Group of blade rows

Patent metadata

Field	Value
Publication number	US-9797254-B2
Application number	US-201514626544-A
Country	US
Kind code	B2
Filing date	Feb 19, 2015
Priority date	Feb 27, 2014
Publication date	Oct 24, 2017
Grant date	Oct 24, 2017

Abstract

A blade row group arrangeable in a main flow path of a fluid-flow machine includes N adjacent member blade rows firmly arranged relative to each other in both a meridional direction (m) and a circumferential direction (u). A relative secondary passage length (v′) and a relative secondary passage width (w′) each increase at least in one part of the area between the mean meridional flow line (SLM) and at least one of the main flow path boundaries (HB) towards the main flow path boundary (HB).

First claim

The invention claimed is:

1. A blade row group arrangeable in a main flow path of a fluid-flow machine, comprising:
N adjacent member blade rows firmly arranged relative to each other in both a meridional direction (m) and a circumferential direction (u), where N is ≧2 and (i) designates a running index with values between 1 and N, the N adjacent member blade rows including a front member blade row with front blades (i) each having a leading edge VK(i) and a trailing edge HK(i), and a rear member blade row with rear blades (i+1) each having a leading edge VK(i+1) and a trailing edge HK(i+1),
where the blade row group has two main flow path boundaries (HB),
where, in at least one area of a blade height adjoining one of the main flow path boundaries (HB), between a front section of a suction side of a rear blade (i+1) in the rear member blade row and a rear section of a pressure side of a front blade (i) in the front member blade row, a secondary passage (NP) is provided which guides the flow locally,
where, in each meridional flow line section (m-u plane) through the blade row group:
a chord Se(i) of the front bladed (i) and a chord Se(i+1) of the rear blade (i+1) is defined as a tangent lying on a respective profile on the pressure side,
a profile depth I(i) of the front bladed (i) and the profile depth I(i+1) of the rear blade (i+1) are shown in a direction of the respective chord Se(i), Se(i+1),
a front blade spacing t(i) is defined as a distance in the circumferential direction (u) between two adjacent blades of the front member blade row (i) in a plane defined by the trailing edges of the two adjacent blades,
a front blade stagger angle lambda(i) and a rear blade stagger angle lambda(i+1) being defined as angles of inclination of the respective chord Se(i), Se(i+1), relative to the meridional direction (m),
a mean stagger angle lambdam is defined as a mean value of the stagger angles lambda(i) and lambda(i+1) in accordance with lambdam=(lambda(i)+lambda(i+1))/2,

