US2044113A - Internal combustion engine - Google Patents
Internal combustion engine Download PDFInfo
- Publication number
- US2044113A US2044113A US478460A US47846030A US2044113A US 2044113 A US2044113 A US 2044113A US 478460 A US478460 A US 478460A US 47846030 A US47846030 A US 47846030A US 2044113 A US2044113 A US 2044113A
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- US
- United States
- Prior art keywords
- engine
- air
- fuel
- manifold
- jet
- 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
- 238000002485 combustion reaction Methods 0.000 title description 10
- 239000000446 fuel Substances 0.000 description 24
- 239000007858 starting material Substances 0.000 description 11
- 238000010438 heat treatment Methods 0.000 description 8
- 239000004449 solid propellant Substances 0.000 description 8
- 238000002347 injection Methods 0.000 description 7
- 239000007924 injection Substances 0.000 description 7
- 239000003921 oil Substances 0.000 description 4
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000002000 scavenging effect Effects 0.000 description 1
- 239000007921 spray Substances 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
- F02M1/00—Carburettors with means for facilitating engine's starting or its idling below operational temperatures
-
- 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
- F02M2700/00—Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
- F02M2700/43—Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel
- F02M2700/4302—Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel whereby air and fuel are sucked into the mixture conduit
- F02M2700/434—Heating or cooling devices
- F02M2700/4342—Heating devices
Definitions
- This invention relates to Diesel engines and particularly to apparatus for heating the intake air for Diesel engines.
- One of the important features of the invention resides inthe provision of means for burning a quantity of fuel at the entrance to the intake manifold prior to and during the cranking operation of the engine.
- Another feature of the invention resides in a pump mechanism associated with the starter apparatus for providing fuel for heating the intake air for starting purposes.
- Another important feature of the invention residesin the provision of means for heating the intake air from the exhaust together with means for adding a quantity of exhaust gases to the a intake air for improving the idling operation of the engine.
- Figure ,1 is a side elevation of an engine of the Diesel type to which the present invention has been applied, certain parts being shown in section;
- Figure 2 is a front elevation of the engine showing certain parts in section.
- Diesel engines of the solid fuel injection type, and other types, when used in the smaller sizes for such purposes as on automotive equipment are sometimes found difllcult to start in extremely cold weather, for the heat necessary for igniting the fuel in an engine operating on the Diesel cycle must come from the compression of .the air in the cylinders.
- Starting with a completely cold motor means that a great quantity jof the heat imparted to the air during the compression stroke is dissipated by radiation to the cold metal of the cylinders and pistons.
- cordance with the present invention means are provided to preheat the air for starting purposes prior to its entrance to the cylinders to make up to a large extent radiation.
- This invention includes means for heating the air, from the exhaust of the engine, and for mixing with the air controlled quantities of the exhaust products.
- the invention has, in the present instance, been illustrated in. connection with a Diesel engine oi the air-cooled type having radial cylinfor the heat lost by this mixing with the incoming ders such as used for aircraft.
- the engine may be of the standand two valve type wherein air alone is admitted through the intake valve and the exhaust products vented through the exhaust valve or it may be of the less conventional single valve type wherein one valve performs the dual function of controlling the air inlet and the scavenging. In this latter case; owing to the manifolding required a selector valve is necessary for each cylinder to prevent the exhaust products from; entering the intake manifold and vice versa. Since both "of these features are well known, they have not been illustrated more than conventionally in the drawings.
- the engine will be seen to comprise essentially a central or crank case portion it of barrel formation supporting the radial cylinders ll provided with fins for air cooling.
- the valve-in-the-head type of cylinder is used and' the valve operating in suitable stream lined chambers II from which the exhaust products are conducted,- by either of the valve arrangements previously mentioned.
- the mechanism is housed 1 to the individual exhaust pips ll. Air is conducted to each cylinder through an individual air intake pipe IS.
- the exhaust pipes ll all lead into a ring shaped exhaust manifold II which is provided with a tail pipe 18 for conducting theexhaust products beneath the insilage of the airplane.
