# US 8,770,935 B2 · Propeller arrangement > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 8,770,935 B2 - Document ID: US8770935B2 - Status: Granted - Kind: B2 - Application number: 13/027,653 - Filed: 2011-02-15 - Published: 2011-09-15 - Granted: 2014-07-08 - Earliest claimed: 2010-03-09 - Assignees: ROLLS-ROYCE plc - Applicants: Alexander V. Lavrenko - Inventors: Alexander V. Lavrenko - Web page: https://patentgrep.com/patent/US8770935B2 ## CPC - B64C 11/003: {Variable-diameter propellers; Mechanisms therefor} - B64C 11/48: Units of two or more coaxial propellers - B64D 27/33: Hybrid electric aircraft - B64D 27/026: {comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine (Hybrid electric aircraft B64D27/33)} - B64C: AEROPLANES; HELICOPTERS - B64D: EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT ## Abstract A propeller arrangement has a first propeller assembly providing a row of first propellers, and a second propeller assembly, rearward of the first propeller assembly, providing a row of second propellers. The first and second propellers are radially extendable and retractable. The propeller arrangement further has a control system for controlling the extension and retraction of the first and second propellers. The control system is arranged such that when the propellers of one of the first and second propeller assemblies extend, the propellers of the other of the first and second assemblies retract. ## Claims ### Claim 1 A propeller arrangement having: a first propeller assembly providing a row of first propellers, and a second propeller assembly, rearward of the first propeller assembly, providing a row of second propellers, the first and second propellers being unitary components and radially extendable and retractable, and a control system configured with a controller so as to control the extension and retraction of the first and second propellers; the control system is arranged such that when the propellers of one of the first and second propeller assemblies extend, the propellers of the other of the first and second assemblies retract. ### Claim 2 (depends on 1) A propeller arrangement according to claim 1, wherein the first propeller assembly and the second propeller assembly are contra-rotating. ### Claim 3 (depends on 1) A propeller arrangement according to claim 1, wherein the control system is hydraulically powered. ### Claim 4 (depends on 3) A propeller arrangement according to claim 3, wherein the control system comprises a plurality of first hydraulic chambers operatively connected to respective roots of the first propellers and a plurality of second hydraulic chambers operatively connected to respective roots of the second propellers, the first and second hydraulic chambers being arranged such that varying the hydraulic pressure therein applies a radial force on the respective propellers, and the control system allowing hydraulic pressure to be transmitted between the first and second chambers, whereby, when the propellers of one of the first and second propeller assemblies extend, the pressure of hydraulic fluid in the corresponding hydraulic chambers varies and is transmitted to the hydraulic chambers of the other of the first and second propeller assemblies, causing the propellers of the other of the first and second assemblies to retract. ### Claim 5 (depends on 4) A propeller arrangement according to claim 4, wherein the hydraulic chambers are arranged such that increasing the hydraulic pressure in the hydraulic chambers applies a radially inward force on the respective propellers. ### Claim 6 (depends on 4) A propeller arrangement according to claim 4, wherein each hydraulic chamber is provided by a respective hydraulic cylinder and piston arrangement. ### Claim 7 (depends on 6) A propeller arrangement according to claim 6, wherein the roots of the propellers form the pistons of the cylinder and piston arrangements. ### Claim 8 (depends on 4) A propeller arrangement according to claims 4, wherein the control system provides a first operating mode in which the first propellers extend under centrifugal force, whereby the pressure of hydraulic fluid in the first chambers varies and is transmitted to hydraulic fluid in the second chambers, causing the second propellers to retract against centrifugal force acting thereon. ### Claim 9 (depends on 8) A propeller arrangement according to claim 8, wherein, under the first operating mode, the tips of the first propellers are extended radially further outwards of the tips of the second propellers. ### Claim 10 (depends on 8) A propeller arrangement according to claim 8, wherein the control system further comprises a hydraulic pressure power source which is operatively connected to the roots of the second propellers, the control system providing a second operating mode in which the hydraulic pressure power source operates on the second propellers to cause them to extend, whereby the pressure of hydraulic fluid in the second chambers varies and is transmitted to hydraulic fluid in the first chambers, causing the first propellers to retract against centrifugal force acting thereon. ### Claim 11 (depends on 10) A propeller arrangement according to claim 10, wherein, under the second operating mode, the tips of the second propellers are extended radially towards the tips of the first propellers. ### Claim 12 (depends on 10) A propeller arrangement according to claim 10, wherein the control system provides a third operating mode in which the first hydraulic chambers are isolated from the second hydraulic chambers, preventing hydraulic pressure being transmitted therebetween. ### Claim 13 (depends on 1) A propeller arrangement according to claim 1, wherein the control system is electrically powered. ### Claim 14 (depends on 1) A turboprop engine having the propeller arrangement according to claim 1. ### Claim 15 A turboprop engine having a propeller arrangement having: a first propeller assembly providing a row of first propellers, and a second propeller assembly, rearward of the first propeller assembly, providing a row of second propellers, the first and second propellers being radially extendable and retractable, and a control system configured with a controller so as to control the extension and retraction of the first and second propellers; the control system is arranged such that when the propellers of one of the first and second propeller assemblies extend, the propellers of the other of the first and second assemblies retract. ### Claim 16 A propeller arrangement having: a first propeller assembly providing a row of first propellers, and a second propeller assembly, rearward of the first propeller assembly, providing a row of second propellers, the first and second propellers being unitary components and radially extendable and retractable by actuation at their roots, and a control system configured with a controller so as to control the extension and retraction of the first and second propellers; the control system is arranged such that when the propellers of one of the first and second propeller assemblies extend, the propellers of the other of the first and second assemblies retract.