US2068678A - Injection valve tip - Google Patents
Injection valve tip Download PDFInfo
- Publication number
- US2068678A US2068678A US5877A US587735A US2068678A US 2068678 A US2068678 A US 2068678A US 5877 A US5877 A US 5877A US 587735 A US587735 A US 587735A US 2068678 A US2068678 A US 2068678A
- Authority
- US
- United States
- Prior art keywords
- tip
- fuel
- orifices
- valve
- injection valve
- 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 - Lifetime
Links
- 238000002347 injection Methods 0.000 title description 8
- 239000007924 injection Substances 0.000 title description 8
- 239000000446 fuel Substances 0.000 description 19
- 229910000831 Steel Inorganic materials 0.000 description 7
- 239000010959 steel Substances 0.000 description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- 229910052799 carbon Inorganic materials 0.000 description 6
- 238000002485 combustion reaction Methods 0.000 description 4
- 239000003921 oil Substances 0.000 description 4
- 229910000906 Bronze Inorganic materials 0.000 description 2
- 239000010974 bronze Substances 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 238000000889 atomisation Methods 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 150000001721 carbon Chemical class 0.000 description 1
- 229910021386 carbon form Inorganic materials 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 229910021385 hard carbon Inorganic materials 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000033001 locomotion Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 239000004071 soot Substances 0.000 description 1
- 230000007480 spreading Effects 0.000 description 1
- 238000007514 turning Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/1826—Discharge orifices having different sizes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/1846—Dimensional characteristics of discharge orifices
Definitions
- the present invention relates to valve tips for Diesel engines.
- valve tips In certain types of Diesel engines the fuel oil is injected through a nozzle at very high pressure 5 produced by suitable pumps and under the control of valve gear.
- the valve tips heretofore in common use have been made of steel and have a hollow conical tip provided with asuitable number of very small fuel metering holes drilled to through the tip to the seat for the valve stem, the holes'being opened and closed by the valve. These tips lose efficiency very rapidly on account of the clogging of'the nozzle holes, which appears to result from a carbon deposit formed by the incomplete combustion of the residual oil in the tip. The carbon forms a crust which interferes with the injection of fuel and may eventually clog the entire hole of the nozzle so that the engine does not receive the designed charge of fuel.
- the present invention contemplates the provision of injection valve tips of an improved form and operation whereby the useful life of the tip is greatly extended, the power which may be had from the engine increased, and whereby the engine speed may be controlled through much wider limits than with ordinary nozzles.
- the tip is redesigned so that the fuel passes through nozzle openings of stepped cross section.
- the inner part of the nozzle opening is drilled to the small diameter to control the quantity of fuel admitted. This very small hole leads into a larger diameter passageway through which the jet is projected.
- the invention also contemplates the disposition of the nozzles so as to produce a flatter spray than has been customary whereby an improved combustion of the fuel takes place, and to produce a cushioning effect with no appreciable rise in temperature of exhaust gases.
- FIG. 1 illustrates in section and at an enlarged scale a typical valve tip such as heretofore in use
- Fig. 2 is a fragmentary view at a still further enlarged scale showing the orifice in common use and illustrating how it is clogged by carbon;
- Fig. 3 is a view similar to Figure 1 of the preferred form of tip embodying the present invention.
- Figs. 4 and 5 are side and end elevational views of the tip shown in Figure 3; and 5 Fig. 6 is a fragmentary enlarged view through the orifice of the tip of Figure 3.
- the common valve tip of Figures 1 and 2 is in the form of a single piece of steel I! turned to the shape shown and drilled to provide a num- 10 her of orifices II, which meter the fuel and lead to a valve seat It. These orifices are opened and closed by a valve stem l3 and suitable gear not shown.
- the orifices are in the form of small holes of from 0.008 inch to 0.015 inch in diameter 15 depending on horse power of engine.
- These tips usually have a conicalpoint of an angle of about and the orifices are drilled at an angle of about 72 to with face of tip, with the result that the spray from the tip is confined into a 20 narrow cone of about 72. Examinations of tips which have seen service usually shows a heavy, hard carbon deposit or crust about the nozzle This is indicated at- I4 in Figure 2.