- the intake pipes]! are similarly connected to ;a ring shaped inlet manifold 20 on the front of the engine and just behind the propeller 2
- This manifold is provided with a depending inlet pipe 22 which is bent forward to provide the scoop portion 23 in the slip stream.
- the portion 22 enters the manifold between the junca manner fully described in the patent to Iansing, No. 1,739,469.
- such a starter comprises a small fly wheel element adapted to be brought up to speed by means of an electric motor 28 or a hand crank on the end of the shaft 21 and that after this fly wheel has been brought 'up to speed it is connected through a train of reducing gears and a manually operable clutch to the shaft of the engine and turns over the engine until the energy of the fly wheel is dissipated.
- This form of starter is particularly valuable for the present invention for it operates from 10 to 20 seconds prior to the cranking while the fly wheel is being brought up to speed and continues to operate during the cranking operation.
- the shaft 21 for the hand cranking operation rotates at a fairly low speed and is made use of to supply fuel to a jet 30 in the air inlet pipe 22, which is burned upon coming in contact with the incandescent element 3
- the jet is directed upwardly so that atomized fuel strikes the plug and is ignited and heats the air in the intake manifold both prior to and during the cranking operation and at the same time dilutes it with certain products of combustion. This ensures quick and easy starting.
- Fuel oil of the type used in the engine is supplied to the pipe 33 leading to the jet by means of a plunger pump 'il actuated by the cam 35 on the shaft 21 of the starter.
- This pump may comprise a simple plunger 38 operating in the cylinder 31 which is supplied with oil under low pressure through the pipe 38 and inlet 39
- the plunger When the plunger is in the position shown in the drawings, oil flows into the space above the piston or plunger and as the cam lifts the plunger and it closes oil the inlet 39, the oil is forced through the check valves ll and into the pipe 33.
- the plunger is returned by means of the helical spring ll.
- a coaxial tube 50 is arranged within the air intake manifold 20 and is connected at the top by means of a pipe 5
- the tube 50 is provided with an outlet in the form of a neck 53 concentric within the inlet portion 22 of the air manifold.
- This neck is provided with a butterfly throttle valve 54 controlled by means of a shaft 55 and operating crank 56.
- the butterfly valve I 54 is opened the desired amount during idling to permit a flow of exhaust products through the tube 50 due not only to the pressure in the exhaust manifold but also to the aspirator action of the air.
- the quantity of exhaust products flowing through the tube 50 and into the intake manifold is regulated by the position of the butterfly valve so that not only is the air heated by contact with the surface of the tube 1 50 but it is also given a certain quantity of heat by the mixing of the exhaust products therewith so that the engine can be operated satisfactorily at idling and at low speeds.
- an air intake manifold for a plurality of cylinders an entrance duct for said manifold through which all the air to the cylinders passes during normal operation of the engine, a fuel burner jet directly in said duct and means to supply fuel to said jet automatically only prior to and during cranking of said engine.
- a manifold for a plurality of cylinders to supply air only, a fuel jet in said manifold, means in said manifold to ignite fuel from the jet therein, a starter for said engine, a fuel pump to supply fuel to said jet and means to actuate said pump from said starter only.
- Diesel engine of the solid fuel injection type in combination, an intake pipe for all the air to the cylinders, means to spray fuel into said intake pipe during cranking of the engine, means to ignite the fuel in the intake pipe and means to simultaneously inject solid fuel into the cylinders.
- a main air intake duct for the cylinders for the cylinders, a fuel jet directly in said duct, an impulse starter for said engine, means actuated by said starter to eject fuel from said jet prior to cranking the engine and means to ignite the fuel in said duct.
- an air inlet manifold for the cylinders having an entrance duct, a fuel jet in said duct, a glow plug positioned to ignite fuel issuing from said jet, an impulse starter for said engine having a rotatable inertia element, a pump to supply fuel to said jet and means to drive the pump from the inertia element of said starter while it is attaining speed and during the cranking of the engine.
