FIELD: aviation. SUBSTANCE: air-conditioning system includes main for taking air from engine, cold and hot air lines provided with respective adjusting dampers and connected with main feeding the mixed air to cabin compartment; air-conditioning system contains also cooling turbine. Cold air line after cooling turbine is brought in communication with pipe line feeding the cold air to equipment compartments fitted with shut-off damper operated from altitude sensor and cross-connected with throttle valve by means of bypass line. EFFECT: enhanced efficiency. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SYSTEM FOR PREPARATION AND DELIVERY OF AIR TO FLYING VEHICLE COMPARTMENTS | 2001 |
|
RU2220885C2 |
| AIRCRAFT AIR-CONDITIONING SYSTEM | 1997 |
|
RU2170192C2 |
| DEVICE FOR COOLING UNITS OF AIRCRAFT ELECTRONIC EQUIPMENT | 1997 |
|
RU2124460C1 |
| FUEL SYSTEM OF MANEUVERABLE AIRCRAFT | 1996 |
|
RU2121944C1 |
| AIR CONDITIONING SYSTEM OF HERMETIC ZONE OF FLYING APPARATUS | 2016 |
|
RU2637080C1 |
| COMPLEX AIR CONDITIONING SYSTEM OF THE AIRCRAFT | 2017 |
|
RU2682758C1 |
| AIR CONDITIONER FOR VEHICLE POWERED BY INTERNAL COMBUSTION CHAMBER | 1994 |
|
RU2065126C1 |
| METHOD OF CONTROLLING AIRCRAFT CABIN AIR TEMPERATURE AND DEVICE TO THIS END | 2009 |
|
RU2401775C1 |
| APPARATUS FOR ELECTRICAL ADJUSTMENT OF ON-BOARD RADAR ANTENNA | 1997 |
|
RU2133477C1 |
| AIRCRAFT FUEL SYSTEM | 1997 |
|
RU2140379C1 |
