Blade pitch varying mechanism

Claim 2

A gas turbine engine comprising: (a) a stationary member; (b) first and second rotating members coaxially disposed about said stationary member; (c) an annular gas flowpath coaxial with said first and second rotating members; (d) a plurality of first and second rotor blades attached to said first and second rotating members, respectively, and extending into said flowpath such that a gas stream flowing through said flowpath causes said first and said second rotating members to counterrotate; (e) a plurality of forward and aft variable pitch propulsor blades coupled to and disposed radially outwardly of said first and second rotating members, respectively; (f) a driven gear coaxially coupled to one of said propulsor blades whereby angular displacement of said driven gear with respect to a radius of said rotating member causes a pitch change of said propulsor blade; (g) a driving gear coupled to said driven gear, one of said driven gear and said driving gear being an internal gear and the other of said driven gear and said driving gear being a pinion gear, said internal gear being eccentrically disposed about said pinion gear and having more gear teeth than does said pinion gear with the gear teeth of both said internal gear and said pinion gear being dimensioned for intermeshing; and (h) means for eccentrically revolving said driving gear with respect to said driven gear whereby said driven gear is angularly displaced in response to said driving gear for changing blade pitch.

Claim 3

A gas turbine engine in accordance with claim 1 wherein; (a) said driven gear comprises said pinion gear; and (b) said driving gear comprises said internal gear.

Claim 4

A gas turbine engine in accordance with claim 2 further comprising means for preventing angular rotation of said internal gear with respect to a radius of said rotating member.

Claim 5

A gas turbine engine in accordance with claim 2 wherein said revolving means comprise: (a) a first circular member coupled to said rotating member; (b) means for eccentrically rotating said first circular member with respect to said rotating structure; and (c) means for converting the eccentric rotation of said first circular member into a revolving motion of said internal gear about said pinion gear.

Claim 6

A gas turbine engine in accordance with claim 4 further comprising means for preventing angular rotation of said internal gear with respect to said rotating member.

Claim 7

A gas turbine engine in accordance with claim 5 wherein said internal gear is on an internal surface of a rigid annulus.

Claim 8

A gas turbine engine in accordance with claim 6 wherein said converting means comprise a first circular void within said annulus and dimensioned to receive said first circular member whereby the eccentric rotation of said first circular member with respect to said rotating member causes each point on said annulus to move in a circular path thereby causing said internal gear to revolve about said pinion gear.

Claim 9

A gas turbine engine in accordance with claim 7 wherein said means for eccentrically rotating said first circular member comprises: (a) a shaft rotatably coupled to said rotating member and rotatable, with respect to said rotating member, about a longitudinal axis of said shaft, said first circular member being eccentrically fixed to said shaft whereby rotation of said shaft with respect to said rotating member causes said first circular member to eccentrically rotate with respect to said rotating member; and (b) motor means coupled to said shaft for rotating said shaft.

Claim 10

A gas turbine engine in accordance with claim 8 wherein said motor means comprise a hydraulic motor.

Claim 11

A gas turbine engine in accordance with claim 7 wherein said means for preventing angular rotation of said internal gear with respect to said rotating member comprises: (a) a second circular void within said annulus; (b) a second circular member within said second void and eccentrically coupled to said rotating member whereby the eccentricity of said second circular member is substantially equivalent to the eccentricity of said first circular member; and (c) means for synchronizing the rotation of said first circular member with the relative rotation of said second circular member.

Claim 12

A gas turbine engine in accordance with claim 10 further comprising means for synchronizing the pitch of all said propulsor blades.

Claim 13

A gas turbine engine in accordance with claim 10 further comprising blade pitch varying means coupled to each of said propulsor blades.

Claim 14

A gas turbine engine in accordance with claim 12 further comprising means for synchronizing the pitch of all of said propulsor blades.

Claim 15

In a gas turbine engine including a stationary member, a rotating structure coaxially disposed about the stationary member, and annular gas flowpath coaxial with the rotating structure, a plurality of rotor blades coupled to the rotating structure and extending into the gas flowpath such that a gas stream flowing through the flowpath causes the rotating structure to rotate with respect to the stationary member, and a plurality of variable pitch propulsor blades coupled to and disposed radially outwardly of the rotating structure, means disposed radially outwardly of the annular gas flowpath for varying the pitch of the propulsor blades comprising: (a) a driven gear coaxially coupled to one of the propulsor blades whereby angular displacement of said driven gear with respect to the rotating structure causes angular displacement of the propulsor blade with respect to the rotating structure; (b) a driving gear coupled to said driven gear, one of said driven gear and said driving gear being an internal gear and the other of said driven gear and said driving gear being a pinion gear, said internal gear being eccentrically disposed about said pinion and having more gear teeth than does said pinion gear with the gear teeth of both said internal gear and said pinion gear being dimensioned for intermeshing; and (c) means for eccentrically revolving said driving gear with respect to said driven gear whereby said driven gear is angularly displaced with respect to the rotating structure.

