INTERNAL COMBUSTION ENGINE Russian patent published in 2016 - IPC F28D15/02 F01K11/04 

FIELD: machine building.

SUBSTANCE: invention relates to power engineering and can be used as an aircraft engine. Internal combustion engine includes tight housing (1) in form of truncated cone partially filled with heat carrier. Housing includes evaporator (2) and capacitor (3). In housing there is a heat-insulation ring (4), which is an element of housing and rigidly fastened with both evaporator and condenser of engine. To heat-insulation ring is rigidly attached impeller (5) of turbine with working blades, encircled by rim (6). Turbine wheel is rigidly secured to hollow shaft (7) of engine. Nozzle is installed on hollow shaft gear (8) of turbine, encircled by a rim (9), which is made up of internal annular magnet. Rims of both wheels are mounted so that annular gap (10) is formed with housing. Wheel with nozzle blades is installed with possibility of rotation relative to hollow shaft - on bearings (11). Above inner annular magnet there is outer annular magnet (12) rigidly connected to housing (13) of aircraft. On hollow motor shaft is rigidly fixed screw (14). In engine housing, in condensation zone, there are heat-conducting rods (15) on which are rigidly fixed plates (16), profile formed by technological operation "rolling" on both sides. Spiral is located around evaporator combustion chamber (17) with nozzles (18). Inside evaporator there is a metallic finely porous sponge (19).

EFFECT: higher engine power, safety of its transportation in idle state, as well as reduced weight and size.

3 cl, 8 dwg