Composite aircraft propeller blade

Claim 2

A composite aircraft propeller blade adapted to provide for a smooth transfer of centrifugal and bending forces to a propeller hub member, said propeller blade comprising a rigid base retention plug having a radially inner end surface, a core of spacer material extending outwardly from said base plug and having opposite side surfaces converging together, a series of overlapping plies of resin-bonded fibrous plastics material overlying each of said side surfaces of said core, each of said plies including substantially parallel reinforcing fibers, a resin-bonded outer covering on said overlapping plies and forming the outer surface of said blade, said resin-bonded overlapping plies and outer covering forming leading and trailing blade edge portions projecting substantially forwardly and rearwardly from said base plug, a first portion of said plies and corresponding said reinforcing fibers on both of said side surfaces of said core extending inwardly around said inner end surface of said base plug and being bonded to said inner end surface, and means for securing said base plug to the hub member.

Claim 3

A propeller blade as defined in claim 1 wherein said base plug has a generally wedge-shaped cross-sectional configuration with said inner surface disposed within a generally dovetail-shape recess within the hub member, and said first portion of said plies extend adjacent said inner surface within the recess.

Claim 4

A propeller blade as defined in claim 1 wherein said base plug includes horn portions projecting into said portions of said blade from an intermediate portion, and said horn portions cooperate to form said inner surface receiving said first portion of said plies.

Claim 5

A propeller blade as defined in claim 3 wherein said intermediate portion of said base plug extends into a recess within the hub member, and said intermediate portion cooperates to form said inner surface receiving said first portion of said plies.

Claim 6

A propeller blade as defined in claim 1 wherein said fiber of said first portion of said plies extend generally parallel to a longitudinal axis of said blade to provide said blade with substantial bending stiffness relative to the hub member.

Claim 7

A propeller blade as defined in claim 5 wherein a second portion of said plies comprises substantially parallel fibers orientated at an angle with respect to said longitudinal axis to provide the blade with substantial torsional stiffness relative to the hub member.

Claim 8

A propeller blade as defined in claim 6 wherein said fibers in said second portion of said plies extend at both positive and negative angles with respect to said longitudinal axis.

Claim 9

A propeller blade as defined in claim 6 wherein said first portion of said plies overlie said second portion of said plies.

Claim 10

A propeller blade as defined in claim 1 wherein said base plug defines a cavity, and said spacer material forming said core extends into said cavity.

Claim 11

A propeller blade as defined in claim 1 and including a low modulus material forming one of said inner edge portions of said blade to provide for a generally uniform and smooth transfer of forces from said trailing inner edge portion through said base plug to said hub member.

Claim 12

A propeller blade as defined in claim 1 wherein said first portion of said plies extending around said base plug are interleaved in an alternating manner adjacent said inner surface of said base plug.

Claim 13

A propeller blade as defined in claim 1 wherein said inner surface of said base plug is generally concaved and defines a cavity receiving said first portion of said plies, and a wedge-shaped shank member projecting into said cavity in conforming relation and bonded to said first portion of said plies.

Claim 14

A propeller blade as defined in claim 1 wherein said first portion of said plies extending around said inner surface of said base plug form a precision base surface, and a set of metal corner shells bonded to said base surface.

Claim 15

A propeller blade as defined in claim 1 wherein said core of spacer material extends outwardly from said base plug by a distance less than one half of the overall length of said propeller blade.

Claim 16

A propeller blade as defined in claim 13 wherein the hub member has opposing retention lips defining an undercut recess, said base plug has a wedge-shaped inner portion forming said inner surface, and said wedge-shaped inner portion cooperates with said corner shells and the retention lips to compress said first portion of said plies therebetween.

Claim 17

A composite aircraft propeller blade adapted to provide for a smooth transfer of centrifugal and bending forces to a propeller hub member defining an undercut recess for receiving a base portion of the blade, said propeller blade comprising a rigid base retention plug having a radially inner end surface, a core of spacer material extending outwardly from said base plug and having opposite side surfaces converging together, a series of overlapping plies of resin-bonded fibrous plastics material overlying each of said side surfaces of said core, each of said plies including substantially parallel reinforcing fibers, a resin-bonded outer covering on said overlapping plies and forming the outer surface of said blade, said resin-bonded overlapping plies and outer covering forming leading and trailing blade edge portions projecting substantially forwardly and rearwardly from said base plug, a first portion of said plies and corresponding said reinforcing fibers on both of said side surfaces of said core including inner edge portions extending inwardly around said base plug and overlying said inner end surface of said base plug, said edge portions of said plies extending from one side of said core being interleaved with said edge portions of said plies extending from the other side of said core and being bonded to said inner end surface, and means for securing said base plug within the recess of the hub member.

Claim 18

A composite aircraft propeller blade adapted to provide for a smooth transfer of centrifugal and bending forces to a propeller hub member defining an undercut recess for receiving a base portion of the blade, said propeller blade comprising a rigid base retention plug having a radially inner end surface, a core of spacer material extending outwardly from said base plug and having opposite side surfaces converging together, a series of overlapping plies of resin-bonded fibrous plastics material overlying each of said side surfaces of said core, each of said plies including substantially parallel reinforcing fibers, a resin-bonded outer covering on said overlapping plies and forming the outer surface of said blade, said resin-bonded overlapping plies and outer covering forming leading and trailing blade edge portions projecting substantially forwardly and rearwardly from said base plug, a first portion of said plies and corresponding said reinforcing fibers on both of said side surfaces of said core including inner edge portions extending inwardly around said base plug and overlying said inner end surface of said base plug, said edge portions of said plies extending from one side of said core being interleaved with said edge portions of said plies extending from the other side of said core and being bonded to said inner end surface, and means for securing said base plug within the recess of the hub member.

