METHOD TO DETERMINE CURVILINEAR PROFILE OF DISC BLADES Russian patent published in 2014 - IPC F01C1/12 

Abstract RU 2530928 C2

FIELD: engines and pumps.

SUBSTANCE: invention relates to the field of propulsion engineering and relates to the method for determination of curvilinear profile of disc blades in a multi-rotor internal combustion engine according to the patent RU 2325542 C2 and makes it possible to simplify manufacturing technology. Disc blades with a ledge and a groove comprising an appropriate profile in the form of identical curved lines coupled to each other, differing by the fact that each curve of the blades line is described by equations XM1 = R·cos(φ+ αi)-r·sin(β+2αi); YM1 = R·sin (φ+ αi)-r·cos (β+2αi), where R - centre-to-centre distances between discs 1 and 2; φ - summary angle of the angle of centres of the ledge or the groove δ and the angle forming a curved line, φ1 or φ2, cos φ 1 = cos φ 2 = R 2 r ; α1 - angle; r - disc radius; β - rated angle according to the formula β=φ12+(90°±δ).

EFFECT: method makes it possible to treat disc blades both with ledges and grooves by means of slotting, milling and polishing, thus making it possible to significantly simplify the manufacturing technology.

3 dwg

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RU 2 530 928 C2

Authors

Ashmarin Aleksej Kadyrovich

Ivanov Boris Mikhajlovich

Kochetkov Maksim Nikolaevich

Dates

2014-10-20Published

2011-03-25Filed