- the valve tip is made of two turnings.
- the outer oneor shroud I5 is of bronze which has high thermal conductivity and istherefore quickly cooled by the air taken into 40 the cylinder. It therefore expands and contracts with each cycle.
- the inner member I6 is of steel for strength. These. members are made accurately to-size so that when the steel insert is forced into the sheath the joint is oil tight.
- the 45 steel liner i5 is adapted to receive the valve stem l1 and has a seat l8 for the valve stem.
- the outer sheath is provided with a plurality of comparatively large holes, about 1 5' inch in 50 diameter as indicated at l9. These holes are preferably drilled before the steel insert is forced in place.
- the fuel orifices 20 are drilled very carefully so as to proceed fromthe centers of the larger holes. These orifices are of the proper 55 diameter for the quantity of fuel they are to supply and are preferably drilled at about 50 to the tip axis.
- the spread of the jet is therefore approximately 50" from the axis of the tip. This spreads the jets further from the axis than usual and produces a widely spreading fan-like fiame. It avoids the sudden blow to which the pistons and connected parts are usually subjected and has been found to materially reduce the noise of the engine and the wear on the bearings.
- the stepped orifice is similar to a mouthpiece or pipe having a sudden enlargement. There is sinuous flow along the pipe, the stream suddenly enlarging to fill the pipe. The fuel is, however, sprayed out without loss of volume or material loss of energy, except for eddy motions. ⁇ Vhatever fuel is left in the passage after an explosion, with any contamination by carbon, is washed away by the next charge so that clean oil is always being passed over the surfaces.
- an injection valve tip having an insert provided with small diameter orifices through which the fuel is injected into the cylinder and an outer sheath provided with means about the orifices to prevent the incomplete combustion of fuel adjacent the orifices whereby clogging of the orifices by carbon is prevented.
- a Diesel engine injection tip having an outer sheath and an insert, the insert having small diameter fuel metering passages, the sheath having co-axialperforations of substantially larger diameter to provide it with cylindrical openings which shroud and protect each of the fuel passages.
- a tip as claimed in claim 2 characterized in that the insert is of hard metal to withstand the action of the valve stem and the sheath is of a metal having a greater temperature conductivity.
- a Diesel engine injection tip having an outer bronze sheath and a steel insert, the insert having small diameter fuel metering passages, the
- sheath having co-axial performations of substantially larger diameter to provide it with cylindrical openings which shroud and protect each of the fuel passages.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Description
lam. 26, 1937. R. H. HOADLEY 2,068,673
' INJECTION VALVE TIP Filed Feb. 9, 1935 Y i=5. .El,
1H mpsbml'ron W -HodLey ATTORNEY Patented Jan. 26, 1937.
UNITED STATES PATENT OFFICE INJECTION VALVE TIP Raymond B. Hoadley, Bronx, N. Y.
Application February 9, 1935, Serial No. 5,877
' Claims. (01. 299-1071) The present invention relates to valve tips for Diesel engines.
In certain types of Diesel engines the fuel oil is injected through a nozzle at very high pressure 5 produced by suitable pumps and under the control of valve gear. The valve tips heretofore in common use have been made of steel and have a hollow conical tip provided with asuitable number of very small fuel metering holes drilled to through the tip to the seat for the valve stem, the holes'being opened and closed by the valve. These tips lose efficiency very rapidly on account of the clogging of'the nozzle holes, which appears to result from a carbon deposit formed by the incomplete combustion of the residual oil in the tip. The carbon forms a crust which interferes with the injection of fuel and may eventually clog the entire hole of the nozzle so that the engine does not receive the designed charge of fuel.
The present invention contemplates the provision of injection valve tips of an improved form and operation whereby the useful life of the tip is greatly extended, the power which may be had from the engine increased, and whereby the engine speed may be controlled through much wider limits than with ordinary nozzles.
In carrying out the invention, the tip is redesigned so that the fuel passes through nozzle openings of stepped cross section. The inner part of the nozzle opening is drilled to the small diameter to control the quantity of fuel admitted. This very small hole leads into a larger diameter passageway through which the jet is projected.
These larger holes act as a shroud or sheath and protect the orifices from clogging by carbon.
