Двигатель будущего, Дизельный ДВС, прототип - двигатель Баландина, последняя разработка, ноу-хау, передовая мысль, супер мотор, стратегически важный проект
The Albert Gurdjiyan's turbine engine (TE) .
On Figure 1, is represented TE a sectional view in a plane, containing an axis the primary shaft (PS); on Figure 2, is represented TE, sectional view on А-А across an axes PS; on Figure 3, is represented section of compressor equipped sector cutting zolotnik gate (CZG) a sectional view on В-В; on Figure 4, is represented. section of the turbine with CZG, sectional view on С-С; on Figure 5, is represented. CZG a sectional view on D-D.
Offered TE, contains: Tank 1, with a rotor consisting from PS 2 on which are established of section a compressor 3 and turbine 4, between which in tank around PS are located on a circle of the camera of periodic combustion (CC) 5-14 nearest to CC of section of a compressor and turbine, are made with sectors of a CZG 15, 16 in a plane the blades executed on halves of circles of compressor and turbine, and CZG of the turbine is mounted with offset forwards on a direction of rotation on a quarter of a circle rather CZG of a compressor, owing to that they are divided on sectors: airing-E, compression-F, combustion-J, exhaust-H. PS is executed empty and in him Is established the additional shaft 17, on which are fixed of additional section of compressor 18 and turbine 19, rotated opposite to a main rotor. CZG are equipped transmitting channels 20, 21 from the party CC. The fuel channel passes on the primary shaft through the turbine in nearest to CC section of a compressor, where passing through CZG, is divided and leaves on opposite CC the party blades at a level CC (on the drawing is not shown). In CC 5 established the device for ignition fuel 22. In tank between CC and PS and from an exterior from CC through channels of air cooling 23 with the basic bulkheads 24 are located on a circle.
Offered TE works as follows: When a rotor the containing of compressor
3 and turbine 4, on PS 2, rotating, combines sectors Е of compressor and turbine with CC
5, in given CC there is the airing with substitution of spent gases by working mixture
owing to operation of compressor and turbine (C&T), when with CC sector F C&T is
combined, there is the compression in connection with an overlap CC on the part of the
turbine CZG 16, further, when with CC sector J C&T is combined, there is the
combustion, since. CC is blocked CZG with both parties, the ignition is made by the system
24 and products of combustion from CC 14, arriving on transmitting channels 22, 23, then
the working body on the same channels partially arrives in following CC 6, further when
with CC sector H C&T is combined, there is the exhaust - running cycle, since. CC is
blocked CZG on the part of a compressor and the working body untwists the turbine and
compressor in one party, and additional turbine 19 and compressor 18 on the shaft 17 in