Core-protecting fan modules and turbofan engines containing the same

Patent metadata

Field	Value
Publication number	US-10670040-B2
Application number	US-201715439430-A
Country	US
Kind code	B2
Filing date	Feb 22, 2017
Priority date	Feb 22, 2017
Publication date	Jun 2, 2020
Grant date	Jun 2, 2020

Abstract

Embodiments of a core-protecting fan module are provided, as are embodiments of a turbofan engine containing such a fan module. In an embodiment, the core-protecting fan module contains a nose member, a fan rotor downstream of the nose member, a full span stator downstream of the fan rotor, and a splitter structure downstream of the fan rotor. The fan rotor includes a plurality of fan blades, which extends from a rotor hub and which is angularly spaced about a rotational axis. Certain fundamental angular relationships are observed between the angles formed by rotational axis, the nose member, the fan rotor, and a leading edge of the splitter structure to reduce contaminant ingestion by the core flow path and to promote moisture shedding to reduce susceptibility to icing within the fan module, while further avoiding or minimizing negative impacts to other structural and functional aspects of the turbofan engine.

First claim

What is claimed is:

1. A core-protecting fan module, comprising:
a nose member;
a fan rotor downstream of the nose member, the fan rotor comprising:
a rotor hub rotatable about a rotational axis; and
a plurality of fan blades angularly spaced about the rotational axis;

a full span stator downstream of the fan rotor; and
a splitter structure downstream of the fan rotor;
wherein, in a cross-section plane containing the rotational axis, the rotational axis forms:
a first angle (θ 1 ) with a line extending from a foremost intersection between the rotational axis and the nose member (P N_LE ) to a point at which the rotor hub intersects a leading edge of a first fan blade included in the plurality of fan blades (P B_LE_IN );
a second angle (θ 2 ) with a line extending from P B_LE_IN to a point at which the rotor hub intersects a trailing edge of the first fan blade (P B_TE_IN ); and
a third angle (θ 3 ) with a line extending from P B_TE_IN to a leading edge of the splitter structure;

wherein the first angle is greater than the third angle (θ 1 >θ 3 ), the second angle is greater than the third angle (θ 2 >θ 3 ), and the first angle is less than the sum of the second and third angles (θ 1 <θ 2 +θ 3 ); and
wherein the nose member has a radius (R N ) measured in a radial direction from P N_LE to P B_LE_IN and further has a length (L N ) measured along the rotational axis from P N_LE to P B_LE_IN , and wherein

0.5
≤

R
N

L
N

≤
0.65

,

and
wherein the rotor hub has a length (L H ) measured along the rotational axis from P B_LE_IN to P B_TE_IN wherein the leading edge of the splitter structure is offset from P B_LE_IN along the rotational axis by a longitudinal clearance (L OFFSET ), and wherein L H >0.75(L OFFSET ).

2. The core-protecting fan module of claim 1 wherein the plurality of fan blades consists of a predetermined number (n) of fan blades, and wherein 16≤n≤24.

3. The core-protecting fan module of claim 2 wherein

R
N

R
TOTAL

<
0.32

,

and wherein R TOTAL is a radial dimension measured from P N_LE to P B_LE_OUT , as taken along an axis perpendicular to the rotational axis.

4. The core-protecting fan module of claim 2 wherein the core-protecting fan module comprises:
a first dimension (R N ) measured in a radial direction from P N_LE to P B_LE_IN ;
a second dimension (R H ) measured in a radial direction from P B_LE_IN to P B_TE_IN ; and
a third dimension (R OFFSET ) measured in a radial direction from P B_TE_IN to the leading edge of the splitter structure (P SPLT_LE ); and
wherein R N <R H +R OFFSET .

5. The core-protecting fan module of claim 2 wherein θ 3 >0.5(θ 1 ).

6. The core-protecting fan module of claim 2 wherein θ 2 >22 degrees.

7. The core-protecting fan module of claim 2 wherein the first angle (θ 1 ) and the second angle (θ 2 ) differ by less than one half the third angle (θ 3 ).

