Coaxial transmission/center hub subassembly for a rotor assembly having ducted, coaxial counter-rotating rotors

• US 5,351,913 A
• Filed: 06/22/1992
• Issued: 10/04/1994
• Est. Priority Date: 06/22/1992
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Cycon, James P., Millea, Vincent F., Kohlhepp, Fred W.
• Primary Examiner(s): Huppert, Michael S.
• Assistant Examiner(s): BIDWELL, ANNE
• Application Number:
  US07/903,065
• Time in Patent Office: 834 Days
• Field of Search: 244/12.2, 244/23 C, 244/34 A, 244/17.23, 244/17.11, 244/60, 416/115, 416/128, 416/129, 416/98, 416/102
• US Class Current: 244/60
• CPC Class Codes: B64C 27/20 Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
• CPC Class Codes: B64C 27/33 having flexing arms
• CPC Class Codes: B64C 27/605 including swash plate, spider or cam mechanisms
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 20/65 Composite materials
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 2201/20 Remote controls
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 30/24 Coaxial rotors
• CPC Class Codes: B64U 30/26 Ducted or shrouded rotors
• CPC Class Codes: B64U 50/11 using internal combustion piston engines
• CPC Class Codes: B64U 50/14 ducted or shrouded
• CPC Class Codes: B64U 50/20 Transmission of mechanical power to rotors or propellers
• CPC Class Codes: F02B 2075/025 two

Abstract

One embodiment of a coaxial transmission/center hub subassembly for a rotor assembly having ducted, coaxial counter-rotating rotors includes a single stage transmission, a transmission housing, and a center hub support structure that are structurally and functionally interactive. The transmission housing includes upper and lower standpipe housings secured in combination with a middle housing. The single stage transmission includes an input pinion gear rotatably mounted in combination with the middle housing, and upper and lower spiral bevel gears rotatably coupled in combination with the input pinion gear to provide counter-rotation thereof. The spiral bevel gears include integral rotor shafts, respectively, rotatably mounted in the standpipe housings. The hub support structure is configured for securement of the middle housing internally in combination therewith, with respective surfaces thereof in abutting engagement so that dynamic loads of the rotors and thermal loads are directly coupled into the hub support structure via the middle housing while bending moments of the rotors are canceled in the middle housing. The hub support structure has radially extending arms for mounting the coaxial transmission/center hub subassembly in fixed coaxial relation to an airframe structure and for coupling the dynamic and thermal loads to the airframe structure. External surfaces of the standpipe housings function as sliding surfaces for linear motion of swashplate subassemblies to minimize the separation between the rotors so that the airframe structure has a compact aerodynamic and structural envelope. The transmission housing is internally configured to provide a splash lubrication subsystem.

Claims

1. A coaxial transmission/center hub subassembly for a rotor assembly of an aerial vehicle having ducted counter-rotating rotors defining a rotational axis for the aerial vehicle, the aerial vehicle having a toroidal fuselage with a plurality of inwardly extending radial struts and including an engine, the rotor assembly including upper and lower swashplate subassemblies, comprising:

center hub support structure means for mounting said coaxial transmission/center hub assembly in fixed coaxial relation to the toroidal fuselage utilizing the plurality of inwardly extending radial support struts;

a multi-member transmission housing including

an upper standpipe housing secured in combination with said center hub support structure means, and

a lower standpipe housing secured in combination with said center hub support structure means; and

a single stage transmission subsystem including

an upper bevel gear including an upper rotor shaft rotatably mounted in combination in said upper standpipe housing,

a lower bevel gear including a lower rotor shaft rotatably mounted in combination in said lower standpipe housing, said upper and lower rotor shafts providing means for mounting the counter-rotating rotors in combination with said coaxial transmission/center hub subassembly, and

an input gear rotatably mounted in combination in said center hub support structures means, said input gear being mechanically coupled in combination with said upper and lower bevel gears and the engine to couple torque therefrom to the counter-rotating rotors; and

wherein

said upper and lower standpipe housings are secured in combination with said center hub support structure means in opposed relation along the rotational axis of the aerial vehicle; and

wherein

external surfaces of said upper and lower standpipe housings provide sliding surfaces for bi-directional linear movement of the upper and lower swashplate subassemblies, respectively.

2. The coaxial transmission/center hub subassembly of claim 1 wherein said center hub support structure means includes a cylindrical body having at least three integral, outwardly extending radial support arms for rigidly attaching said coaxial transmission/center hub subassembly in combination with the plurality of inwardly extending radial support arms in fixed coaxial relation with the toroid fuselage.