where, in each trailing edge point H of the front blade (i) an auxiliary coordinate system having a first, a second and a third coordinate direction (s, q, or) is provided, with the first coordinate direction (s) facing downstream at the angle lambdam against the meridional direction (m), the second coordinate direction (q), perpendicular to the first coordinate direction (s), facing away from the pressure side of the front blade (i), and the third coordinate direction (or) being perpendicular to the first coordinate direction (s) and to the second coordinate direction (q),
where a secondary passage length v is defined as a distance between the trailing edge point H of the front blade (i) and a leading edge point V of the rear blade (i+1) in a direction of the first coordinate direction (s), and vSLM identifies a value on a mean meridional flow line (SLM),
where a standardized secondary passage length is defined in accordance with vn=v/l(i) and vnSLM identifies a value on the mean meridional flow line (SLM),
where a relative secondary passage length v′ is defined in accordance with v′=(v−vSLM)/l(i),
where a secondary passage width w is defined as a distance between the trailing edge point H of the front blade (i) and a point P on the suction side of the rear blade (i+1), where the point P results as an intersection point of an orthogonal (O) erected in the trailing edge point H of the front blade (i) in the first coordinate direction (s) with the suction side of the rear blade (i+1), where the orthogonal (O) is oriented against the second coordinate direction (q) leading away from the pressure side of the front blade (i), where a connection of all points P determined along the blade height in various meridional flow line sections results in a suction-side projection line PLSS(i+1) of the rear blade (i+1),
where wSLM identifies a value of w on the mean meridional flow line (SLM),
where a standardized secondary passage width is defined in accordance with wn=w/(t(i) cos lambdam), and wnSLM identifies a value of wn on the mean meridional flow line (SLM), and
where a relative secondary passage width w′ is defined in accordance with w′=(w−wSLM)/(t(i) cos lambdam),
where a relative secondary passage length v′ and the relative secondary passage width w′ each increase towards one of the main flow path boundaries (HB) at least in one part of ante area between the mean meridional flow line (SLM) and the one of the main flow path boundaries (HB),
where the values for the relative secondary passage length v′ and the relative secondary passage width w′ are, on at least one of the main flow path boundaries (HB), greater than on the mean meridional flow line (SLM) in a main flow path center,
where, in a view directed upstream and parallel to the first coordinate direction (s) in the mean meridional flow line blade section, a degree of bulge WGh2 of the trailing edge HK(i) of the front blade (i) in the area between the mean meridional flow line (SLM) and at least one of the main flow path boundaries (HB) is greater than a degree of bulge WGp of the suction-side projection line PLSS(i+1) of the rear blade (i+1),
where a degree of bulge WGh2 of the trailing edge HK(i) is defined as a greatest ascertainable distance (dh2) between the trailing edge HK(i) and a straight connecting line (Lh2) of points of the trailing edge HK(i) on the mean meridional flow line (SLM) and at one of the main flow path boundaries (HB) relative to a meridional flow surface-orthogonal distance (dor) on the trailing edge HK(i) between the one of the main flow path boundaries (HB) and the mean meridional flow line (SLM), in accordance with WGh2=dh2/dor, and the degree of bulge (WGp) of the suction-side projection line PLSS(i+1) is defined as a greatest ascertainable distance (dp) between the projection line PLSS(i+1) and a straight connecting line (Lp) of points of the projection line PLSS(i+1) on the mean meridional flow line (SLM) and at one of the main flow path boundaries (HB) relative to the meridional flow surface-orthogonal distance (dor) between the one of the main flow path boundaries (HB) and the mean meridional flow line (SLM), in accordance with WGp=dp/dor.

2. The blade row group in accordance with claim 1 , wherein the relative secondary passage length v′ in an area adjoining one of the main flow path boundaries (HB) rises continuously towards the one of the main flow path boundaries (HB).

3. The blade row group in accordance with claim 1 , wherein the relative secondary passage length v′ in an area adjoining one of the main flow path boundaries (HB) remains constant.

4. The blade row group in accordance with claim 1 , wherein the relative secondary passage length v′ in an area adjoining one of the main flow path boundaries (HB) decreases towards the one of the main flow path boundaries (HB).

5. The blade row group in accordance with claim 1 , wherein a distribution of the relative secondary passage length v′ over a main flow path penetration (HE) is completely below an upper limit curve v′o and completely above a lower limit curve v′u, where the upper limit curve v′o is provided by:
v′o=− 6 E -08( HE )**4+4 E -07( HE )**3+0.0004( HE )**2−0.0224( HE )+0.45

and the lower limit curve is provided by:
v′u= 5 E -08( HE )**4−5 E -06( HE )**3+0.0003( HE )**2−0.0111( HE )+0.05.

6. The blade row group in accordance with claim 1 , wherein the relative secondary passage width w′ in an area adjoining one of the main flow path boundaries (HB) rises continuously towards the one of the main flow path boundaries (HB).

7. The blade row group in accordance with claim 1 , wherein the relative secondary passage width w′ in an area adjoining one of the main flow path boundaries (HB) remains constant.

8. The blade row group

Assignees

• Rolls Royce Deutschland Ltd & Co Kg

Inventors

• Guemmer Volker

Classifications

• F01D5/146

  of blades with tandem configuration, split blades or slotted blades · CPC title

• F04D29/324

  Blades · CPC title

• F04D29/544

  Blade shapes · CPC title

• Y02T50/673

  Cross-Sectional Technologies · mapped topic

• F01D5/022 Primary

  with concentric rows of axial blades · CPC title