- an air intakepassage to provide all of the air to the cylinders during'normal and starting operations of the engine, means to supply some of the fuel regularly used by the engine to said passage, and means to burn said fuel directly and entirely in said passage by combination with a portion of said air, prior to and during cranking of the engine to start the same.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
June 16, 1936. 1.. M. WOOLSON INTERNAL COMBUSTION ENGINE Filed Aug. 28, 1930 2 Sheets-Sheet l 3 nw ntoz June 16, 1936- 1.. M. WOOLSON INTERNAL COMBUSTION ENGINE Filed Aug. 28, 1930 2 Sheets-Sheet 2 lbum, 5
Patented June 16, 1936 UNITED STATES PATENT OFFICE 2,044,113 INTERNAL COMBUSTION ENGINE field Village, Mich Car Company, Michigan late .08 Detroi execntrlx, Bloom- Paekard Motor Application August 28. 1930, Serial No. 4'l8, 460
'lclalml.
This invention relates to Diesel engines and particularly to apparatus for heating the intake air for Diesel engines.
It is a general object of the present invention to provide novel means for heating the intake air for Diesel engines.
More particularly it is an object of the invention to provide means for heating the intake air for Diesel engines prior to and during the cranking operation and during idling or low speed running.
One of the important features of the invention resides inthe provision of means for burning a quantity of fuel at the entrance to the intake manifold prior to and during the cranking operation of the engine.
Another feature of the invention resides in a pump mechanism associated with the starter apparatus for providing fuel for heating the intake air for starting purposes.
Another important feature of the invention residesin the provision of means for heating the intake air from the exhaust together with means for adding a quantity of exhaust gases to the a intake air for improving the idling operation of the engine.
Other and further features and objects of, the invention will be more apparent to those skilled in the art upon a consideration of the accompanying drawings and following specification wherein is disclosed a single exemplary embodiment oi the invention with the understanding, however, that such changes may be made therein as fall within the scope of the appended claims githout departing from the spirit of the inven- In said drawings:
Figure ,1 is a side elevation of an engine of the Diesel type to which the present invention has been applied, certain parts being shown in section; and
Figure 2 is a front elevation of the engine showing certain parts in section.
Diesel engines of the solid fuel injection type, and other types, when used in the smaller sizes for such purposes as on automotive equipment are sometimes found difllcult to start in extremely cold weather, for the heat necessary for igniting the fuel in an engine operating on the Diesel cycle must come from the compression of .the air in the cylinders. Starting with a completely cold motor means that a great quantity jof the heat imparted to the air during the compression stroke is dissipated by radiation to the cold metal of the cylinders and pistons. In a:-
cordance with the present invention, means are provided to preheat the air for starting purposes prior to its entrance to the cylinders to make up to a large extent radiation.
l'.'he idling characteristics of a Diesel engine,
it has been found, are improved by heating the incoming air and by air a quantity of the exhaust products of combustion. This invention includes means for heating the air, from the exhaust of the engine, and for mixing with the air controlled quantities of the exhaust products.
The invention has, in the present instance, been illustrated in. connection with a Diesel engine oi the air-cooled type having radial cylinfor the heat lost by this mixing with the incoming ders such as used for aircraft. For purposes of this application, the engine may be of the standand two valve type wherein air alone is admitted through the intake valve and the exhaust products vented through the exhaust valve or it may be of the less conventional single valve type wherein one valve performs the dual function of controlling the air inlet and the scavenging. In this latter case; owing to the manifolding required a selector valve is necessary for each cylinder to prevent the exhaust products from; entering the intake manifold and vice versa. Since both "of these features are well known, they have not been illustrated more than conventionally in the drawings.
'- Referring now to the drawings, the engine will be seen to comprise essentially a central or crank case portion it of barrel formation supporting the radial cylinders ll provided with fins for air cooling. In the present instance, the valve-in-the-head type of cylinder is used and' the valve operating in suitable stream lined chambers II from which the exhaust products are conducted,- by either of the valve arrangements previously mentioned.
mechanism is housed 1 to the individual exhaust pips ll. Air is conducted to each cylinder through an individual air intake pipe IS. The exhaust pipes ll all lead into a ring shaped exhaust manifold II which is provided with a tail pipe 18 for conducting theexhaust products beneath the insilage of the airplane.
