CN103321752B - A kind ofly to rinse and the autonomous device of oil sealing for combustion gas turbine oil system - Google Patents
A kind ofly to rinse and the autonomous device of oil sealing for combustion gas turbine oil system Download PDFInfo
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- CN103321752B CN103321752B CN201310193256.4A CN201310193256A CN103321752B CN 103321752 B CN103321752 B CN 103321752B CN 201310193256 A CN201310193256 A CN 201310193256A CN 103321752 B CN103321752 B CN 103321752B
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- oil
- purifier
- fuel tank
- oil purifier
- gas turbine
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- Turbine Rotor Nozzle Sealing (AREA)
- Lubricants (AREA)
Abstract
Rinse and the autonomous device of oil sealing for combustion gas turbine oil system, comprise four oil purifiers, solenoid valve, electric control system, two oil pumps, fuel tank, sampling cock; Wherein: the first oil purifier is connected with fuel tank by the first oil pump, first oil purifier is connected with the second oil purifier, second oil purifier is connected with the 4th oil purifier by solenoid valve, 3rd oil purifier is connected with fuel tank by sampling cock, 4th oil purifier is connected with fuel tank by the second oil pump, electric control system is connected with solenoid valve, the second oil pump and the first oil pump respectively, and workpiece is arranged in fuel tank top.Advantage of the present invention: under the bar not decomposing turbo-starter is shown in, the various turbo-starter of complete machine state is cleaned, under separate state, turbo-starter is cleaned, the oil system of continual maintenance starter motor part can clean, reduce starter motor oil system and pollute impact on engine oil system turbidity test.
Description
Technical field
The present invention relates to small gas turbine lubricating oil cleaning equipment field, particularly a kind ofly to rinse for combustion gas turbine oil system and the autonomous device of oil sealing.
Background technique
Small gas turbine, be the widely used a kind of auxiliary power unit of aviation field, in using process, often occur oil system pollution problem, market there is no available independent flushing equipment, manufactory can only be returned repair, add very large sending to applying unit and accomplish this.
Summary of the invention
The object of the invention is to rinse the oil system of small gas turbine for the convenience of the users, spy provides and a kind ofly to rinse and the autonomous device of oil sealing for combustion gas turbine oil system.
The invention provides and a kind ofly to rinse and the autonomous device of oil sealing for combustion gas turbine oil system, it is characterized in that: described to rinse for combustion gas turbine oil system and the autonomous device of oil sealing, comprise the first oil purifier 1, second oil purifier 2,3rd oil purifier 3,4th oil purifier 4, solenoid valve 5, electric control system 6, second oil pump 7, fuel tank 8, sampling cock 9, the first oil pump 10;
Wherein: the first oil purifier 1 is connected with fuel tank 8 by the first oil pump 10, first oil purifier 1 is connected with the second oil purifier 2, second oil purifier 2 is connected with the 4th oil purifier 4 by solenoid valve 5,3rd oil purifier 3 is connected with fuel tank 8 by sampling cock 9,4th oil purifier 4 is connected with fuel tank 8 by the second oil pump 7, electric control system 6 is connected with solenoid valve 5, second oil pump 7 and the first oil pump 10 respectively, and workpiece 11 is arranged in fuel tank 8 top.
Described rinse for combustion gas turbine oil system and the autonomous device of oil sealing, cleansing medium is the oil sealing of HP-8A aero oil.
Described the first oil purifier 1, second oil purifier 2, the 3rd oil purifier 3 and the 4th oil purifier 4 material are food-grade stainless steel 304.
Rinse and the autonomous device of oil sealing for combustion gas turbine oil system, the oil sealing of use HP-8A aero oil, as cleansing medium, is heated during work to 80 DEG C.By cascade filtration mode, make to enter 5 grade standards reached by the lubricating oil of the turbo-starter cleaned in GJB-420A.
Advantage of the present invention:
Of the present inventionly to rinse and the autonomous device of oil sealing for combustion gas turbine oil system, when there is exceeding the pollution that technical specifications specify in starter motor oil system, under the bar not decomposing turbo-starter is shown in, the various turbo-starter of complete machine state is cleaned, thus gets rid of because turbo-starter oil system pollutes the cross pollution caused engine oil system.
Clean turbo-starter under separate state, the oil system polluted isolated from main engine part oil system, meanwhile, to judgement, to search pollution sources significant.The oil system of continual maintenance starter motor part can clean, reduce starter motor oil system and pollute impact on engine oil system turbidity test.
Accompanying drawing explanation
Below in conjunction with drawings and the embodiments, the present invention is further detailed explanation:
Fig. 1 is the autonomous device theory structure schematic diagram for the flushing of combustion gas turbine oil system and oil sealing.
Embodiment
Embodiment 1
Present embodiments provide and a kind ofly to rinse and the autonomous device of oil sealing for combustion gas turbine oil system, it is characterized in that: described to rinse for combustion gas turbine oil system and the autonomous device of oil sealing, comprise the first oil purifier 1, second oil purifier 2,3rd oil purifier 3,4th oil purifier 4, solenoid valve 5, electric control system 6, second oil pump 7, fuel tank 8, sampling cock 9, the first oil pump 10;
Wherein: the first oil purifier 1 is connected with fuel tank 8 by the first oil pump 10, first oil purifier 1 is connected with the second oil purifier 2, second oil purifier 2 is connected with the 4th oil purifier 4 by solenoid valve 5,3rd oil purifier 3 is connected with fuel tank 8 by sampling cock 9,4th oil purifier 4 is connected with fuel tank 8 by the second oil pump 7, electric control system 6 is connected with solenoid valve 5, second oil pump 7 and the first oil pump 10 respectively, and workpiece 11 is arranged in fuel tank 8 top.
Described rinse for combustion gas turbine oil system and the autonomous device of oil sealing, cleansing medium is the oil sealing of HP-8A aero oil.
Described the first oil purifier 1, second oil purifier 2, the 3rd oil purifier 3 and the 4th oil purifier 4 material are food-grade stainless steel 304.
Rinse and the autonomous device of oil sealing for combustion gas turbine oil system, the oil sealing of use HP-8A aero oil, as cleansing medium, is heated during work to 80 DEG C.By cascade filtration mode, make to enter 5 grade standards reached by the lubricating oil of the turbo-starter cleaned in GJB-420A.
Embodiment 2
Present embodiments provide and a kind ofly to rinse and the autonomous device of oil sealing for combustion gas turbine oil system, it is characterized in that: described to rinse for combustion gas turbine oil system and the autonomous device of oil sealing, comprise the first oil purifier 1, second oil purifier 2,3rd oil purifier 3,4th oil purifier 4, solenoid valve 5, electric control system 6, second oil pump 7, fuel tank 8, sampling cock 9, the first oil pump 10;
Wherein: the first oil purifier 1 is connected with fuel tank 8 by the first oil pump 10, first oil purifier 1 is connected with the second oil purifier 2, second oil purifier 2 is connected with the 4th oil purifier 4 by solenoid valve 5,3rd oil purifier 3 is connected with fuel tank 8 by sampling cock 9,4th oil purifier 4 is connected with fuel tank 8 by the second oil pump 7, electric control system 6 is connected with solenoid valve 5, second oil pump 7 and the first oil pump 10 respectively, and workpiece 11 is arranged in fuel tank 8 top.
Rinse and the autonomous device of oil sealing for combustion gas turbine oil system, the oil sealing of use HP-8A aero oil, as cleansing medium, is heated during work to 80 DEG C.By cascade filtration mode, make to enter 5 grade standards reached by the lubricating oil of the turbo-starter cleaned in GJB-420A.
Claims (1)
1. one kind is rinsed and the autonomous device of oil sealing for combustion gas turbine oil system, it is characterized in that: described to rinse for combustion gas turbine oil system and the autonomous device of oil sealing, comprise the first oil purifier (1), second oil purifier (2), 3rd oil purifier (3), 4th oil purifier (4), solenoid valve (5), electric control system (6), second oil pump (7), fuel tank (8), sampling cock (9), the first oil pump (10);
Wherein: the first oil purifier (1) is connected with fuel tank (8) by the first oil pump (10), first oil purifier (1) is connected with the second oil purifier (2), second oil purifier (2) is connected with the 4th oil purifier (4) by solenoid valve (5), 3rd oil purifier (3) is connected with fuel tank (8) by sampling cock (9), 4th oil purifier (4) is connected with fuel tank (8) by the second oil pump (7), electric control system (6) respectively with solenoid valve (5), second oil pump (7) is connected with the first oil pump (10), workpiece (11) is arranged in fuel tank (8) top, described rinse for combustion gas turbine oil system and the autonomous device of oil sealing, cleansing medium is the oil sealing of HP-8A aero oil, described the first oil purifier (1), the second oil purifier (2), the 3rd oil purifier (3) and the 4th oil purifier (4) material are food-grade stainless steel 304.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310193256.4A CN103321752B (en) | 2013-05-22 | 2013-05-22 | A kind ofly to rinse and the autonomous device of oil sealing for combustion gas turbine oil system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310193256.4A CN103321752B (en) | 2013-05-22 | 2013-05-22 | A kind ofly to rinse and the autonomous device of oil sealing for combustion gas turbine oil system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103321752A CN103321752A (en) | 2013-09-25 |
| CN103321752B true CN103321752B (en) | 2015-12-23 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310193256.4A Expired - Fee Related CN103321752B (en) | 2013-05-22 | 2013-05-22 | A kind ofly to rinse and the autonomous device of oil sealing for combustion gas turbine oil system |
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| Country | Link |
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| CN (1) | CN103321752B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107188107A (en) * | 2017-06-02 | 2017-09-22 | 中国航发南方工业有限公司 | Engine oil seals car and the oil sealing method carried out using this oil seal vehicle |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103706584B (en) * | 2013-11-27 | 2015-09-16 | 沈阳黎明航空发动机(集团)有限责任公司 | A kind of engine accessory power rating casing rinses, engine accessory gearbox |
| US20150159505A1 (en) * | 2013-12-06 | 2015-06-11 | General Electric Company | Gas turbine organic acid based inter-rinse |
| CN104595034B (en) * | 2014-11-07 | 2016-02-10 | 沈阳黎明航空发动机(集团)有限责任公司 | A kind of purging method of Aero-Engine Lubrication System |
| CN114251178B (en) * | 2020-09-25 | 2023-08-08 | 中国航发商用航空发动机有限责任公司 | Gas turbine engine and oil extraction method for gas turbine engine |
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| US5499693A (en) * | 1994-04-02 | 1996-03-19 | Abb Management Ag | Method and apparatus for lubricating the bearings of a turbocharger |
| CN101392864A (en) * | 2007-09-18 | 2009-03-25 | 曼柴油机欧洲股份公司 | Device and method for cleaning lubricant and lubricant circulation system |
| CN103089454A (en) * | 2013-02-04 | 2013-05-08 | 哈尔滨东安发动机（集团）有限公司 | Digital control apparatus of micro gas turbine |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2994245B2 (en) * | 1995-09-22 | 1999-12-27 | 株式会社東芝 | Turbine oil flushing device |
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2013
- 2013-05-22 CN CN201310193256.4A patent/CN103321752B/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5499693A (en) * | 1994-04-02 | 1996-03-19 | Abb Management Ag | Method and apparatus for lubricating the bearings of a turbocharger |
| CN101392864A (en) * | 2007-09-18 | 2009-03-25 | 曼柴油机欧洲股份公司 | Device and method for cleaning lubricant and lubricant circulation system |
| CN103089454A (en) * | 2013-02-04 | 2013-05-08 | 哈尔滨东安发动机（集团）有限公司 | Digital control apparatus of micro gas turbine |
Non-Patent Citations (2)
| Title |
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| 《大流量高清洁度滑油清洗设备的研制与应用》;陈丽等;《中国海上油气》;20121031;第24卷(第5期);全文 * |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107188107A (en) * | 2017-06-02 | 2017-09-22 | 中国航发南方工业有限公司 | Engine oil seals car and the oil sealing method carried out using this oil seal vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103321752A (en) | 2013-09-25 |
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Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6 Patentee after: Chinese Hangfa Shenyang Liming Aero engine limited liability company Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6 Patentee before: Liming Aeroplane Engine (Group) Co., Ltd., Shenyang City |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151223 Termination date: 20210522 |