# US 10,479,483 B2 · Pitch control assembly and propeller assembly and method of adjusting pitch > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,479,483 B2 - Document ID: US10479483B2 - Status: Granted - Kind: B2 - Application number: 15/196,145 - Filed: 2016-06-29 - Published: 2017-01-12 - Granted: 2019-11-19 - Earliest claimed: 2015-07-08 - Assignees: GE Aviation Systems LLC - Applicants: Ge Aviation Systems LLC - Inventors: David Raju Yamarthi; Rajendra Vishwanath Pawar; Amit Arvind Kurvinkop; Sandeep Kumar; Murugesan Periasamy; Ravindra Shankar Ganiger; Bajarang Agrawal; Nagashiresha G. - Web page: https://patentgrep.com/patent/US10479483B2 ## CPC - B64C 11/38: fluid, e.g. hydraulic - B64C: AEROPLANES; HELICOPTERS ## Abstract Pitch control assembly and propeller blade assembly having a spider hub are disclosed. The spider hub includes a hub and a set of arms spaced circumferentially about the hub and projecting radially from the hub, wherein the set of arms are configured to receive a set of blades such that a blade root of a blade is rotationally mountable into an arm included in the set of arms, a crosshead located within the hub and axially moveable relative to the hub, a torque tube located in the arm and extending into the hub, wherein a pitch angle of the blade can be adjusted by axially moving the crosshead to rotate the torque tube to effect a corresponding rotation of the blade. ## Claims ### Claim 1 A propeller assembly, comprising: a spider hub comprising a hub defining an interior and a set of arms spaced circumferentially about the hub and projecting radially from the hub, wherein the set of arms are configured to receive a set of blades such that a blade root of a blade of the set of blades is rotationally mounted to an outer periphery of an arm included in the set of arms; a crosshead located within the interior of the hub and axially moveable relative to the hub; a torque tube located in the arm and extending into the hub, and having opposing first and second ends, with the first end configured to mount to a proximal most portion of the blade of the set of blades, the torque tube spanning a length, between the first end and second end, from the outer periphery of the arm to the interior of the hub; and a motion converter located within the interior of the hub and coupling the crosshead to the second end of the torque tube, the motion converter configured for converting axial movement of the crosshead into rotational movement of the torque tube and a pitch angle of the blade can be adjusted by axially moving the crosshead to rotate the torque tube to effect a corresponding rotation of the blade. ### Claim 2 (depends on 1) The propeller assembly of claim 1 wherein the motion converter includes a link fixedly mounted to the torque tube and a needle bearing pivotally coupling the link to the crosshead. ### Claim 3 (depends on 2) The propeller assembly of claim 2 wherein the crosshead includes a crosshead flange that includes a pair of spaced rails provided on the crosshead to define a channel between the pair of spaced rails, and the needle bearing includes a bearing retained within the channel. ### Claim 4 (depends on 3) The propeller assembly of claim 3 wherein the bearing is rotatably mounted to the link. ### Claim 5 (depends on 3) The propeller assembly of claim 3 wherein the first end of the torque tube is fixedly mounted to the blade root. ### Claim 6 (depends on 5) The propeller assembly of claim 5 wherein the first end of the torque tube is keyed to the blade root. ### Claim 7 (depends on 5) The propeller assembly of claim 5, further comprising a bushing located within the arm and configured for supporting the second end of the torque tube. ### Claim 8 (depends on 2) The propeller assembly of claim 2 wherein the motion converter is configured to pivot at a first end, which is rotatably connected to the crosshead, and fixedly mounted to the torque tube at a second end. ### Claim 9 (depends on 1) The propeller assembly of claim 1 wherein the blade root does not extend into the hub. ### Claim 10 A pitch control assembly for a propeller comprising a spider hub having a hub with a set of arms, and a set of blades rotatably mounted to the set of arms, comprising: a crosshead configured for axial movement relative to the hub, the crosshead spaced from the set of blades and having a crosshead flange that includes a pair of spaced rails provided on the crosshead to define a channel between the pair of spaced rails; a torque tube having a first end opposing a second end, with the first end configured to fixedly mount to a blade included in the set of blades and the second end extending into the hub; and a motion converter including a link fixedly mounted to the torque tube and a needle bearing pivotally coupling the link to the crosshead, wherein the needle bearing includes a bearing retained within the channel, the motion converter adapted to convert the axial movement of the crosshead into rotational movement of the torque tube; wherein a pitch angle of the blade is adjusted by axially moving the crosshead to rotate the torque tube to effect a corresponding rotation of the blade included in the set of blades. ### Claim 11 (depends on 10) The pitch control assembly of claim 10 wherein the bearing is rotatably mounted to the link. ### Claim 12 (depends on 11) The pitch control assembly of claim 11 wherein the link is fixedly mounted to the second end of the torque tube. ### Claim 13 (depends on 10) The pitch control assembly of claim 10 wherein the torque tube extends outside of the hub.