Rotor apparatus

Patent metadata

Field	Value
Publication number	US-10358211-B2
Application number	US-201415108867-A
Country	US
Kind code	B2
Filing date	Jan 2, 2014
Priority date	Jan 2, 2014
Publication date	Jul 23, 2019
Grant date	Jul 23, 2019

Abstract

A rotor apparatus is provided and includes a first rotor shaft disposed to rotatably support a first rotor, a second rotor shaft disposed to rotatably support a second rotor and first and second bearing elements disposed to support the first rotor shaft within the second rotor shaft and to pre-load the first rotor shaft in one of tension and compression and the second rotor shaft in the other one of tension and compression.

First claim

What is claimed is:

1. A rotor apparatus, comprising:
a first rotor shaft disposed to rotatably support a first rotor;
a second rotor shaft disposed to rotatably support a second rotor; and
first and second bearing elements disposed to support the first rotor shaft within the second rotor shaft and to pre-load the first rotor shaft in one of tension and compression and the second rotor shaft in the other one of tension and compression;
wherein, when the first rotor shaft is in tension and the second rotor shaft is in compression, then a pre-loaded axial length of the first rotor shaft is longer than an unloaded axial length of the first rotor shaft, and a pre-loaded axial length of the second rotor shaft is shorter than an unloaded axial length of the second rotor shaft, and, when the first rotor shaft is in compression and the second rotor shaft is in tension, then a pre-loaded axial length of the first rotor shaft is shorter than an unloaded axial length of the first rotor shaft, and a pre-loaded axial length of the second rotor shaft is longer than an unloaded axial length of the second rotor shaft.

2. The rotor apparatus according to claim 1 , further comprising:
a first gear train operably coupled to the first rotor shaft to drive rotation of the first rotor shaft; and
a second gear train operably coupled to the second rotor shaft to drive rotation of the second rotor shaft,
wherein the first bearing elements are disposed along the first and second rotor shafts proximate to the second gear train.

3. A rotor apparatus, comprising:
a first rotor shaft disposed to rotatably support a first rotor;
a second rotor shaft disposed to rotatably support a second rotor;
first and second bearing elements disposed to support the first rotor shaft within the second rotor shaft and to pre-load the first rotor shaft in one of tension and compression and the second rotor shaft in the other one of tension and compression;
a transmission housing of a rotorcraft; and
third bearing elements disposed between the first rotor shaft and the transmission housing and between the second rotor shaft and the transmission housing to support the first and second rotor shafts against the transmission housing.

4. The rotor apparatus according to claim 1 , wherein the first and second bearing elements pre-load the first rotor shaft in tension against the second rotor shaft.

5. The rotor apparatus according to claim 1 , wherein the first and second bearing elements pre-load the first and second rotor shafts against one another.

6. The rotor apparatus according to claim 1 , wherein at least one of the first and second rotor shafts comprises lightweight and high strength metallic materials, alloys or composites.

7. The rotor apparatus according to claim 1 , further comprising an annulus defined between the first and second rotor shafts and between the first and second bearing elements, and a fluid disposed in the annulus to thermally match the first and second rotor shafts.

8. The rotor apparatus according to claim 1 wherein:
the first rotor shaft has a first longitudinal axis;
the second rotor shaft has a second longitudinal axis, and
the first and second rotor shafts are preloaded in a direction defined substantially in parallel with the first and second longitudinal axes of the first and second rotor shafts.

9. The rotor apparatus according to claim 8 , further comprising:
a first gear train operably coupled to the first rotor shaft to drive rotation of the first rotor shaft; and
a second gear train operably coupled to the second rotor shaft to drive rotation of the second rotor shaft,
wherein the first bearing elements are disposed along the first and second rotor shafts proximate to the second gear train and the second bearing elements are axially spaced from the first bearing elements and the second gear train.

10. The rotor apparatus according to claim 8 , further comprising:
a transmission housing of a rotorcraft; and
third bearing elements disposed between the first rotor shaft and the transmission housing and between the second rotor shaft and the transmission housing to support the first and second rotor shafts against the transmission housing.

11. The rotor apparatus according to claim 8 , wherein the first and second bearing elements pre-load the first rotor shaft in tension against the second rotor shaft.

12. The rotor apparatus according to claim 8 , wherein the first and second bearing elements pre-load the first and second rotor shafts against one another.

13. The rotor apparatus according to claim 8 , wherein at least one of the first and second rotor shafts comprises lightweight and high strength metallic materials, alloys or composites.

14. The rotor apparatus according to claim 8 , further comprising an annulus defined between the first and second rotor shafts, and a fluid disposed in the annulus to thermally match the first and second rotor shafts.

15. An aircraft, comprising:
an airframe;
an engine, which produces a rotary output; and
a transmission, which transmits the rotary output from the engine to the rotor apparatus of claim 1 .

16. The rotor apparatus of claim 1 , wherein the first rotor shaft rotates in a first direction;
and the second rotor shaft rotates in a second direction; and
the first and second bearing elements are disposed to rotatably support the first rotor shaft substantially concentrically within the second rotor shaft.

17. The rotor apparatus according to claim 1 , wherein the first and second bearing elements are disposed between the first and second rotor shafts and the first and second bearing elements are axially spaced with respect to each other.

18. A rotor apparatus, comprising:
a first rotor shaft disposed to rotatably support a first rotor;
a second rotor shaft disposed to rotatably support a second rotor; and
first and second bearing elements disposed to support the first rotor shaft within the second rotor shaft and to pre-load the first rotor shaft in one of tension and compression and the second rotor shaft in the other one of tension and compression;
wherein the first rotor shaft includes first bearing support elements disposed to impinge upon axially exterior sides of inner races of the first and second bearing elements, and the second rotor shaft includes second bearing support elements disposed to impinge upon axially interior sides of outer races of the first and second bearing elements.

19. The rotor apparatus according to claim 3 , wherein the third bearing elements include rollers disposed between the second rotor shaft and the transmission housing.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Gmirya Yuriy

Classifications

• B64C27/58

  Transmitting means, e.g. interrelated with initiating means or means acting on blades (means acting on blades B64C27/72) · CPC title

• B64C27/32

  Rotors · CPC title

• B64C2027/8281

  comprising horizontal tail planes · CPC title

• B64D35/06

  the propellers or rotors being counter-rotating · CPC title

• B64C2027/8236

  including pusher propellers · CPC title