# US 11,299,265 B2 · Rotor blade folding system > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 11,299,265 B2 - Document ID: US11299265B2 - Status: Granted - Kind: B2 - Application number: 16/426,787 - Filed: 2019-05-30 - Published: 2020-12-03 - Granted: 2022-04-12 - Earliest claimed: 2019-05-30 - Assignees: Lockheed Martin Corporation - Applicants: Lockheed Martin Corporation - Inventors: David N. Schmaling; Andrew C. Goodwin; Yair Preiss - Web page: https://patentgrep.com/patent/US11299265B2 ## CPC - B64C 27/50: Blades foldable to facilitate stowage of aircraft - B64C 27/10: arranged coaxially - B64C 27/48: Root attachment to rotor head - B64C: AEROPLANES; HELICOPTERS ## Abstract A rotor blade attachment assembly for use with a rotor hub to which a rotor blade assembly is connected includes a hub extender having an inboard end and an outboard end. The inboard end of the hub extender is configured to form a connection with the rotor hub. A blade fold axis about which the rotor blade rotates relative to the rotor hub is defined at the connection. An inboard bearing is mounted within an interior of the hub extender adjacent the inboard end and an outboard hearing is mounted within the interior of the hub extender adjacent the outboard end. A tension torsion strap is operably coupled to the inboard bearing and the outboard bearing. ## Claims ### Claim 1 A rotor blade attachment assembly for use with a rotor hub to which a rotor blade assembly is connected, the rotor blade attachment assembly comprising: a hub extender having an inboard end and an outboard end, wherein the inboard end of the hub extender is configured to form a connection with the rotor hub, wherein a blade fold axis about which the rotor blade rotates relative to the rotor hub is defined at the connection; an inboard bearing mounted within an interior of the hub extender adjacent the inboard end; an outboard bearing mounted within an interior of the hub extender adjacent the outboard end; a tension torsion strap operably coupled to the inboard bearing and the outboard bearing; an anchor located within the interior of the hub extender, the anchor being coupled to the tension torsion strap at a pin connection disposed at a first end of the tension torsion strap; and a pitch control coupling coupled to the inboard bearing, wherein the pitch control coupling includes a first portion having a C-like shape, the first portion configured to surround a first side of the inboard bearing. ### Claim 2 (depends on 1) The rotor blade attachment assembly of claim 1, wherein the inboard end includes a clevis having an upper portion and a lower portion, the connection being formed at both the upper portion and the lower portion. ### Claim 3 (depends on 1) The rotor blade attachment assembly of claim 1, wherein at least one of the inboard bearing and the outboard bearing is an elastomeric bearing. ### Claim 4 (depends on 1) The rotor blade attachment assembly of claim 1, wherein the hub extender is formed from a composite material. ### Claim 5 (depends on 1) The rotor blade attachment assembly of claim 1, wherein a cross-sectional area of the hub extender reduces over a length of the hub extender. ### Claim 6 (depends on 1) The rotor blade attachment assembly of claim 1, wherein the pitch control coupling is rotatable about a pitch axis. ### Claim 7 (depends on 1) The rotor blade attachment assembly of claim 1, wherein the blade fold axis is located inboard of the inboard bearing. ### Claim 8 (depends on 1) The rotor blade attachment assembly of claim 1, wherein the anchor couples the inboard bearing to a first end of the tension torsion strap. ### Claim 9 (depends on 1) The rotor blade attachment assembly of claim 1, further comprising an outboard bearing bracket located at least partially within the interior of the hub extender, the outboard bearing bracket coupling the outboard bearing to a second end of the tension torsion strap. ### Claim 10 A rotor assembly comprising: a rotor hub rotatable about an axis; a plurality of rotor blade assemblies connected to the rotor hub, wherein the plurality of rotor blade assemblies include a torque tube and at least one of the plurality of rotor blade assemblies includes a blade attachment assembly, the blade attachment assembly including: a rigid hub extender having configured to form a connection with the rotor hub, wherein a blade fold axis of the rotor blade assembly is defined at the connection; at least one bearing mounted within an interior of the hub extender, the at least one bearing including an inboard bearing mounted adjacent an inboard end of the hub extender; a tension torsion strap mounted within the interior of the hub extender, the tension torsion strap being rotatable about a pitch axis of the at least one rotor blade assembly and being translationally fixed relative to the pitch axis of the at least one rotor blade assembly; an anchor located within the interior of the hub extender, the anchor being coupled to the tension torsion strap at a pin connection disposed at a first end of the tension torsion strap; and a pitch control coupling mounted to the torque tube, wherein the pitch control coupling includes a first portion having a C-like shape, the first portion configured to surround a first side of an inboard bearing. ### Claim 11 (depends on 10) The rotor hub assembly of claim 10, wherein the rotor hub further comprises a plurality of hub arms and the connection is formable between an inboard end of the hub extender and one of the plurality of hub arms. ### Claim 12 (depends on 11) The rotor hub assembly of claim 11, wherein the plurality of hub arms includes at least one hub arm having a clevis including an opening, and a portion of the inboard end of the hub extender is receivable within the opening. ### Claim 13 (depends on 11) The rotor hub assembly of claim 11, further comprising a hub fairing mounted to the rotor hub. ### Claim 14 (depends on 13) The rotor hub assembly of claim 13, wherein the hub fairing includes a cut out adjacent the at least one of the plurality of rotor blade assemblies that is foldable about the blade fold axis. ### Claim 15 (depends on 10) The rotor blade assembly of claim 10, wherein the blade attachment assembly further comprises a pitch control assembly rotatable about the pitch axis. ### Claim 16 (depends on 15) The rotor blade assembly of claim 15, wherein the pitch control assembly is operable to rotate the torque tube about the pitch axis. ### Claim 17 (depends on 16) The rotor blade assembly of claim 16, wherein the pitch control assembly further comprises: a horn spindle coupling rotationally mounted to the rotor hub; and the pitch control coupling, wherein the pitch control coupling rotationally engages the horn spindle coupling when the blade attachment assembly is in the flight position. ### Claim 18 (depends on 17) The rotor blade assembly of claim 17, wherein an interface between the pitch control coupling and the horn spindle coupling includes a toothed interlock that rotationally locks the pitch control coupling to the horn spindle coupling. ### Claim 19 (depends on 10) The rotor blade assembly of claim 10, wherein the at least one bearing further includes an outboard bearing mounted adjacent an outboard end of the hub extender, and the tension torsion strap.