Lightweight propeller blade with improved retention capacity

Patent metadata

Field	Value
Publication number	US-9849969-B2
Application number	US-201514663941-A
Country	US
Kind code	B2
Filing date	Mar 20, 2015
Priority date	Mar 20, 2015
Publication date	Dec 26, 2017
Grant date	Dec 26, 2017

Abstract

A propeller blade assembly includes a spar extending along a propeller blade axis and an outer sleeve surrounding the spar portion at a root end of the rotor blade assembly. The spar is adhesively bonded to the outer sleeve at an interface portion. A spar maximum diameter along the interface portion is larger than an outer sleeve minimum diameter along the interface portion. A method of assembling a propeller blade includes installing an outer sleeve over a spar at a root end of the spar, the spar a not fully cured composite component, and urging the spar into compressive conformance with the outer sleeve at an interface portion of the propeller blade assembly. A spar maximum diameter along the interface portion is larger than an outer sleeve minimum diameter along the interface portion. The spar is cured thereby adhesively bonding the spar to the outer sleeve at the interface portion.

First claim

What is claimed is:

1. A propeller blade assembly comprising:
a spar extending along a propeller blade axis;
an outer sleeve surrounding the spar portion at a root end of the rotor blade assembly, the spar adhesively bonded to the outer sleeve at an interface portion, a spar maximum diameter along the interface portion larger than an outer sleeve minimum diameter along the interface portion;
an inner ring disposed in a spar cavity, the inner ring including:
an inboard inner ring; and
an outboard inner ring, the inboard inner ring and the outboard inner ring defining a ring split line transverse to the propeller blade axis; and

a wedge disposed inside of the inner ring, installation of the wedge urging the inner ring into contact with the spar, thus urging the spar into conformal compressive contact with the outer sleeve at the interface portion.

2. The propeller blade assembly of claim 1 , wherein the inner ring is segmented.

3. The propeller blade assembly of claim 1 , wherein the wedge is an inboard wedge and an outboard wedge, relative to the propeller blade axis, the inboard wedge secured to the outboard wedge via one or more bolts.

4. The propeller blade assembly of claim 1 wherein an outer surface of the outer sleeve is configured to interface with one or more bearing rows.

5. The propeller blade assembly of claim 1 , wherein the interface portion is defined by a convex surface of the spar and a complimentary concave surface of the outer sleeve.

6. The propeller blade assembly of claim 1 , wherein the interface portion is defined by a concave surface of the spar and a complimentary convex surface of the outer sleeve.

7. The propeller blade assembly of claim 1 , wherein the spar is formed from a composite material and the outer sleeve is formed from a metal material.

8. A method of assembling a propeller blade comprising:
installing an outer sleeve over a spar at a root end of the spar, the spar a not fully cured composite component;
installing an inner ring in a spar cavity, the inner ring including:
an inboard inner ring; and
an outboard inner ring, the inboard inner ring and the outboard inner ring defining a ring split line transverse to a propeller blade axis;

urging the spar into compressive conformance with the outer sleeve at an interface portion of the propeller blade assembly via a wedge installed inside of the inner ring, a spar maximum diameter along the interface portion larger than an outer sleeve minimum diameter along the interface portion; and
curing the spar thereby adhesively bonding the spar to the outer sleeve at the interface portion.

9. The method of claim 8 , wherein installation of the wedge results in expansion of the inner ring into contact with the spar.

10. The method of claim 8 , wherein the wedge is an inboard wedge and an outboard wedge, relative to the propeller blade axis, the inboard wedge is tightened to the outboard wedge via one or more bolts;
wherein the tightening of the inboard wedge to the outboard wedge urges the inner ring into contact with the spar.

11. The method of claim 8 , further comprising preforming the interface portion of the spar prior to installing the outer sleeve over the spar.

12. The method of claim 8 , wherein the interface portion is defined by a convex surface of the spar and a complimentary concave surface of the outer sleeve.

13. The method of claim 8 , wherein the interface portion is defined by a concave surface of the spar and a complimentary convex surface of the outer sleeve.

Assignees

• Hamilton Sundstrand Corp
• Hamilton Sunstrand Corp

Inventors

• Nagle David P
• Smith Stephen L

Classifications

• B64C11/06

  for variable-pitch blades · CPC title

• B64C2027/4736

  from composite materials · CPC title

• B64C11/26 Primary

  Fabricated blades · CPC title