GB2032002A - A device for cleaning a turbine - Google Patents
A device for cleaning a turbine Download PDFInfo
- Publication number
- GB2032002A GB2032002A GB7933625A GB7933625A GB2032002A GB 2032002 A GB2032002 A GB 2032002A GB 7933625 A GB7933625 A GB 7933625A GB 7933625 A GB7933625 A GB 7933625A GB 2032002 A GB2032002 A GB 2032002A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- closure member
- shut
- control
- cleaning
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/002—Cleaning of turbomachines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B77/00—Component parts, details or accessories, not otherwise provided for
- F02B77/04—Cleaning of, preventing corrosion or erosion in, or preventing unwanted deposits in, combustion engines
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Cleaning By Liquid Or Steam (AREA)
- Supercharger (AREA)
- Lift Valve (AREA)
Abstract
A device for cleaning a turbine, more particularly an exhaust-gas driven turbine connected to the exhaust tail-pipe of an internal combustion engine, comprises a washing nozzle (1) disposed in the tail-pipe wall (2) and having at least one fluid inlet orifice (6) which is supplied via an internal cavity (3) in the nozzle with cleaning fluid, a shut- off valve (4) to control the quantity of fluid supplied, a closure member (7) to close off the fluid inlet orifice (6), a guide rod (8) carrying the closure member (7), a spring (11) to hold the closure member (7) in the closed position, and an electromagnetic and/or pneumatic actuated element (10) to open the guide rod and closure member against the force of the spring. <IMAGE>
Description
SPECIFICATION
A device for cleaning a turbine
This invention relates to a device for cleaning a turbine, more particularly an exhaust-gas driven turbine connected to the exhaust tail-pipe of an internal combustion engine, the device comprising a washing nozzle disposed in the tail-pipe wall and having at least one nozzle aperture which is supplied via an internal cavity in the nozzle with an amount of cleaning fluid, a shut-off valve to control the quantity of cleaning fluid supplied, a closure member to control the shut-off valve, a guide rod in operative connection with the closure member, and a spring to hold the closure member in the closed position.
In the case of a known device of this kind, there is a representation or description of an injection valve for periodically washing the turbine of an exhaust-gas driven turbosupercharger, in which a closure member in the form of a needle valve prevents sooting of the nozzle aperture. In the known device, the needle valve is connected to a piston, and when the shut-off valve is opened the cleaning fluid or detergent exerts pressure on the piston and thus raises the needle valve and sprays the fluid used for the cleaning operation. In order to end the washing process the shut-off valve is closed, so that the pressure of the detergent in the
nozzle cavity drops and the nozzle aperture is blocked by the closure member, since the force of the spring loading the piston is now greater than the pressure in the nozzle cavity.The disadvantage of the aforementioned device for cleaning a turbine is that, although the pressure in the nozzle
cavity drops after the nozzle has been shut off by the closure member, nearly the entire nozzle cavity
remains full of cleaning fluid, which begins to boil and evaporate owing to the high temperature of the tail-pipe and the washing nozzle. This results in increased corrosion of all parts of the nozzle and in deposits of lime from the water and residues of the detergent added to the water, the deposits forming particularly on the closure member and the associated actuating means. As a result of this defect, the washing nozzle becomes unserviceable after a reiatively short time in operation.
The object of the invention, therefore, is to avoid the aforementioned difficulties and thus accurately guide the washing nozzle without evaporating the cleaning fluid in the nozzle cavity.
This problem is solved according to the invention by providing a device for cleaning a turbine, more particularly an exhaust-gas driven turbine connected to the exhaust tail-pipe of an internal combustion engine, the device comprising a washing nozzle disposed in the tail-pipe wall and having at least one nozzle aperture which is supplied via an internal cavity in the nozzle with a quantity of cleaning fluid, a shut-off valve to control the quantity of fluid supplied, a closure member to control the shut-off valve, a guide rod operatively connected with the closure member, a spring to hold the closure member in the closed position, and an electromagnetic and/or pneumatic actuating element to move the guide rod against the force of the spring.
With this arrangement the nozzle cavity through which the cleaning fluid flows is separated, spatially and in operation, from the means actuating the closure member, thus avoiding problems regarding corrosion and deposits of cleaning fluid on the nozzle actuating means. The actuating element can be disposed at a location in the washing nozzle where it is protected from cleaning additives to the fluid which are corrosive, and it is not exposed to the considerable temperature fluctuations in the exhaust tail-pipe wall. In addition, since the opening and closure times of the closure member are controlled independently of the pressure of the cleaning fluid in the nozzle cavity, the cavity is completely emptied after each cleaning cycle.