The intake pipes]! are similarly connected to ;a ring shaped inlet manifold 20 on the front of the engine and just behind the propeller 2|. This manifold is provided with a depending inlet pipe 22 which is bent forward to provide the scoop portion 23 in the slip stream. The portion 22 enters the manifold between the junca manner fully described in the patent to Iansing, No. 1,739,469. Briefly, it may be stated, that such a starter comprises a small fly wheel element adapted to be brought up to speed by means of an electric motor 28 or a hand crank on the end of the shaft 21 and that after this fly wheel has been brought 'up to speed it is connected through a train of reducing gears and a manually operable clutch to the shaft of the engine and turns over the engine until the energy of the fly wheel is dissipated. This form of starter is particularly valuable for the present invention for it operates from 10 to 20 seconds prior to the cranking while the fly wheel is being brought up to speed and continues to operate during the cranking operation. The shaft 21 for the hand cranking operation rotates at a fairly low speed and is made use of to supply fuel to a jet 30 in the air inlet pipe 22, which is burned upon coming in contact with the incandescent element 3| of a glow plug 3! suitably connected in circuit with the starting battery to glow during the starting operation. 'The jet is directed upwardly so that atomized fuel strikes the plug and is ignited and heats the air in the intake manifold both prior to and during the cranking operation and at the same time dilutes it with certain products of combustion. This ensures quick and easy starting.
Fuel oil of the type used in the engine is supplied to the pipe 33 leading to the jet by means of a plunger pump 'il actuated by the cam 35 on the shaft 21 of the starter. This pump may comprise a simple plunger 38 operating in the cylinder 31 which is supplied with oil under low pressure through the pipe 38 and inlet 39 When the plunger is in the position shown in the drawings, oil flows into the space above the piston or plunger and as the cam lifts the plunger and it closes oil the inlet 39, the oil is forced through the check valves ll and into the pipe 33. The plunger is returned by means of the helical spring ll.
It will be obvious that .the apparatus just described functions only during the starting operation and is not satisfactory for maintaining heated air in the intake manifold during idling or slow speed nmning. This latter heating can be effected by making use of the heat in the exhaust of the engine. For this purpose a coaxial tube 50 is arranged within the air intake manifold 20 and is connected at the top by means of a pipe 5| to the exhaust manifold at 52. At the lower side the tube 50 is provided with an outlet in the form of a neck 53 concentric within the inlet portion 22 of the air manifold. This neck is provided with a butterfly throttle valve 54 controlled by means of a shaft 55 and operating crank 56.
In the use of this device the butterfly valve I 54 is opened the desired amount during idling to permit a flow of exhaust products through the tube 50 due not only to the pressure in the exhaust manifold but also to the aspirator action of the air. The quantity of exhaust products flowing through the tube 50 and into the intake manifold is regulated by the position of the butterfly valve so that not only is the air heated by contact with the surface of the tube 1 50 but it is also given a certain quantity of heat by the mixing of the exhaust products therewith so that the engine can be operated satisfactorily at idling and at low speeds.
Having thus described the invention, what is claimed as new and desired to be secured by Letters Patents is:
1. In an internal combustion engine, in combination, an air intake manifold for a plurality of cylinders, an entrance duct for said manifold through which all the air to the cylinders passes during normal operation of the engine, a fuel burner jet directly in said duct and means to supply fuel to said jet automatically only prior to and during cranking of said engine.
2. In an internal combustion engine of the solid fuel injection Diesel type, in combination,
- a manifold for a plurality of cylinders to supply air only, a fuel jet in said manifold, means in said manifold to ignite fuel from the jet therein, a starter for said engine, a fuel pump to supply fuel to said jet and means to actuate said pump from said starter only.
3. In 8. Diesel engine of the solid fuel injection type, in combination, an intake pipe for all the air to the cylinders, means to spray fuel into said intake pipe during cranking of the engine, means to ignite the fuel in the intake pipe and means to simultaneously inject solid fuel into the cylinders.
4. In an internal combustion engine of the solid fuel injection type, in combination, a main air intake duct for the cylinders, a fuel jet directly in said duct, an impulse starter for said engine, means actuated by said starter to eject fuel from said jet prior to cranking the engine and means to ignite the fuel in said duct.