The invention also contemplates the disposition of the nozzles so as to produce a flatter spray than has been customary whereby an improved combustion of the fuel takes place, and to produce a cushioning effect with no appreciable rise in temperature of exhaust gases.
Other and further objects of the invention wi appear as the description proceeds:
The accompanying drawing shows, for purposes of illustrating the present invention, one of the many embodiments in which the invention may take form, it being understood that the drawing is illustrative of the invention rather than limiting the same. In the drawing:
Fig. 1 illustrates in section and at an enlarged scale a typical valve tip such as heretofore in use; Fig. 2 is a fragmentary view at a still further enlarged scale showing the orifice in common use and illustrating how it is clogged by carbon;
7 opening.
Fig. 3 is a view similar to Figure 1 of the preferred form of tip embodying the present invention; 1
Figs. 4 and 5 are side and end elevational views of the tip shown in Figure 3; and 5 Fig. 6 is a fragmentary enlarged view through the orifice of the tip of Figure 3.
The common valve tip of Figures 1 and 2 is in the form of a single piece of steel I!) turned to the shape shown and drilled to provide a num- 10 her of orifices II, which meter the fuel and lead to a valve seat It. These orifices are opened and closed by a valve stem l3 and suitable gear not shown. The orifices are in the form of small holes of from 0.008 inch to 0.015 inch in diameter 15 depending on horse power of engine. These tips usually have a conicalpoint of an angle of about and the orifices are drilled at an angle of about 72 to with face of tip, with the result that the spray from the tip is confined into a 20 narrow cone of about 72. Examinations of tips which have seen service usually shows a heavy, hard carbon deposit or crust about the nozzle This is indicated at- I4 in Figure 2.
It appears to come from the burning or breaking 5 down of the exposed surface of the droplet oil which is held in the orifice of the nozzle. The engine power and ease of starting andhandling is seriously impaired. Due to the clogging of the orifices the cylinders work unevenly. This pro- 30 motes a smoky exhaust due to poor and incomplete combustion. The building up of this carbon I deposit is progressive and it interferes with the discharge of the fuel, both as to quantity and its atomization. 35
In the construction of Figure 3, embodying the present improvements, the valve tip is made of two turnings. The outer oneor shroud I5 is of bronze which has high thermal conductivity and istherefore quickly cooled by the air taken into 40 the cylinder. It therefore expands and contracts with each cycle. The inner member I6 is of steel for strength. These. members are made accurately to-size so that when the steel insert is forced into the sheath the joint is oil tight. The 45 steel liner i5 is adapted to receive the valve stem l1 and has a seat l8 for the valve stem. The
end of the tip is turned to have a cone of The outer sheath is provided with a plurality of comparatively large holes, about 1 5' inch in 50 diameter as indicated at l9. These holes are preferably drilled before the steel insert is forced in place. The fuel orifices 20 are drilled very carefully so as to proceed fromthe centers of the larger holes. These orifices are of the proper 55 diameter for the quantity of fuel they are to supply and are preferably drilled at about 50 to the tip axis. The spread of the jet is therefore approximately 50" from the axis of the tip. This spreads the jets further from the axis than usual and produces a widely spreading fan-like fiame. It avoids the sudden blow to which the pistons and connected parts are usually subjected and has been found to materially reduce the noise of the engine and the wear on the bearings.
The stepped orifice is similar to a mouthpiece or pipe having a sudden enlargement. There is sinuous flow along the pipe, the stream suddenly enlarging to fill the pipe. The fuel is, however, sprayed out without loss of volume or material loss of energy, except for eddy motions. \Vhatever fuel is left in the passage after an explosion, with any contamination by carbon, is washed away by the next charge so that clean oil is always being passed over the surfaces.
Experience with the fuel tips herein described show that the engine operation is greatly improved, both as to maximum power available and flexibility of control. The exhaust gases are clear and free of smoke or soot, and the exhaust temperature low. While of general use in Diesel engines, they have been found to be of especial advantage for use on marine engines where it is important to avoid shut down for repairs, and where maneuverability of the ship is necessary.