Claim 16

In a gas turbine engine including a stationary member, a rotating structure coaxially disposed about the stationary member, and annular gas flowpath coaxial with the rotating structure, a plurality of rotor blades coupled to the rotating structure and extending into the gas flowpath such that a gas stream flowing through the flowpath causes the rotating structure to rotate with respect to the stationary member, and a plurality of variable pitch propulsor blades coupled to and disposed radially outwardly of the rotating structure, means disposed radially outwardly of the annular gas flowpath for varying the pitch of the propulsor blades comprising: (a) a driven gear coaxially coupled to one of the propulsor blades whereby angular displacement of said driven gear with respect to the rotating structure causes angular displacement of the propulsor blade with respect to the rotating structure; (b) a driving gear coupled to said driven gear, one of said driven gear and said driving gear being an internal gear and the other of said driven gear and said driving gear being a pinion gear, said internal gear being eccentrically disposed about said pinion and having more gear teeth than does said pinion gear with the gear teeth of both said internal gear and said pinion gear being dimensioned for intermeshing; and (c) means for eccentrically revolving said driving gear with respect to said driven gear whereby said driven gear is angularly displaced with respect to the rotating structure.

Claim 17

Blade pitch varying means in accordance with claim 14 wherein: (a) said driven gear comprises said pinion gear; and (b) said driving gear comprises said internal gear.

Claim 18

Blade pitch varying means in accordance with claim 15 further comprising means for preventing angular rotation of said internal gear with respect to the rotating structure.

Claim 19

Blade pitch varying means in accordance with claim 15 wherein said revolving means comprise: (a) a first circular member coupled to the rotating structure; (b) means for eccentrically rotating said first circular member with respect to the rotating structure; and (c) means for converting the eccentric rotation of said first circular member into a revolving motion of said internal gear about said pinion.

Claim 20

Blade pitch varying means in accordance with claim 17 further comprising means for preventing angular rotation of said internal gear with respect to the rotating structure.

Claim 21

Blade pitch varying means in accordance with claim 18 wherein said internal gear is on an internal surface of a rigid annulus.

Claim 22

Blade pitch varying means in accordance with claim 19 wherein said converting means comprise a first circular void within said annulus dimensioned to receive said first circular member whereby the eccentric rotation of said first circular member with respect to the rotating structure causes each point on said annulus to move in a circular path thereby causing said internal gear to revolve about said pinion.

Claim 23

Blade pitch varying means in accordance with claim 20 wherein said means for eccentrically rotating said first circular member comprises: (a) a shaft rotatably coupled to the rotating structure and rotatable, with respect to the rotating structure, about a longitudinal axis of said shaft, said first circular member being eccentrically fixed to said shaft whereby rotation of said shaft with respect to the rotating structure causes said first circular member to eccentrically rotate with respect to the rotating structure; and (b) motor means coupled to said shaft for rotating said shaft.

Claim 24

Blade pitch varying means in accordance with claim 21 wherein said motor means comprise a hydraulic motor.

Claim 25

Blade pitch varying means in accordance with claim 21 wherein said means for preventing angular rotation of said internal gear with respect to the rotating structure comprises: (a) a second circular void within said annulus; (b) a second circular member within said second void and eccentrically coupled to the rotating structure whereby the eccentricity of said second circular member is substantially equivalent to the eccentricity of said first circular member; (c) means for synchronizing the rotation of said first circular member with the relative rotation of said second circular member.

Claim 26

Blade pitch varying means in accordance with claim 23 further comprising means for sunchronizing the pitch of all the propulsor blades.

Claim 27

Blade pitch varying means in accordance with claim 23 further comprising blade pitch varying means coupled to each of the propulsor blades.

Claim 28

Blade pitch varying means in accordance with claim 25 further comprising means for synchronizing the pitch of all of the propulsor blades.