5. In a multi-cylindered solid fuel injection type Diesel engine, in combination, an air inlet manifold for the cylinders having an entrance duct, a fuel jet in said duct, a glow plug positioned to ignite fuel issuing from said jet, an impulse starter for said engine having a rotatable inertia element, a pump to supply fuel to said jet and means to drive the pump from the inertia element of said starter while it is attaining speed and during the cranking of the engine.
6. In a Diesel engine of the solid fuel injection type, in combination, an inlet pipe for all the air supplied to the cylinders, a fuel jet in said pipe, jet to burn only in said air and in said pipe, a starter for said engine having a part which moves before and during the actual cranking of the engine and a pump driven by said part to supply fuel to said jet.
7. In an internal combustion engine of the solid fuel injection type, in combination, an air intakepassage to provide all of the air to the cylinders during'normal and starting operations of the engine, means to supply some of the fuel regularly used by the engine to said passage, and means to burn said fuel directly and entirely in said passage by combination with a portion of said air, prior to and during cranking of the engine to start the same.
EMMA F. WOOLSON, Executrz'a: of. the Estate of Lionel M. Woolson,
Deceased.
means to ignite fuel issuing from said
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US478460A US2044113A (en) | 1930-08-28 | 1930-08-28 | Internal combustion engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US478460A US2044113A (en) | 1930-08-28 | 1930-08-28 | Internal combustion engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2044113A true US2044113A (en) | 1936-06-16 |
Family
ID=23900033
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US478460A Expired - Lifetime US2044113A (en) | 1930-08-28 | 1930-08-28 | Internal combustion engine |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2044113A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2700945A (en) * | 1950-11-17 | 1955-02-01 | Harold S Hill | Combined humidifier and preheater of air for combustion apparatus |
| US2904028A (en) * | 1955-06-14 | 1959-09-15 | Maschf Augsburg Nuernberg Ag | Preheating apparatus for internal-combustion engines |
| US3335710A (en) * | 1965-03-09 | 1967-08-15 | Gen Motors Corp | Diesel engine flame primer |
| US3400699A (en) * | 1966-06-08 | 1968-09-10 | Ford Motor Co | Preheater unit for an internal combustion engine |
| US3794007A (en) * | 1971-03-27 | 1974-02-26 | Daimler Benz Ag | Process and apparatus for multi-fuel operation of an air-compressing and auto-igniting injection internal combustion engine |
| US4957072A (en) * | 1988-11-28 | 1990-09-18 | Goldowsky Michael P | Balanced radial engine |
| US5003935A (en) * | 1988-11-28 | 1991-04-02 | Goldowsky Michael P | Balanced radial engine |
| US6769384B2 (en) | 2001-07-07 | 2004-08-03 | Thomas J. Dougherty | Radial internal combustion engine with floating balanced piston |
-
1930
- 1930-08-28 US US478460A patent/US2044113A/en not_active Expired - Lifetime
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2700945A (en) * | 1950-11-17 | 1955-02-01 | Harold S Hill | Combined humidifier and preheater of air for combustion apparatus |
| US2904028A (en) * | 1955-06-14 | 1959-09-15 | Maschf Augsburg Nuernberg Ag | Preheating apparatus for internal-combustion engines |
| US3335710A (en) * | 1965-03-09 | 1967-08-15 | Gen Motors Corp | Diesel engine flame primer |
| US3400699A (en) * | 1966-06-08 | 1968-09-10 | Ford Motor Co | Preheater unit for an internal combustion engine |
| US3794007A (en) * | 1971-03-27 | 1974-02-26 | Daimler Benz Ag | Process and apparatus for multi-fuel operation of an air-compressing and auto-igniting injection internal combustion engine |
| US4957072A (en) * | 1988-11-28 | 1990-09-18 | Goldowsky Michael P | Balanced radial engine |
| US5003935A (en) * | 1988-11-28 | 1991-04-02 | Goldowsky Michael P | Balanced radial engine |
| US6769384B2 (en) | 2001-07-07 | 2004-08-03 | Thomas J. Dougherty | Radial internal combustion engine with floating balanced piston |
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