AT131454B - Arrangement of the auxiliary machines in aircraft internal combustion engines with star-shaped cylinder arrangement and fuel injection. - Google Patents
Arrangement of the auxiliary machines in aircraft internal combustion engines with star-shaped cylinder arrangement and fuel injection.Info
- Publication number
- AT131454B AT131454B AT131454DA AT131454B AT 131454 B AT131454 B AT 131454B AT 131454D A AT131454D A AT 131454DA AT 131454 B AT131454 B AT 131454B
- Authority
- AT
- Austria
- Prior art keywords
- arrangement
- star
- internal combustion
- fuel injection
- combustion engines
- Prior art date
Links
Landscapes
- Fuel-Injection Apparatus (AREA)
Description
<Desc/Clms Page number 1>
EMI1.1
EMI1.2
<Desc/Clms Page number 2>
Zylinder ist eine besondere Brennstoffpumpe zugeordnet. Zu dem Zylinder 1 gehört die Brennstoffpumpe 7. Sämtliche Brennstoffpumpen liegen sternförmig in einer Ebene vor dem Zylinderstern auf der Luftschraubenseite und werden durch einen einzigen Nocken 8 gesteuert, der auf der Kurbelwelle angeordnet ist. Die erforderliche Spül- und Ladeluft wird durch ein Gebläse 5 geliefert, das iiber ein Vorgelege 6 von der Kurbelwelle angetrieben wird. Der Spülgebläseantrieb ist auf der den Brennstoffpumpen und der Luftschraube entgegengesetzten Seite des Zylindersterns angeordnet, wodurch eiue überaus günstige Bauart der Maschine erzielt wird.
Die gleiche Anordnung kann auch für Fahrzeuge und für ortsfeste Zwecke mit gleichem Vorteil Verwendung finden.
<Desc / Clms Page number 1>
EMI1.1
EMI1.2
<Desc / Clms Page number 2>
A special fuel pump is assigned to the cylinder. The fuel pump 7 belongs to the cylinder 1. All fuel pumps lie in a star shape in a plane in front of the cylinder star on the propeller side and are controlled by a single cam 8 which is arranged on the crankshaft. The required scavenging and charge air is supplied by a fan 5, which is driven by the crankshaft via a reduction gear 6. The scavenging fan drive is arranged on the side of the cylinder star opposite the fuel pumps and the propeller, which results in an extremely inexpensive design of the machine.
The same arrangement can also be used with the same advantage for vehicles and for stationary purposes.
Claims (1)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE131454X | 1930-07-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
AT131454B true AT131454B (en) | 1933-01-25 |
Family
ID=5664065
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT131454D AT131454B (en) | 1930-07-25 | 1931-06-30 | Arrangement of the auxiliary machines in aircraft internal combustion engines with star-shaped cylinder arrangement and fuel injection. |
Country Status (1)
Country | Link |
---|---|
AT (1) | AT131454B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1223191B (en) * | 1962-08-04 | 1966-08-18 | Kloeckner Humboldt Deutz Ag | Power plant |
DE3132764A1 (en) * | 1981-08-19 | 1983-05-11 | Otto 7615 Zell Meier | Tandem installation for the generation of heat, cold and electrical current |
-
1931
- 1931-06-30 AT AT131454D patent/AT131454B/en active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1223191B (en) * | 1962-08-04 | 1966-08-18 | Kloeckner Humboldt Deutz Ag | Power plant |
DE3132764A1 (en) * | 1981-08-19 | 1983-05-11 | Otto 7615 Zell Meier | Tandem installation for the generation of heat, cold and electrical current |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
AT131454B (en) | Arrangement of the auxiliary machines in aircraft internal combustion engines with star-shaped cylinder arrangement and fuel injection. | |
DE344072C (en) | Working method for multi-cylinder internal combustion engines | |
CH158030A (en) | Injection internal combustion engine with cylinders arranged in a star shape for vehicles, in particular for aircraft. | |
DE619954C (en) | Multi-cylinder internal combustion engine | |
AT133027B (en) | Two-stroke diesel engine with controlling piston for aircraft propulsion. | |
CH136126A (en) | Double-acting internal combustion engine with a supercharging pump driven by an exhaust gas turbine. | |
DE964909C (en) | Air-cooled two-stroke internal combustion engine and crankcase scavenging | |
AT100376B (en) | Method and device for increasing the performance of four-stroke diesel engines. | |
AT139343B (en) | Internal combustion engine. | |
AT50966B (en) | Working methods for internal combustion engines. | |
AT92249B (en) | Internal combustion engine with a capsule blower. | |
DE736195C (en) | Multi-cylinder piston power or working machine | |
AT129652B (en) | Two-stroke internal combustion engine for heavy fuel oil with spark ignition. | |
DE358645C (en) | Two-stroke explosion engine with working cylinders and charge pump arranged at an angle to one another | |
AT83580B (en) | Two-stroke internal combustion engine with cylinders facing each other. | |
DE661892C (en) | Internal combustion turbine | |
AT60423B (en) | High-speed internal combustion engine for liquid fuels. | |
DE545768C (en) | Internal combustion engine in which a reciprocating engine and a turbine work together in such a way that part of the combustion gases of the reciprocating engine act on the turbine | |
DE446677C (en) | Power plant | |
AT99546B (en) | Cooling device for internal combustion engines. | |
DE435331C (en) | Fuel pump | |
AT123289B (en) | Fuel injection device for internal combustion engines, in particular diesel engines. | |
DE704950C (en) | Auxiliary machine set driven in groups for mobile systems, especially for aircraft, with steam turbine drive | |
AT145392B (en) | Device for adjusting the ignition point when starting internal combustion engines. | |
GB425987A (en) | Improved driving mechanism for internal combustion engines |