3. The coaxial transmission/center hub subassembly of claim 2 wherein said center hub support structure means further comprises a middle housing secured in combination with said cylindrical body so that external surfaces of said middle housing abuttingly engage internal surfaces of said center hub support structure, said middle housing forming part of said multi-member transmission housing wherein said upper and lower standpipe housings are secured in combination therewith and said input gear is rotatably mounted in combination therein.

4. The coaxial transmission/center hub subassembly of claim 1 wherein said tempter hub support structure means comprises:

a center hub support structure including a cylindrical body having at least three integral, outwardly extending radial support arms for rigidly attaching said coaxial transmission/center hub subassembly in combination with the plurality of inwardly extending radial support struts in fixed coaxial relation with the toroidal fuselage; and

a middle housing secured in combination with said cylindrical body so that external surfaces of said middle housing abuttingly engage internal surfaces of said center hub support structure;

said middle housing forming part of said multi-member transmission housing wherein said upper and lower standpipe housings are secured in combination therewith and said input gear is rotatably mounted in combination therein.

5. The coaxial transmission/center hub subassembly of claim 4 wherein said multi-member transmission housing is internally configured to provide a splash lubrication subsystem for said single stage transmission subsystem.

6. The coaxial transmission/center hub subassembly of claim 4 wherein said multi-member transmission housing includes a splash lubrication subsystem comprising:

said middle housing including a pinion chamber;

said upper and lower standpipe housings having standpipe chambers and cored passages; and

said upper and lower standpipe housings in combination defining a central reservoir for oil for said splash lubrication subsystem;

said central reservoir being fluidically interconnected to said pinion chamber, said standpipe chambers, and said cored passages to define said splash lubrication subsystem;

rotary motion of said upper and lower bevel gears circulating oil through said splash lubrication subsystem.

7. The coaxial transmission/center hub subassembly of claim 1 wherein said center hub support structure means comprises:

a center hub support structure including a cylindrical body having at least three integral, outwardly extending radial support arms for rigidly attaching said coaxial transmission/center hub subassembly in combination with the plurality of inwardly extending radial support struts in fixed coaxial relation with the toroidal fuselage; and

a middle housing fabricated as an integral part of said cylindrical body;

said middle housing forming part of said multi-member transmission housing wherein said upper and lower standpipe housings are secured in combination therewith and said input gear is rotatably mounted in combination therein.

8. The coaxial transmission/center hub subassembly of claim 7 wherein said multi-member transmission housing includes a splash lubrication subsystem comprising:

said middle housing including a pinion chamber;

said upper and lower standpipe housings having standpipe chambers and cored passages; and

said upper and lower standpipe housings in combination defining a central reservoir for oil for said splash lubrication subsystem;

said central reservoir being fluidically interconnected to said pinion chamber, said standpipe chambers, and said cored passages to define said splash lubrication subsystem;

rotary motion of said upper and lower bevel gears circulating oil through said splash lubrication subsystem.

9. A coaxial transmission/center hub subassembly for a rotor assembly of an aerial vehicle having ducted counter-rotating rotors defining a rotational axis for the aerial vehicle, the aerial vehicle having a toroidal fuselage with a plurality of inwardly extending radial support struts and including an engine, the rotor assembly including upper and lower swashplate subassemblies, comprising:

a center hub support structure that includes a cylindrical body having at least three integral, outwardly extending radial support arms for rigidly attaching said coaxial transmission/center hub subassembly in combination with the plurality of inwardly extending radial support struts in fixed coaxial relation with the toroidal fuselage;

a multi-member transmission housing including

a middle holding secured in combination with said cylindrical body so that external surfaces of said middle housing abuttingly engage internal surfaces of said center hub support structure,

an upper standpipe housing secured in combination with said middle housing, and

a lower standpipe housing secured in combination with said middle housing, and

a single stage transmission subsystem including

an upper bevel gear including an upper rotor shaft rotatably mounted in combination in said upper standpipe housing,

a lower bevel gear including a lower rotor shaft rotatably mounted in combination in said lower standpipe housing, said upper and lower rotor shafts providing means for mounting the counter-rotating rotors in combination with said coaxial transmission/center hub subassembly, and

an input gear rotatably mounted in combination in said middle housing, said input gear being mechanically coupled in combination with said upper and lower bevel gears and the engine to couple torque therefrom to the counter-rotating rotors; and

wherein

said upper and lower standpipe housings are secured in combination with said middle housing in opposed relation along the rotational axis of the aerial vehicle; and

wherein

external surfaces of said upper and lower standpipe housings provide sliding surfaces for bi-directional linear movement of the upper and lower swashplate subassemblies, respectively.