It is obvious that the invention may be embodied in many forms and constructions within the scope of the claims, and I wish it to be understood that the particular form shown is but one of the my forms. Various modifications and changes being possible, I do not otherwise limit myself in any way with respect thereto.
What is claimed is:
1. In a Diesel engine an injection valve tip having an insert provided with small diameter orifices through which the fuel is injected into the cylinder and an outer sheath provided with means about the orifices to prevent the incomplete combustion of fuel adjacent the orifices whereby clogging of the orifices by carbon is prevented.
2. A Diesel engine injection tip having an outer sheath and an insert, the insert having small diameter fuel metering passages, the sheath having co-axialperforations of substantially larger diameter to provide it with cylindrical openings which shroud and protect each of the fuel passages.
3. A tip as claimed in claim 2, characterized in that the insert is of hard metal to withstand the action of the valve stem and the sheath is of a metal having a greater temperature conductivity.
4. A tip as claimed in claim 2, wherein the sheath perforations are approximately six times the diameter of the metering passages.
5. A Diesel engine injection tip having an outer bronze sheath and a steel insert, the insert having small diameter fuel metering passages, the
sheath having co-axial performations of substantially larger diameter to provide it with cylindrical openings which shroud and protect each of the fuel passages.
RAYMOND H. noarinn r.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US5877A US2068678A (en) | 1935-02-09 | 1935-02-09 | Injection valve tip |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US5877A US2068678A (en) | 1935-02-09 | 1935-02-09 | Injection valve tip |
Publications (1)
Publication Number | Publication Date |
---|---|
US2068678A true US2068678A (en) | 1937-01-26 |
Family
ID=21718166
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US5877A Expired - Lifetime US2068678A (en) | 1935-02-09 | 1935-02-09 | Injection valve tip |
Country Status (1)
Country | Link |
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US (1) | US2068678A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2556171A (en) * | 1945-11-13 | 1951-06-12 | Harold M Dudek | Injection valve assembly |
US2639193A (en) * | 1947-02-05 | 1953-05-19 | American Bosch Corp | Fuel injection device |
WO1980000064A1 (en) * | 1978-06-14 | 1980-01-24 | Ingemanssons Ingenjorsbyra Ab | A blowing device having a low noise level |
DE3004033A1 (en) * | 1980-02-05 | 1981-08-13 | Klöckner-Humboldt-Deutz AG, 5000 Köln | DEVICE AND METHOD FOR COOLING INJECTION NOZZLE HOLES |
DE3114386A1 (en) * | 1981-04-01 | 1982-10-14 | Gebrüder Sulzer AG, 8401 Winterthur | Nozzle of a fuel injection valve for a diesel engine |
DE3113466A1 (en) * | 1981-04-03 | 1982-10-14 | Klöckner-Humboldt-Deutz AG, 5000 Köln | Method for fixing a cap on a nozzle body |
WO2003027483A1 (en) * | 2001-08-29 | 2003-04-03 | Robert Bosch Gmbh | Fuel injection valve |
-
1935
- 1935-02-09 US US5877A patent/US2068678A/en not_active Expired - Lifetime
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2556171A (en) * | 1945-11-13 | 1951-06-12 | Harold M Dudek | Injection valve assembly |
US2639193A (en) * | 1947-02-05 | 1953-05-19 | American Bosch Corp | Fuel injection device |
WO1980000064A1 (en) * | 1978-06-14 | 1980-01-24 | Ingemanssons Ingenjorsbyra Ab | A blowing device having a low noise level |
DE3004033A1 (en) * | 1980-02-05 | 1981-08-13 | Klöckner-Humboldt-Deutz AG, 5000 Köln | DEVICE AND METHOD FOR COOLING INJECTION NOZZLE HOLES |
DE3114386A1 (en) * | 1981-04-01 | 1982-10-14 | Gebrüder Sulzer AG, 8401 Winterthur | Nozzle of a fuel injection valve for a diesel engine |
DE3113466A1 (en) * | 1981-04-03 | 1982-10-14 | Klöckner-Humboldt-Deutz AG, 5000 Köln | Method for fixing a cap on a nozzle body |
WO2003027483A1 (en) * | 2001-08-29 | 2003-04-03 | Robert Bosch Gmbh | Fuel injection valve |
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