Propeller blades

Patent metadata

Field	Value
Publication number	US-11215058-B2
Application number	US-201916692273-A
Country	US
Kind code	B2
Filing date	Nov 22, 2019
Priority date	Nov 27, 2018
Publication date	Jan 4, 2022
Grant date	Jan 4, 2022

Abstract

A propeller blade comprises a composite blade spar and at least one cover shell section adhesively bonded to the blade spar by a thermoplastic adhesive.

First claim

The invention claimed is:

1. A propeller blade comprising:
a composite blade spar; and
at least one cover shell section adhesively bonded to the blade spar by a thermoplastic adhesive;
wherein the at least one cover shell section comprises a plurality of layers; and
wherein the layers comprise an electrically conductive lightning protection layer which can be heated in order to heat the thermoplastic adhesive.

2. A propeller blade as claimed in claim 1 , comprising a first cover shell section covering a first side of the blade spar and a second cover shell section covering a second side of the blade spar.

3. A propeller blade as claimed in claim 1 , wherein the at least one cover shell section comprises at least one fiber reinforced layer.

4. A propeller blade as claimed in claim 1 , wherein the layers comprise an external erosion resistant layer.

5. A propeller blade as claimed in claim 1 , wherein the blade spar comprises a structural spar element and leading and trailing edge cores, and a fiber layer wrapped around the structural spar element and the cores.

6. A propeller blade as claimed in claim 1 , further comprising an erosion resistant sheath and/or electrical de-icer bonded to the blade with a thermoplastic adhesive.

7. A propeller blade as claimed in claim 1 , wherein the thermoplastic adhesive is a PPO/PS (polyphenylene oxide/polystyrene) or a modified PA (polyamide), PEI (polyether imide), PAEK (polyaryletherketone) or PEKK (polyetherketoneketone) adhesive.

8. A propeller blade according to claim 1 , wherein the electrically conductive lightning protection layer comprises a metallic mesh.

9. A propeller blade according to claim 1 , wherein the electrically conductive lightning protection layer is connected to a power source through electrical connections.

10. A propeller blade according to claim 1 , wherein the electrically conductive lightning protection layer is close to the adhesive such that the electrically conductive lightning protection layer can provide heat in a targeted manner to reduce overheating of other components of the blade.

11. A propeller blade according to claim 1 , wherein the electrically conductive lightning protection layer is configured to receive a current in order to heat the thermoplastic adhesive.

12. A method of repairing a propeller blade comprising a composite blade spar and at least one cover shell section adhesively bonded to the blade spar by a thermoplastic adhesive, the method comprising:
heating the propeller blade to a temperature above the melting temperature of the thermoplastic adhesive;
removing a damaged shell section; and
adhesively bonding a replacement cover shell section to the blade using a thermoplastic adhesive, wherein the heating includes heating an electrically conductive lightning protection layer provided in the at least one cover shell section.

13. A method as claimed in claim 12 , wherein a layer of thermoplastic adhesive is deposited on opposed surfaces of the blade spar and the at least one cover shell section prior to attachment of the at least one cover shell section to the blade spar.

14. A method as claimed in claim 12 , wherein the heating includes passing an electric current through the electrically conductive layer provided in the at least one cover shell section.

15. A method as claimed in claim 12 , wherein the same thermoplastic adhesive is used to attach the replacement cover shell section as attached the original cover shell sections.

Assignees

• Ratier Figeac Sas

Inventors

• Le-Meur Kevin
• Brion Patrice

Classifications

• B29C73/00

  Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D ({linings for tyres acting locally B60C5/142;} retreading tyres B29D30/54; devices for covering leaks in pipes or hoses F16L55/16) · CPC title

• B64F5/40

  Maintaining or repairing aircraft · CPC title

• F05D2230/80

  Repairing, retrofitting or upgrading methods · CPC title

• F05D2230/90

  Coating; Surface treatment · CPC title

• F01D5/147 Primary

  Construction, i.e. structural features, e.g. of weight-saving hollow blades (F01D5/148, F01D5/16 and F01D5/20 take precedence; blade shape F01D5/141; blades with cooling or heating channels or cavities F01D5/18; heating, heat-insulating or cooling means on blades F01D5/18) · CPC title