Claim 29

In a gas turbine engine including a rotating structure and a plurality of variable pitch propulsor blades extending radially outwardly from the rotating structure, means for varying the pitch of each of the blades comprising: (a) a driven gear coaxially coupled about a root of the propulsor blades whereby rotation of said driven gear with respect to a radius of the rotating structure causes a pitch change of a corresponding propulsor blade; (b) a driving gear operatively coupled to said driven gear, one of said driven gear and said driving gear being an internal gear and the other of said driven gear and said driving gear being a pinion gear, said internal gear being eccentrically disposed about said pinion and having more gear teeth than does said pinion gear with the gear teeth of both said internal gear and said pinion being dimensioned for intermeshing; and (c) means for eccentrically revolving said driving gear with respect to said driven gear, said driven gear being angularly displaced with resepect to a radius of the rotating structure in response to eccentric motion of said driving gear.

Claim 30

In a gas turbine engine including a rotating structure and a plurality of variable pitch propulsor blades extending radially outwardly from the rotating structure, means for varying the pitch of each of the blades comprising: (a) a driven gear coaxially coupled about a root of the propulsor blades whereby rotation of said driven gear with respect to a radius of the rotating structure causes a pitch change of a corresponding propulsor blade; (b) a driving gear operatively coupled to said driven gear, one of said driven gear and said driving gear being an internal gear and the other of said driven gear and said driving gear being a pinion gear, said internal gear being eccentrically disposed about said pinion and having more gear teeth than does said pinion gear with the gear teeth of both said internal gear and said pinion being dimensioned for intermeshing; and (c) means for eccentrically revolving said driving gear with respect to said driven gear, said driven gear being angularly displaced with resepect to a radius of the rotating structure in response to eccentric motion of said driving gear.

Claim 31

Blade pitch varying means in accordance with claim 27 wherein: (a) said driven gear comprises said pinion; and (b) said driving gear comprises said internal gear.

Claim 32

Blade pitch varying means in accordance with claim 28 further comprising means for preventing angular rotation of said internal gear with respect to the rotating structure.

Claim 33

Blade pitch varying means in accordance with claim 28 wherein said revolving means comprise: (a) a first circular member coupled to the rotating structure; (b) means for eccentrically rotating said first circular member with respect to the rotating structure; and (c) means for converting the eccentric rotation of said first circular member into a revolving motion of said internal gear about said pinion.

Claim 34

Blade pitch varying means in accordance with claim 30 further comprising means for preventing angular rotation of said internal gear with respect to the rotating structure.

Claim 35

Blade pitch varying means in accordance with claim 31 wherein said internal gear is on an internal surface of a rigid annulus.

Claim 36

Blade pitch varying means in accordance with claim 32 wherein said converting means comprise a first circular void within said annulus and dimensioned to receive said first circular member whereby the eccentric rotation of said first circular member with respect to the rotating structure causes each point on said annulus to move in a circular path thereby causing said internal gear to revolve about said pinion.

Claim 37

Blade pitch varying means in accordance with claim 33 wherein said means for eccentricaly rotating said first circular member comprises: (a) a shaft rotatably coupled to the rotating structure and rotatable, with respect to the rotating structure, about a longitudinal axis of said shaft, said first circular member being eccentrically fixed to said shaft whereby rotation of said shaft with respect to the rotating structure causes said first circular member to eccentrically rotate with respect to the rotating structure; and (b) motor means coupled to said shaft for rotating said shaft.

Claim 38

Blade pitch varying means in accordance with claim 34 wherein said motor means comprise a hydraulic motor.

Claim 39

Blade pitch varying means in accordance with claim 34 wherein said means for preventing angular rotation of said internal gear with respect to the rotating structure comprises: (a) a second circular void within said annulus; (b) a second circular member within said second void and eccentrically coupled to the rotating structure whereby the eccentricity of said second circular member is substantially equivalent to the eccentricity of said first circular member; and (c) means for synchronizing the rotation of said first circular member with the relative rotation of said second circular member.

Claim 40

Blade pitch varying means in accordance with claim 36 further comprising means for synchronizing the pitch of all the propulsor blades.

Claim 41

Blade pitch varying means in accordance with claim 36 further comprising blade pitch varying means coupled to each of the propulsor blades.

Claim 42

Blade pitch varying means in accordance with claim 38 further comprising means for synchronizing the pitch of all of the propulsor blades.