Двигатель будущего, Дизельный ДВС, прототип - двигатель Баландина, последняя разработка, ноу-хау, передовая мысль, супер мотор, стратегически важный проект

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.

2_Turb.gif (29037 bytes)

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 other.

All other CC with 6 on 14 work in above described mode, is consecutive on a during of rotation of the main turbine.

Use in cyclic TE established in a plane The blades on sections of the turbine and compressor CZG in a complex with group located on a circle CC allows to simplify the system gas-distribution and to receive at any moment of time all processes of operation in different CC, that will supply balanced operation of the turbine and compressor, so will increase reliability and power TE.

Fulfilment CZG on halves of circles of compressor and turbine with offset CZG of the turbine forwards on a course of rotation on a quarter of a circle rather CZG of a compressor allows in each of CC consistently to receive four processes of operation - airing, compression, combustion, exhaust, that improvement of parameters of profitability will ensure.

The installation in PS of the additional shaft, on which are fixed additional секторы of a compressor and turbine rotated opposite to a main rotor, allows to lift power, and in connection with absence of device to rectifying of the and possibility to lift pressure in CC, not increasing frequency of rotation of the main turbine and compressor, to improve the efficiency of the engine.

Equipment CZG from the party CC channels for transmitting, and fuel channel, which, passes on the main shaft through the turbine in прилегающую to CC section of a compressor and further through CZG, then is divided and arrives on an exterior blades at a level CC, allows to increase power at the expense of increase of frequency of rotation of the main turbine and compressor, since центробежно sprayed, the heated up fuel, ignited by products of combustion from prior CC will have time qualitatively and quickly to burn down even for very short time.