8. The core-protecting fan module of claim 2 wherein 27 degrees≤θ 1 ≤33 degrees.

9. The core-protecting fan module of claim 2 wherein the full span stator comprises a first stator vane having an inboard trailing edge portion and an outboard trailing edge portion;
wherein the inboard trailing edge portion is located forward of the leading edge of the splitter structure, as taken along the rotational axis; and
wherein the outboard trailing edge portion is located aft of the leading edge of the splitter structure, as taken along the rotational axis.

10. The core-protecting fan module of claim 2 wherein the plurality of fan blades and the rotor hub are integrally formed as a blisk.

11. A core-protecting fan module, comprising:
a full span stator having a plurality of stator vanes;
a fan rotor upstream of the full span stator, the fan rotor comprising:
a rotor hub rotatable about a rotational axis; and
a plurality of fan blades extending from the rotor hub and angularly spaced about the rotational axis;

a nose member adjacent and upstream of the rotor hub, the nose member comprising:
a radius (R N ) measured in a radial direction from a foremost intersection between the rotational axis and the nose member (P N_LE ) to an intersection between the rotor hub and a leading edge of a first fan blade in the plurality of fan blades (P B_LE_IN ); and
a length (L N ) measured along the rotational axis from P N_LE to P B_LE_IN ;
wherein the plurality of fan blades consists of a predetermined number (n) of fan blades;

wherein 16≤n≤24, while

0.5
≤

R
N

L
N

≤
0.65

,

and
wherein the rotor hub has a length (L H ) measured along the rotational axis from P B_LE_IN to P B_TE_IN , wherein the leading edge of the splitter structure is offset from P B_LE_IN along the rotational axis by a longitudinal clearance (L OFFSET ), and wherein L H >0.75(L OFFSET ).

12. The core-protecting fan module of claim 11 further comprising:
a core flow path downstream of the fan rotor;
a bypass flow path downstream of the fan rotor; and
a splitter structure partitioning the bypass flow path and the core flow path, the splitter structure comprising a leading edge offset from P B_LE_IN along the rotational axis by the longitudinal clearance (L OFFSET ).

13. The core-protecting fan module of claim 12 wherein the full span stator comprises a first stator vane having an inboard trailing edge portion and an outboard trailing edge portion;
wherein the inboard trailing edge portion is located forward of the leading edge of the splitter structure, as taken along the rotational axis; and
wherein the outboard trailing edge portion is located aft of the leading edge of the splitter structure, as taken along the rotational axis.

14. The core-protecting fan module of claim 13 wherein the rotor hub has a radial dimension (R H ) measured in a radial direction from P B_LE_IN to a point at which the rotor hub intersects a trailing edge of the first fan blade (P B_TE_IN ), and wherein R H >R OFFSET .

15. The core-protecting fan module of claim 11 wherein, in a cross-section plane containing the rotational axis, the rotational axis forms:
a first angle (θ 1 ) with a line extending from P N_LE to P B_LE_IN ;
a second angle (θ 2 ) with a line extending from P B_LE_IN to a point at which the rotor hub intersects a trailing edge of the first fan blade (P B_TE_IN ); and
a third angle (θ 3 ) with a line extending from P B_TE_IN to the leading edge of the splitter structure;
wherein θ 1 >θ 3 , while θ 2 >θ 3 .

Assignees

• Honeywell Int Inc

Inventors

• Nolcheff Nick
• Repp John
• Hayes Jeffrey
• Gunaraj John A
• Gebre-Giorgis Yoseph

Classifications

• F05D2240/20

  Rotors · CPC title

• F04D29/325 Primary

  for axial flow fans (blade mountings F04D29/34, blades F04D29/38) · CPC title

• F02K3/06 Primary

  with front fan · CPC title

• F02C7/05

  having provisions for obviating the penetration of damaging objects or particles · CPC title

• B64C11/14

  Spinners · CPC title