US1941805A - Injection engine - Google Patents
Injection engine Download PDFInfo
- Publication number
- US1941805A US1941805A US678353A US67835333A US1941805A US 1941805 A US1941805 A US 1941805A US 678353 A US678353 A US 678353A US 67835333 A US67835333 A US 67835333A US 1941805 A US1941805 A US 1941805A
- Authority
- US
- United States
- Prior art keywords
- chamber
- injection engine
- pistons
- cylinder
- passage
- 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
- 238000002485 combustion reaction Methods 0.000 description 8
- 239000000446 fuel Substances 0.000 description 8
- 239000012530 fluid Substances 0.000 description 5
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 239000000203 mixture Substances 0.000 description 2
- 238000005266 casting Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000010779 crude oil Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
Images
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
- F02B21/00—Engines characterised by air-storage chambers
Definitions
- My invention relates to a fuel injection internal combustion engine of the type which embodies an air chamber in which fluid is compressed during the compression stroke of the piston and from which the fluid issues during the working stroke of the piston.
- the purpose of the instant invention is to provide an improved construction wherein organized rotary turbulence of the mixture in the combustion chamber is secured.
- the purpose of the instant invention is to embody the above in a double-acting engine.
- Figure 2 is a horizontal sectional view taken on the plane of the line P-Q of Figure 1.
- FIG. 1 shows the pistons in the position of greatest compression, and the space between the pistons constitutes the combustion chamber 0.
- a passage- 0 way, formed in the cylinder casting, enters each side of the combustion chamber c, tangentially, as shown.
- the main axis of each of these passageways lies horizontally alongside the cylinder,
- An air storagechamber a and a fuel nozzle b is provided for each of these passageways, lying on the main axis thereof referred to.
- the air 0 chamber a is formed in a plug, which is inserted in the end of the passageway, the air chamber being thus located so that the opening therefrom is directed toward the curved part of the passageway and toward the combustion chamber, as shown.
- the fuel nozzle b is oppositely disposed, so that fuel issuing therefrom issues toward the airschamber.
- Suitable mechanism is of course provided to cause the nozzle 1) to inject fuel at the proper time in the cycle, beginning with the final com- 75 pression. This injection is into the passageways, as will be clear, and contact of crude oil with the pistons is prevented.
- the arrangement may be used for two-stroke and also for four-stroke cycle engines.
- a cylinder and a piston operating therein said cylinder having a passage opening into the cylinder through the peripheral wall and substantially tangentially thereof, said passage extending outward from the cylinder bore and substantially tangent thereto, an air storage chamber opening into the outer end of the passage through an orifice disposed to eject air into said passage lengthwise and toward the inner end thereof, and an injection nozzle opening into said passage adjacent the inner end thereof and outward beyond the cylinder bore, said nozzle being disposed to inject fuel lengthwise of the passage and toward the outer end thereof.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
Jan. 2, 1934'. LANG 1,941,805
INJECTION ENGINE Original Filed Dec. 1, 1930 J77 7/19/7201? Fa 2.2 242mg.
K 1 MW,
Patented Jan. 2, 1934 UNITED STATES PATENT OFFICE INJECTION ENGINE stein Original application December 1, 1930, Serial and in Germany December 27,
1929. Divided and this application June 30, 1933. Serial No. 678,353
1 Claim.
My invention relates to a fuel injection internal combustion engine of the type which embodies an air chamber in which fluid is compressed during the compression stroke of the piston and from which the fluid issues during the working stroke of the piston.
This application is a division of my copending application, Serial No. 499,223, filed December 1, 1930, for fuel injection internal combustion engines.
The purpose of the instant invention is to provide an improved construction wherein organized rotary turbulence of the mixture in the combustion chamber is secured.
In its more specific aspects, the purpose of the instant invention is to embody the above in a double-acting engine. I
My invention is illustrated in the accompanying drawing, in which Figure 1 is a vertical axial sectional view of those portions of the engine with which my invention is concerned; and
Figure 2 is a horizontal sectional view taken on the plane of the line P-Q of Figure 1.
The drawing shows the cylinder, and opposed pistons which reciprocate therein. Figure 1 shows the pistons in the position of greatest compression, and the space between the pistons constitutes the combustion chamber 0. A passage- 0 way, formed in the cylinder casting, enters each side of the combustion chamber c, tangentially, as shown. The main axis of each of these passageways lies horizontally alongside the cylinder,
and each of them curves inwardly to the com! bustion chamber, communicating therewith pref erably through an oblong slot, as shown.