The nozzle cavity can be reliably emptied as follows: The control element for the actuating element is operated in common with the shut-off valve for the cleaning fluid, but the delay element is provided for switching off the control element.
In the case of a pneumatic actuating element, the delay element can be a special arrangement of the control piston in the shut-offvalve, relative to its position in the control element. If the control element is electromagnetic, the delay can be brought about by a timing means in the form of a switch which is e.g. damped or delayed at one side.
Alternatively the closure member can be mechanically actuated, if a cable or spindle is connected to the guide rod. The closure member can be adjusted via the spindle, e.g., by means of an angular drive or flexible shaft, alternatively, in accordance with the previously-described embodiments, the closure member can be mechanically controlled in dependence on the position of the shut-off valve.
The invention will be more clearly understood from the following description, with reference to the accompanying drawings, which show two simplified embodiments of the invention. In the drawings:
Figure lisa view, half in section, of a washing nozzle according to the invention comprising a closure member in the form of a needle valve; and
Figure 2 is a view, half in section, of a washing nozzle according to the invention comprising a closure member in the form of a poppet valve.
Both Figures 1 and 2 diagrammatically show a washing nozzle 1 secured in a pocket, core, nest or the like 2 of an exhaust tail-pipe wall (not shown).
Nozzie 1 has an internal cavity 3 connected at one end by a shut-off valve 4 to a supply means for a cleaning fluid, whereas the other end opens via an aperture 6 into the interior of the tail-pipe.
Outside the cleaning periods, aperture 6 is blocked by a closure member 7 which is in operative connection with a pneumatic actuating element 9 via a guide rod 8. Element 9 comprises a pneumatic control piston 10 which is permanently connected to rod 8 and counteracts the force of a spring 11 when the closure member 7 and guide
rod 8 are in the open position. A pressure control
chamber 12 is provided on the end face of piston
10 remote from spring 11 and can be connected
by a control element 13 to a pneumatic supply
device 14.A sealing element 16 having packing
washers 1 7 is disposed between cavity 3 and
chamber 12, and a leakage oil bore 18 is formed
between washers 1 7. Valve 4 and control element 1 3 have a common switching device 15 which
couples the two multi-way valves to as to provide
a common switching point for the switchingsff valve and the control element 13, i.e., in its
position for reducing pressure in chamber 12,
compared with the switching-off of the supply of
cleaning fluid to cavity 3 by valve 4. If required,
element 13 and element 9 can be equipped for an
electric control system, in which element 13 is
constructed as an electric regulating switch and
piston 12 is replaced by a magnet armature for
electromagnetic actuation.
Nozzle 1 operates as follows:
During the washing process, cleaning fluid flows from the conveyor device 5 through the shut-off valve 4 into the nozzle cavity 3. At the same time, control element 13 is opened and pressure builds up in the pneumatic actuating element 9, thus pushing piston 10 against the force of spring 11 and opening the closure member 7. As a result, cleaning fluid flows through aperture 6 out of cavity 3 and is sprayed into the exhaust tail-pipe, thus removing combustion residues from the exhaust-gas driven turbine. At the end of the cleaning cycle, valve 4 and element 3 move to a position cutting off the supply of fluid to nozzle 1. In this position, member 7 is still open but no fluid is supplied to cavity 3, which is completely emptied. It is only after a delay that element 1 3 reaches a position in which the pressure in the control chamber is reduced, whereupon member 7 closes aperture 6.
This ensures that cavity 3 is always completely empty between washing cycles, so that cleaning fluid cannot evaporate in this region and deposits cannot form in cavity 3, member 7 or aperture 6.
In addition, element 9 is spatially and operatively separated from cavity 3, thus preventing element 9 from being damaged by corrosion or excessive heat.
Claims (6)
1. A device for cleaning a turbine, more particularly an exhaust-gas driven turbine connected to the exhaust tail-pipe of an internal combustion engine, the device comprising a washing nozzle disposed in the tail-pipe wall and having at least one nozzle aperture which is supplied via an internal cavity with a quantity of cleaning fluid, a shut-off valve to control the quantity of fluid supplied, a closure member to control the shut-off valve, a guide rod operatively connected with the closure member, a spring to hold the closure member in the closed position, and an electromagnetic and/or pneumatic actuating element to move the guide rod against the force of the spring.
2. A device according to claim 1, comprising a control piston secured to the guide rod, the control piston being spring-loaded in one direction and movable in the other direction by compressed air from a pressure control chamber connected to a source of compressed air.
