Fluid flow machine
View Patent ↗A fluid flow engine ( 1 ), in particular a turbo engine, has at least one guide vane row ( 5 ) with a plurality of guide vanes ( 6 ) and at least one rotor blade row ( 7 ) with a plurality of rotor blades ( 8 ). One guide vane row ( 5 ) and one rotor blade row ( 7 ) that follows the former directly downstream with respect to a working gas flow ( 11 ), together form a stage ( 10 ) of the fluid flow engine ( 1 ). To reduce the load on the rotor blades ( 8 ), the guide vanes ( 6 ) and the rotor blades ( 8 ) are coordinated at least in one stage ( 10 ) so that in a reference relative position between the respective guide vane ( 6 ) and the respective rotor blade ( 8 ), there is an axial distance (B) and a circumferential distance (C) between the outgoing flow edge ( 16 ) of the respective guide vane ( 6 ) and the oncoming flow edge ( 17 ) of the respective rotor blade ( 8 ) that is measured in the axial direction and is varied along a height (H) of a gas path ( 12 ) running axially between the blade rows ( 5, 7 ) of this stage ( 10 ), said height being measured radially.
1. A fluid flow engine comprising:
at least one guide vane row with a plurality of guide vanes;
at least one rotor blade row having a plurality of rotor blades;
one guide vane row and one rotor blade row following said one guide vane row directly downstream with respect to a working gas flow together forming a stage of the fluid flow engine;
wherein, in at least at one stage, the guide vanes and the rotor blades are configured and arranged so that, in a reference relative position of the respective guide vane and the respective rotor blade, an axial distance B axially measured with respect to a rotational axis of a rotor of the fluid flow engine, and a circumferential distance C circumferentially measured with respect to the rotational axis of the fluid flow engine between an outgoing flow edge of the respective guide vane and an oncoming flow edge of the respective rotor blade, vary along a radially measured height H of a gas path running axially between blade rows of said at least one stage; and
wherein the axial distance B and the circumferential distance C vary according to a second-order polynomial.
2. The fluid flow engine according to claim 1 , wherein the axial distance B decreases at first to a minimum from the inside radially to the outside radially along the gas path height H and then increases.
3. The fluid flow engine according to claim 2 , wherein said minimum of the axial distance B is approximately 50% of the gas path height H.
4. The fluid flow engine according to claim 1 , wherein each blade has a bottom, and said second-order polynomial has the form:
B =b 2 · h 2 +b 1 · h +b 0 ±b k
where
B =B/R, and
h =h/H, and
R=radial distance of a rotor blade bottom from the axis of rotation.
5. The fluid flow engine according to claim 4 , wherein the coefficient b 0 is positive.
6. The fluid flow engine according to claim 5 , wherein the coefficient b 0 has a value of +0.04117.
7. The fluid flow engine according to claim 4 , wherein the coefficient b 1 is negative.
8. The fluid flow engine according to claim 7 , wherein the coefficient b 1 has a value of −0.048122.
9. The fluid flow engine according to claim 4 , wherein the coefficient b 2 is positive.
10. The fluid flow engine according to claim 9 , wherein the coefficient b 2 has a value of +0.04731.
11. The fluid flow engine according to claim 4 , wherein the coefficient b k has a value of 0.0017.
12. The fluid flow engine according to claim 1 , wherein the circumferential distance C increases from the inside radially to the outside radially only along the gas path height H when the guide vanes and the rotor blades are oriented so that the circumferential distance C has a value of approximately zero on the inside radially.
13. The fluid flow engine according to claim 12 , wherein each blade has a bottom, and the second-order polynomial describing the circumferential distance C has the form:
C =c 2 · h 2 +c 1 · h +c 0 ±c k
where
C =C/R, and
h =h/H, and
R=radial distance of a rotor blade bottom from the axis of rotation.
14. The fluid flow engine according to claim 13 , wherein the coefficient c 0 is negative.
15. The fluid flow engine according to claim 14 , wherein the coefficient c 0 has a value of −0.000576.
16. The fluid flow engine according to claim 13 , wherein the coefficient c 1 is positive.
17. The fluid flow engine according to claim 16 , wherein the coefficient c 1 has a value of +0.007282.
18. The fluid flow engine according to claims 13 , wherein the coefficient c 2 is positive.
19. The fluid flow engine according to claim 18 , wherein the coefficient c 2 has a value of 0.035357.
20. The fluid flow engine according to claim 13 , wherein the coefficient c k has a value of 0.0017.