FIELD: engines and pumps.
SUBSTANCE: for overlapping valve plunger turn or move relative to the valve body mechanism move, advanced the position of pistons all valves change synchronously to intermediate positions between the provisions of the "open" to "closed" position and, conversely, when the flow of air change and record simultaneously on all the valves using the transfer control action associated with the mechanism of movement of each valve and control system. Medium control action on air consumption made mechanical and/or electrical. Provided, that in the "closed" position on all valves simultaneously using the minimum management system "orderly" cooling air consumption, necessary to minimize leaf loss profiles on soplovom device and working turbine blades.
EFFECT: reducing the specific fuel consumption for all modes of operation, stability is improved cooling.
2 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR AIR SUPPLY FOR TURBOREACTIVE ENGINE TURBINE COOLING (OPTIONS) | 2017 |
|
RU2656165C1 |
| SYSTEM TO CONTROL FLOW RATE OF AIR COOLING TURBINE OF TURBOJET ENGINE | 2001 |
|
RU2194179C1 |
| AIR FLOW CONTROL SYSTEM FOR COOLING TURBINE OF BYPASS TURBOJET ENGINE | 2015 |
|
RU2614460C1 |
| METHOD OF AND DEVICE TO INCREASE ECONOMY OF TURBOJET ENGINE (VERSIONS) | 2004 |
|
RU2295644C9 |
| METHOD OF CONTROLLING GAS TURBINE ENGINE | 2017 |
|
RU2647017C1 |
| METHOD OF OPERATION AND DESIGN OF TWO-STROKE INTERNAL COMBUSTION ENGINE | 2001 |
|
RU2231658C2 |
| METHOD AND SYSTEM FOR ADJUSTMENT OF CLEARANCE AT TURBINE ROTOR BLADE EDGES | 2011 |
|
RU2566510C2 |
| TURBO ENGINE AND METHOD FOR OPERATION THEREOF | 2017 |
|
RU2674172C1 |
| METHOD OF COOLING TURBINE WHEEL ROTOR OF MULTIMODE TURBOJET ENGINE | 1999 |
|
RU2159335C1 |
| INTERNAL COMBUSTION ENGINE | 2000 |
|
RU2191910C2 |