3. A device according to claim 1 or claim 2, comprising a sealing element having at least two packing washers and disposed between the internal cavity and the pressure control chamber, and leakage oil bores formed between the packing washers.
4. A device according to any preceding claim, in which the shut-off valve has a switching device in common with the control element in operative connection with the actuating element.
5. A device according to claim 4, in which the switching device has a common switching-on point for the shut-off valve and the control element, whereas a delay element is provided for switching off the control element at a different time from the shut-off valve.
6. A device for cleaning a turbine, more particularly an exhaust-gas driven turbine connected to the exhaust tail-pipe of an internal combustion engine, constructed and arranged substantially as herein described, with reference to and as illustrated in the accompanying drawings.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19782842229 DE2842229A1 (en) | 1978-09-28 | 1978-09-28 | DEVICE FOR CLEANING A TURBINE |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2032002A true GB2032002A (en) | 1980-04-30 |
GB2032002B GB2032002B (en) | 1982-10-27 |
Family
ID=6050704
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7933625A Expired GB2032002B (en) | 1978-09-28 | 1979-09-27 | Device for cleaning a turbine |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE2842229A1 (en) |
FR (1) | FR2437493B1 (en) |
GB (1) | GB2032002B (en) |
NL (1) | NL7907200A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4548040A (en) * | 1984-05-11 | 1985-10-22 | Elliott Turbomachinery Company, Inc. | Method and apparatus for determining when to initiate cleaning of turbocharger turbine blades |
US5944483A (en) * | 1995-12-29 | 1999-08-31 | Asea Brown Boveri Ag | Method and apparatus for the wet cleaning of the nozzle ring of an exhaust-gas turbocharger turbine |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19821811B4 (en) * | 1998-05-15 | 2004-06-24 | Mannesmann Ag | Injector |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE244308C (en) * | ||||
FR1037550A (en) * | 1950-05-31 | 1953-09-17 | Daimler Benz Ag | Method for fuel injection using compressed air |
BE528223A (en) * | 1953-04-21 | |||
SE312273B (en) * | 1968-04-24 | 1969-07-07 | Asea Ab | |
DE1910114A1 (en) * | 1969-02-28 | 1970-09-17 | Bosch Gmbh Robert | Injection arrangement for internal combustion engines |
AT293122B (en) * | 1969-03-12 | 1971-09-27 | Semperit Ag | Valve |
DE2120213B1 (en) * | 1971-04-24 | 1972-05-25 | Man | Device for removing deposits on turbines |
FR2234796A5 (en) * | 1973-06-19 | 1975-01-17 | Semt | |
SE387720B (en) * | 1974-12-30 | 1976-09-13 | Stal Laval Turbin Ab | WASHER FOR WASH STEP COMPRESSOR |
CH615987A5 (en) * | 1976-07-23 | 1980-02-29 | Sulzer Ag | Injection valve for a turbocharger-washing device |
DE2641425A1 (en) * | 1976-09-15 | 1978-03-16 | Kloeckner Humboldt Deutz Ag | Turbine cleaning machine with liq. dispensing nozzles - has spring biased protective cover over nozzle orifices movable only by pressure of cleaning liq. |
-
1978
- 1978-09-28 DE DE19782842229 patent/DE2842229A1/en active Granted
-
1979
- 1979-09-26 FR FR7923973A patent/FR2437493B1/en not_active Expired
- 1979-09-27 NL NL7907200A patent/NL7907200A/en not_active Application Discontinuation
- 1979-09-27 GB GB7933625A patent/GB2032002B/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4548040A (en) * | 1984-05-11 | 1985-10-22 | Elliott Turbomachinery Company, Inc. | Method and apparatus for determining when to initiate cleaning of turbocharger turbine blades |
GB2158519A (en) * | 1984-05-11 | 1985-11-13 | Elliott Turbo | Method and apparatus for determining when to initiate cleaning of turbine blades |
US5944483A (en) * | 1995-12-29 | 1999-08-31 | Asea Brown Boveri Ag | Method and apparatus for the wet cleaning of the nozzle ring of an exhaust-gas turbocharger turbine |
Also Published As
Publication number | Publication date |
---|---|
FR2437493B1 (en) | 1986-01-03 |
NL7907200A (en) | 1980-04-01 |
FR2437493A1 (en) | 1980-04-25 |
DE2842229A1 (en) | 1980-05-08 |
GB2032002B (en) | 1982-10-27 |
DE2842229C2 (en) | 1990-02-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |