GUIDE UNIT FOR AIR FLOW AT INLET OF COMBUSTION CHAMBER OF GAS TURBINE ENGINE Russian patent published in 2011 - IPC F23R3/04 F01D9/02 F04D29/54 

Abstract RU 2435104 C2

FIELD: engines and pumps.

SUBSTANCE: straightening unit includes two coaxial shells between which the blades passing mainly in radial direction are arranged. Diffuser includes two coaxial walls representing rotation bodies and connected to each other by means of radial partitions. One of the shells of straightening unit is made in the form of single part with one wall of diffuser, which represents rotation body. The other shell of straightening unit is connected to and fixed on the other diffuser wall representing rotation body. Blades of strengthening unit are rigidly connected through one end to one shell of straightening unit and are located at some distance with a small gap from the other shell on the other end.

EFFECT: simpler manufacturing technology of the straightening unit.

15 cl, 8 dwg

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RU 2 435 104 C2

Authors

Dagene Ljuk Anri Klod

Dates

2011-11-27Published

2007-05-28Filed