Claim 19

A propeller blade as defined in claim 16 wherein said fibers of said first portion of said plies extend generally parallel to a longitudinal axis of said blade to provide said blade with substantial bending stiffness relative to the hub member.

Claim 20

A propeller blade as defined in claim 17 wherein a second portion of said plies comprises substantially parallel fibers orientated at both positive and negative angles with respect to said longitudinal axis to provide the blade with substantial torsional stiffness relative to the hub member, and said first portion of said plies overlie said second portion of said plies.

Claim 21

A propeller blade as defined in claim 16 and including a low modulus material forming one of said inner edge portions of said blade to provide for a generally uniform and smooth transfer of forces from said one inner edge portion through said base plug to said hub member.

Claim 22

A propeller blade as defined in claim 16 wherein said inner end surface of said base plug is generally concaved and defines a cavity receiving said edge portions of said plies arranged in an interleaving manner, and a wedge-shaped shank member projecting into said cavity in conforming relation and bonded to said edge portions of said plies.

Claim 23

A propeller blade as defined in claim 16 and including a set of metal corner shells bonded to said edge portions of said plies extending around said base plug.

Claim 24

A propeller blade as defined in claim 21 wherein the hub member has opposing retention lips defining an undercut said recess, and said base plug has rounded corner portions cooperating with said corner shells and the retention lips to compress said first portion of said plies therebetween.

Claim 25

A propeller blade as defined in claim 16 wherein said base plug includes horn portions projecting into said portions of said blade from an intermediate portion, said intermediate portion projects into the recess and forms said inner end surface, and said first portion of said plies also extend around each of said horn portions of said base plug.

Claim 26

A composite aircraft propeller blade adapted to provide for a smooth transfer of centrifugal and bending forces to a propeller hub member, said propeller blade comprising a rigid base retention plug having an inner end surface, a core of spacer material extending outwardly from said base plug and having opposite side surfaces converging together, a series of overlapping plies of resin-bonded fibrous plastics material overlying each of said side surfaces of said core, each of said plies including substantially parallel reinforcing fibers, a resin-bonded outer covering on said overlapping plies and forming the outer surface of said blade, said resin-bonded overlapping plies and outer covering forming leading and trailing blade edge portions projecting substantially forwardly and rearwardly from said base plug, a first portion of said plies on both of said side surfaces of said core having said fibers orientated at substantial angles with respect to a longitudinal axis of said blade to provide said blade with substantial torsional stiffness relative to the hub member, a second portion of said plies overlying said first portion of said plies on both of said side surfaces of said core and having said fibers orientated generally parallel with respect to said longitudinal axis to provide the blade with substantial bending stiffness relative to the hub member, said second portion of said plies and corresponding said fibers having inner portions extending inwardly around said base plug and overlying said inner end surface of said base plug and being bonded to said inner end surface, and means for securing said base plug to the hub member.

Claim 27

A composite aircraft propeller blade adapted to provide for a smooth transfer of centrifugal and bending forces to a propeller hub member, said propeller blade comprising a rigid base retention plug having an inner end surface, a core of spacer material extending outwardly from said base plug and having opposite side surfaces converging together, a series of overlapping plies of resin-bonded fibrous plastics material overlying each of said side surfaces of said core, each of said plies including substantially parallel reinforcing fibers, a resin-bonded outer covering on said overlapping plies and forming the outer surface of said blade, said resin-bonded overlapping plies and outer covering forming leading and trailing blade edge portions projecting substantially forwardly and rearwardly from said base plug, a first portion of said plies on both of said side surfaces of said core having said fibers orientated at substantial angles with respect to a longitudinal axis of said blade to provide said blade with substantial torsional stiffness relative to the hub member, a second portion of said plies overlying said first portion of said plies on both of said side surfaces of said core and having said fibers orientated generally parallel with respect to said longitudinal axis to provide the blade with substantial bending stiffness relative to the hub member, said second portion of said plies and corresponding said fibers having inner portions extending inwardly around said base plug and overlying said inner end surface of said base plug and being bonded to said inner end surface, and means for securing said base plug to the hub member.

Claim 28

A propeller blade as defined in claim 24 wherein said fibers in said first portion of said plies extend at both positive and negative angles with respect to said longitudinal axis.

Claim 29

A propeller blade as defined in claim 24 wherein said base plug defines an elongated cavity having a U-shaped cross-sectional configuration, and said spacer material forming said core extends into said cavity.

Claim 30

A propeller blade as defined in claim 24 and including a low modulus material forming said trailing inner edge portion of said blade to provide for a generally uniform and smooth transfer of forces from said trailing inner edge portion through said base plug to said hub member.

Claim 31

A propeller blade as defined in claim 24 wherein said second portion of said plies extending around said base plug are interleaved in an alternating manner adjacent said inner surface of said base plug.

Claim 32

A propeller blade as defined in claim 24 wherein said inner surface of said base plug is generally concaved and defines a cavity receiving said second portion of said plies, and a wedge-shaped shank member projecting into said cavity in conforming relation and bonded to said second portion of said plies.

Claim 33

A propeller blade as defined in claim 24 wherein said second portion of said plies extending around said base plug and overlying said inner surface form a precision base surface, and a set of metal corner shells bonded to said base surface.

Claim 34

A propeller blade as defined in claim 24 wherein said base plug includes horn portions projecting into said edge portions of said blade from an intermediate portion, and said horn portions cooperate to form said inner surface receiving said second portion of said plies.