Mistuned bladed rotor and associated manufacturing method

Patent metadata

Field	Value
Publication number	US-10837287-B2
Application number	US-201715411236-A
Country	US
Kind code	B2
Filing date	Jan 20, 2017
Priority date	Jan 20, 2017
Publication date	Nov 17, 2020
Grant date	Nov 17, 2020

Abstract

Mistuned bladed rotors and associated manufacturing methods are disclosed. An exemplary method includes forming two or more blades of the bladed rotor where the two or more blades have substantially identical external aerodynamic surfaces and have different internal configurations causing the two or more blades to have different natural frequencies.

First claim

What is claimed is:

1. A bladed rotor comprising blades of two or more different blade types, each of the different blade types defining an identical external aerodynamic surface and a different internal configuration selected to provide different natural frequencies of the blades of the different blade types, the blades of the different blade types including:
a first blade of a first of the different blade types having a first continuous internal channel extending between two first openings to an exterior of the bladed rotor, the two first openings being located on a hub of the bladed rotor, the first continuous internal channel being closed between the two first openings; and
a second blade of a second of the different blade types having a second continuous internal channel extending between two second openings to the exterior of the bladed rotor, the two second openings being located on the hub of the bladed rotor, the second continuous internal channel being closed between the two second openings, the first and second continuous internal channels having different shapes.

2. The bladed rotor as defined in claim 1 , wherein the first and second blades have blade root fillets of different geometries.

3. A mistuned bladed rotor comprising a plurality of circumferentially distributed blades, two or more of the blades having identical external aerodynamic surfaces and having different internal configurations selected to provide the two or more blades with different natural frequencies, a first of the two or more blades having a first continuous internal channel extending between two first openings to an exterior of the bladed rotor, the two first openings being located on a hub of the bladed rotor, the first continuous internal channel being closed between the two first openings, a second of the two or more blades having a second continuous internal channel extending between two second openings to the exterior of the bladed rotor, the two second openings being located on the hub of the bladed rotor, the second continuous internal channel being closed between the two second openings, the first and second internal channels having different shapes.

4. The bladed rotor as defined in claim 3 , wherein the two first openings are located on a same side of the hub of the bladed rotor.

5. The bladed rotor as defined in claim 3 , wherein the two first openings are located on opposite axial sides of the hub of the bladed rotor.

6. The bladed rotor as defined in claim 3 , wherein the two first openings are occluded by respective plugs.

7. The bladed rotor as defined in claim 3 , wherein the first internal channel extends into the hub of the bladed rotor.

8. The bladed rotor as defined in claim 3 , wherein the two first openings are located in a rim portion of the hub of the bladed rotor.

9. The bladed rotor as defined in claim 3 , wherein the bladed rotor is a centrifugal impeller.

10. The bladed rotor as defined in claim 3 , wherein the bladed rotor is a bladed disk.

11. The bladed rotor as defined in claim 3 , wherein the first and second blades are adjacent one another.

12. A method of manufacturing a mistuned bladed rotor, the method comprising forming blades of the rotor according to two or more different blade types, each of the different blade types defining an identical external aerodynamic surface and a different internal configuration selected to provide different natural frequencies of the blades of the different blade types, the blades of the different blade types including:
a first blade of a first of the different blade types having a first continuous internal channel extending between two first openings to an exterior of the bladed rotor, the two first openings being located on a hub of the rotor, the first continuous internal channel being closed between the two first openings; and
a second blade of a second of the different blade types having a second continuous internal channel extending between two second openings to the exterior of the bladed rotor, the two second openings being located on the hub of the rotor, the second continuous internal channel being closed between the two second openings, the first and second continuous internal channels having different shapes.

13. The method as defined in claim 12 , comprising using additive manufacturing to form the first and second blades.

14. The method as defined in claim 12 , further comprising:
subjecting the first and second blades to hot isostatic pressing; and
subjecting the first and second continuous internal channels to abrasive flow machining.

15. The method as defined in claim 12 , comprising occluding the two first openings using respective plugs.

16. The method as defined in claim 12 , wherein the first and second blades have root fillets of different geometries.

Assignees

• Pratt & Whitney Canada

Inventors

• Abrari Farid

Classifications

• F04D29/284

  for compressors · CPC title

• F05D2240/301

  Cross-sectional characteristics · CPC title

• F05D2230/31

  Layer deposition · CPC title

• F01D5/18

  Hollow blades, {i.e. blades with cooling or heating channels or cavities (structure of hollow blades in general F01D5/147)}; Heating, heat-insulating or cooling means on blades · CPC title

• F01D5/046

  Heating, heat insulation or cooling means · CPC title