An air storagechamber a and a fuel nozzle b is provided for each of these passageways, lying on the main axis thereof referred to. The air 0 chamber a is formed in a plug, which is inserted in the end of the passageway, the air chamber being thus located so that the opening therefrom is directed toward the curved part of the passageway and toward the combustion chamber, as shown. The fuel nozzle b is oppositely disposed, so that fuel issuing therefrom issues toward the airschamber.
The drawing shows two tangential air chamber and fuel nozzle sets, but it will be understood that more than two such sets may be provided.
Upon the compression stroke of the pistons, fluid from between the pistons is compressed in the chamber a, and upon the working stroke of the pistons this fluid issues from the chamber at high velocity, the streams of fluid being directed tangentially into the combustion space 0, as indicated by the arrows in Figure 2, thus imparting high turbulence to the mixture in the combustion space.
Suitable mechanism is of course provided to cause the nozzle 1) to inject fuel at the proper time in the cycle, beginning with the final com- 75 pression. This injection is into the passageways, as will be clear, and contact of crude oil with the pistons is prevented.
The arrangement may be used for two-stroke and also for four-stroke cycle engines.
I claim:
In combination in an injection engine, a cylinder and a piston operating therein, said cylinder having a passage opening into the cylinder through the peripheral wall and substantially tangentially thereof, said passage extending outward from the cylinder bore and substantially tangent thereto, an air storage chamber opening into the outer end of the passage through an orifice disposed to eject air into said passage lengthwise and toward the inner end thereof, and an injection nozzle opening into said passage adjacent the inner end thereof and outward beyond the cylinder bore, said nozzle being disposed to inject fuel lengthwise of the passage and toward the outer end thereof.
FRANZ LANG.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US678353A US1941805A (en) | 1930-12-01 | 1933-06-30 | Injection engine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US49922330A | 1930-12-01 | 1930-12-01 | |
US678353A US1941805A (en) | 1930-12-01 | 1933-06-30 | Injection engine |
Publications (1)
Publication Number | Publication Date |
---|---|
US1941805A true US1941805A (en) | 1934-01-02 |
Family
ID=27053080
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US678353A Expired - Lifetime US1941805A (en) | 1930-12-01 | 1933-06-30 | Injection engine |
Country Status (1)
Country | Link |
---|---|
US (1) | US1941805A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3809027A (en) * | 1972-02-28 | 1974-05-07 | Brunswick Corp | Internal combustion engine |
US4686941A (en) * | 1986-04-01 | 1987-08-18 | Sanshin Kogyo Kabushiki Kaisha | Turbulence generator for two-stroke spark-assisted diesel engines |
US4774919A (en) * | 1986-09-08 | 1988-10-04 | Yamaha Hatsudoki Kabushiki Kaisha | Combustion chamber importing system for two-cycle diesel engine |
US4913111A (en) * | 1986-04-01 | 1990-04-03 | Sanshin Kogyo Kabushiki Kaisha | Turbulence generator for two-stroker spark-assisted diesel engines |
US5111786A (en) * | 1991-05-03 | 1992-05-12 | Ford Motor Company | Air cell for an internal combustion engine |
US20090120094A1 (en) * | 2007-11-13 | 2009-05-14 | Eric Roy Norster | Impingement cooled can combustor |
US20090165435A1 (en) * | 2008-01-02 | 2009-07-02 | Michal Koranek | Dual fuel can combustor with automatic liquid fuel purge |
-
1933
- 1933-06-30 US US678353A patent/US1941805A/en not_active Expired - Lifetime
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3809027A (en) * | 1972-02-28 | 1974-05-07 | Brunswick Corp | Internal combustion engine |
US4686941A (en) * | 1986-04-01 | 1987-08-18 | Sanshin Kogyo Kabushiki Kaisha | Turbulence generator for two-stroke spark-assisted diesel engines |
US4913111A (en) * | 1986-04-01 | 1990-04-03 | Sanshin Kogyo Kabushiki Kaisha | Turbulence generator for two-stroker spark-assisted diesel engines |
US4774919A (en) * | 1986-09-08 | 1988-10-04 | Yamaha Hatsudoki Kabushiki Kaisha | Combustion chamber importing system for two-cycle diesel engine |
US5111786A (en) * | 1991-05-03 | 1992-05-12 | Ford Motor Company | Air cell for an internal combustion engine |
US20090120094A1 (en) * | 2007-11-13 | 2009-05-14 | Eric Roy Norster | Impingement cooled can combustor |
US7617684B2 (en) | 2007-11-13 | 2009-11-17 | Opra Technologies B.V. | Impingement cooled can combustor |
US20090165435A1 (en) * | 2008-01-02 | 2009-07-02 | Michal Koranek | Dual fuel can combustor with automatic liquid fuel purge |
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