Propeller blades

Patent metadata

Field	Value
Publication number	US-10577952-B2
Application number	US-201715498673-A
Country	US
Kind code	B2
Filing date	Apr 27, 2017
Priority date	Apr 27, 2016
Publication date	Mar 3, 2020
Grant date	Mar 3, 2020

Abstract

A propeller blade assembly comprises a propeller blade having a blade root for attaching the propeller blade to a hub. The blade root has a radially outer surface. The assembly further comprises a collar mounted to the blade root. The collar comprises at least two collar segments assembled around the radially outer surface of the blade root. Each collar segment has a radially inner surface, an opposed radially outward surface and first and second circumferential end lugs. The lugs receive fasteners for coupling the collar segments together to form the collar. The collar segments are formed from a flexible plastics material and the radially inner surface of each collar segments engages the radially outer surface of the blade root only over a limited circumferential extent of the collar segment.

First claim

The invention claimed is:

1. A propeller blade assembly comprising:
a propeller blade, said propeller blade having a blade root for attaching the propeller blade to a hub, said blade root having a radially outer surface having a circumferentially extending groove therein;
a collar mounted to the blade root, the collar comprising at least two collar segments assembled around the radially outer surface of the blade root; each collar segment having a radially inner surface, an opposed radially outward surface and first and second circumferential end lugs, said lugs receiving fasteners for coupling the collar segments together to form the collar;
wherein at least one of said collar segments is formed from a flexible material having a lower tensile modulus than that of the blade root and a geometry permitting the collar segment to flex;
wherein said radially inner surface of said collar segment engages the radially outer surface of the blade root only over a limited circumferential extent of said collar segment to permit said collar segment to flex.

2. The propeller blade assembly as claimed in claim 1 wherein said radially inner surface of said collar segment engages the radially outer surface of the blade root over less than 60% of its circumferential extent.

3. The propeller blade assembly as claimed in claim 1 , wherein said radially inner surface of said collar segment comprises at least one radially inwardly extending region for engaging the radially outer surface of the blade root.

4. The propeller blade assembly as claimed claim 1 , wherein said collar comprises two collar segments, each collar segment being formed from a flexible material.

5. The propeller blade assembly as claimed in claim 4 , wherein each said collar segment comprises at least one radially inwardly extending region.

6. The propeller blade assembly as claimed in claim 4 , wherein one collar segment comprises two inwardly extending regions and the other collar segment comprises one inwardly extending region.

7. The propeller blade assembly as claimed in claim 3 , wherein the inwardly extending region is a region having a smaller radius than those of adjacent inner surface regions of the collar segments.

8. The propeller blade assembly as claimed in claim 3 , wherein the inwardly extending region is smoothly joined to adjacent inner surface regions of the collar segments.

9. The propeller blade assembly as claimed in claim 1 , wherein said flexible material has a tensile modulus of below 100 GPa.

10. The propeller blade assembly as claimed claim 1 , wherein said flexible material is a plastics material or aluminium.

11. The propeller blade assembly as claimed claim 1 , wherein at least one end lug of at least one of said collar segments comprises a captive fastener, and an adjacent end lug of an adjacent collar segment comprises an opening for receiving the fastener.

12. The propeller blade assembly as claimed claim 1 , wherein said collar segments are injection moulded components or machined components.

13. The propeller blade assembly as claimed in claim 1 , wherein at least one of said collar segments comprises a mount for an accessory.

14. A method for assembling a propeller blade assembly as claimed in claim 1 comprising:
assembling said at least two collar segments in a groove around the radially outer surface of the blade root with said end lugs of adjacent collar segments opposed to one another; and
tightening fasteners between said opposed end lugs so as to bring said end lugs into face to face contact with each other and to clamp said collar to said blade root.

15. The propeller blade collar comprising:
at least two collar segments for assembly around the radially outer surface of a propeller blade root;
each collar segment comprising a radially inner surface, an opposed radially outward surface and first and second circumferential end lugs, said end lugs receiving fasteners for coupling the collar segments together to form the collar;
wherein at least one of said collar segments is formed from a flexible material and wherein said radially inner surface of said at least one collar segment comprises at least one radially inwardly extending region for engaging the radially outer surface of the blade root over only a limited circumferential extent of the at least one collar segment.

16. The propeller blade collar as claim 15 , wherein said collar comprises two collar segments, each collar segment being formed from a flexible material.

17. The propeller blade collar as claimed in claim 16 , wherein each said collar segment comprises at least one radially inwardly extending region.

18. The propeller blade collar as claimed in claim 17 , wherein one collar segment comprises two inwardly extending regions and the other collar segment comprises one inwardly extending region.

19. The propeller blade collar as claimed in claim 15 , wherein the inwardly extending region is a region having a smaller radius than those of adjacent inner surface regions of the collar segments.

20. The propeller blade collar as claimed in claim 15 , wherein the inwardly extending region is smoothly joined to adjacent inner surface regions of the collar segments.

Assignees

• Ratier Figeac Sas

Inventors

• Andrzejewski Arnaud
• Delmas Catherine
• Seminel Bruno

Classifications

• B64C11/04 Primary

  Blade mountings · CPC title

• F01D5/12

  Blades ({specially adapted for radial flow machines or engines F01D5/04}; blade roots F01D5/30; rotors with blades adjustable in operation F01D7/00; stator blades F01D9/02) · CPC title

• F01D5/02

  Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28}) · CPC title

• F05D2230/60

  Assembly methods · CPC title

• F05D2300/43

  Synthetic polymers, e.g. plastics; Rubber · CPC title