FIELD: engine engineering. SUBSTANCE: gas turbine heaters, devices for cooling supercharging air, air intake housings as well as pipe lines between the parts of the plant and pipe lines connected with the inlet passageways of cylinder heads are arranged in the same manner at one- stage supercharging and double-stage supercharging. At double-stage supercharging, the device for cooling supercharging high-pressure air is mounted instead of the device for cooling supercharging air at one-stage supercharging. High-pressure gas turbine superchargers are mounted instead of gas turbine chargers used at one- stage supercharging. The devices for cooling supercharging air are mounted on air collecting housing. The gas turbine chargers are mounted on the narrow side of the air collecting housing. EFFECT: improved design. 9 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
PISTON INTERNAL COMBUSTION ENGINE WITH SUPERCHARGING | 1990 |
|
RU2011863C1 |
MULTICYLINDER SUPERCHARGED PISTON INTERNAL COMBUSTION ENGINE | 0 |
|
SU1709920A3 |
GAS OUTLET PIPELINE | 1994 |
|
RU2104398C1 |
MULTICYLINDER DIESEL LOW COMPRESSION RATIO ENGINE | 0 |
|
SU1806281A3 |
INTERNAL-COMBUSTION ENGINE EXHAUST PIPE | 0 |
|
SU1766274A3 |
IMPROVEMENT OF ENGINE EXHAUST SYSTEM | 0 |
|
SU1701118A3 |
EXHAUST PIPELINE OF MULTICYLINDER SUPERCHARGED PISTON I.C. ENGINE | 0 |
|
SU1618284A3 |
AIR INTAKE FOR TURBO-JET AIRCRAFT ENGINE | 1991 |
|
RU2039880C1 |
INTERNAL-COMBUSTION ENGINE OIL CHANNEL | 0 |
|
SU1766273A3 |
TURBOJET ENGINE | 1992 |
|
RU2101535C1 |
Authors
Dates
1996-08-20—Published
1991-05-24—Filed