en) 2006-08-30 2006-08-30 Novel device for testing temperature field of combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN200620092990.7U CN200950088Y (en) 2006-08-30 2006-08-30 Novel device for testing temperature field of combustion chamber

Publications (1)

Publication Number Publication Date
CN200950088Y true CN200950088Y (en) 2007-09-19

Family

ID=38892627

Family Applications (1)

Application Number Title Priority Date Filing Date
CN200620092990.7U Expired - Fee Related CN200950088Y (en) 2006-08-30 2006-08-30 Novel device for testing temperature field of combustion chamber

Country Status (1)

Country Link
CN (1) CN200950088Y (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103674302A (en) * 2012-09-14 2014-03-26 贵航发动机设计研究所 Rotating device for measuring fuel-gas temperature field
CN105300545A (en) * 2015-09-25 2016-02-03 中国航空工业集团公司沈阳发动机设计研究所 Engine combustion chamber outlet temperature field test device
CN105466598A (en) * 2015-11-17 2016-04-06 北京动力机械研究所 Rotating temperature measurement device used for measuring miniature combustor outlet temperature field
CN109555600A (en) * 2018-10-29 2019-04-02 中国航发贵阳发动机设计研究所 Aeroengine combustor buring room outlet temperature field rotary measurement device
CN109738193A (en) * 2019-01-08 2019-05-10 哈尔滨电气股份有限公司 Gas-turbine combustion chamber test measures segment structure with air-cooled type
CN110763475A (en) * 2018-07-26 2020-02-07 中国航发商用航空发动机有限责任公司 Measuring section of combustion chamber test equipment and combustion chamber test equipment
CN113739939A (en) * 2021-08-31 2021-12-03 中国航发贵阳发动机设计研究所 Total temperature probe for outlet of combustion chamber

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103674302A (en) * 2012-09-14 2014-03-26 贵航发动机设计研究所 Rotating device for measuring fuel-gas temperature field
CN105300545A (en) * 2015-09-25 2016-02-03 中国航空工业集团公司沈阳发动机设计研究所 Engine combustion chamber outlet temperature field test device
CN105466598A (en) * 2015-11-17 2016-04-06 北京动力机械研究所 Rotating temperature measurement device used for measuring miniature combustor outlet temperature field
CN110763475A (en) * 2018-07-26 2020-02-07 中国航发商用航空发动机有限责任公司 Measuring section of combustion chamber test equipment and combustion chamber test equipment
CN110763475B (en) * 2018-07-26 2021-07-06 中国航发商用航空发动机有限责任公司 Measuring section of combustion chamber test equipment and combustion chamber test equipment
CN109555600A (en) * 2018-10-29 2019-04-02 中国航发贵阳发动机设计研究所 Aeroengine combustor buring room outlet temperature field rotary measurement device
CN109555600B (en) * 2018-10-29 2022-03-04 中国航发贵阳发动机设计研究所 Rotary measuring device for outlet temperature field of combustion chamber of aero-engine
CN109738193A (en) * 2019-01-08 2019-05-10 哈尔滨电气股份有限公司 Gas-turbine combustion chamber test measures segment structure with air-cooled type
CN109738193B (en) * 2019-01-08 2021-04-06 哈尔滨电气股份有限公司 Air-cooled measuring section structure for gas turbine combustion chamber test
CN113739939A (en) * 2021-08-31 2021-12-03 中国航发贵阳发动机设计研究所 Total temperature probe for outlet of combustion chamber

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C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20070919

Termination date: 20140830

EXPY Termination of patent right or utility model