Propeller blade root coupling

• US 10,968,757 B2
• Filed: 03/25/2019
• Issued: 04/06/2021
• Est. Priority Date: 04/10/2018
• Status: Active Grant

• Current Assignee: Ratier Figeac (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Ratier Figeac (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Fages, Christian
• Primary Examiner(s): Kershteyn, Igor
• Application Number:
  US16/362,845
• Publication Number:
  US 20190309639A1
• Time in Patent Office: 743 Days
• CPC Class Codes: B64C 11/04 Blade mountings
• CPC Class Codes: B64C 11/16 Blades
• CPC Class Codes: B64C 27/48 Root attachment to rotor head
• CPC Class Codes: F01D 5/3023 of radial insertion type, e.g. in individual recesses
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A method of mounting a metal blade root to a composite propeller blade body includes inserting a connection portion of the blade body into a bore formed in the blade root, wherein the connection portion comprises at least one depression formed in an outer surface thereof, and applying pressure to the outer surface of the blade root to cause it to deform and engage with the depressions, thereby mechanically coupling the blade root to the propeller blade body.

Claims

1. A method of mounting an airfoil component body to a blade root, comprising:

providing the airfoil component body, the airfoil component body having a connection portion, the connection portion comprising an elongate member with at least one depression formed on an outer surface thereof, wherein the airfoil component body is formed from a fibre-reinforced polymer material;

inserting the connection portion into a bore formed in the blade root, the blade root being a metal blade root; and

deforming the blade root such that a portion of the inner surface of the bore engages with at least one of the depressions in the connection portion to mechanically couple the blade root to the airfoil component body.

2. The method according to claim 1, wherein the at least one depression comprises a groove.

3. The method according to claim 1, wherein the bore and the connection portion each have a non-circular cross-sectional shape.

4. The method according to claim 1, wherein a plurality of fibres extend continuously from a body portion of the airfoil component body into the connection portion.

5. The method according to claim 1, further comprising:

applying an adhesive to at least one of an outer surface of the connection portion and an inner surface of the bore before deforming the blade root, and curing the adhesive after deforming the blade root.

6. The method according to claim 1, further comprising:

fitting one or more brace members within a bore of the connection portion prior to deforming the blade root.

7. The method according to claim 1, wherein the blade root is deformed by a magnetic-pulse system.

8. The method according to claim 1, wherein the airfoil component body comprises a propeller blade body or a spar body for a propeller blade.

9. An airfoil component comprising:

an airfoil component body having a connection portion, the connection portion comprising an elongate member with at least one depression formed on an outer surface thereof, wherein the airfoil component body is formed from a fibre-reinforced polymer material; and

a metal blade root defining a bore;

wherein;

the connection portion is received within the bore; and

an outer surface of the blade root is deformed such that a portion of the inner surface of the bore engages with at least one of the depressions in the connection portion to mechanically couple the blade root to the airfoil component body.

10. The airfoil component according to claim 9, wherein the at least one depression comprises a groove.

11. The airfoil component according to claim 9, wherein the bore and the connection portion each have a non-circular cross-sectional shape.

12. The airfoil component according to claim 9, wherein:

a plurality of the reinforcement fibres extend continuously through both the connection portion and a body portion of the airfoil component body.

13. The airfoil component according to claim 9, further comprising:

an adhesive bonding an outer surface of the connection portion to an inner surface of the bore.

14. A propeller comprising a propeller hub and at least two propeller blades, wherein each of the propeller blades is an airfoil component comprising:

an airfoil component body having a connection portion, the connection portion comprising an elongate member with at least one depression formed on an outer surface thereof, wherein the airfoil component body is formed from a fibre-reinforced polymer material; and

a metal blade root defining a bore;

wherein;

the connection portion is received within the bore; and

an outer surface of the blade root is deformed such that a portion of the inner surface of the bore engages with at least one of the depressions in the connection portion to mechanically couple the blade root to the airfoil component body.