FIELD: aviation.
SUBSTANCE: proposed helicopter has case, main rotor with blades, jet drive of blades mounted in case and fuel tank connected with jet drive by means of passage. Jet drive consists of air intake, intake chamber contraction tube, diffuser and burner connected in succession. Intake chamber is connected with fuel tank by means of passage for delivery of fuel at picked-up revolutions of main rotor blades.
EFFECT: simplified construction and enhanced operational reliability.
8 cl, 15 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HELICOPTER | 2000 |
|
RU2271309C2 |
| JET PISTON ENGINE | 1994 |
|
RU2094630C1 |
| OPERATING METHOD OF PULSE-DETONATION ENGINE IN CENTRIFUGAL FORCE FIELD AND DEVICE FOR IMPLEMENTATION THEREOF IN JET HELICOPTER | 2018 |
|
RU2718726C1 |
| JET ENGINE | 1997 |
|
RU2157907C2 |
| HELICOPTER WITH REACTIVE ROTOR DRIVE | 2018 |
|
RU2706746C1 |
| GAS TURBINE PLANT OPERATING ON HIGH-PRESSURE GASEOUS FUEL | 1996 |
|
RU2149273C1 |
| HELICOPTER POWER PLANT | 0 |
|
SU1794038A3 |
| VTOL AIRCRAFT | 2012 |
|
RU2490173C1 |
| ROCKET VEHICLE, RETURN STAGE OF ROCKET VEHICLE AND METHOD OF ITS LAUNCH UPON RETURN AND SYSTEM OF HELICOPTER PICK-UP OF RETURN STAGE | 2015 |
|
RU2609539C1 |
| VTOL AIRCRAFT | 2014 |
|
RU2546385C1 |
