Rotor dome, a rotor, and a rotorcraft

Patent metadata

Field	Value
Publication number	US-10167077-B2
Application number	US-201514939275-A
Country	US
Kind code	B2
Filing date	Nov 12, 2015
Priority date	Nov 14, 2014
Publication date	Jan 1, 2019
Grant date	Jan 1, 2019

Abstract

A dome for a rotor comprising a cap extending radially from an axis of rotation in elevation towards a periphery and in azimuth over 360 degrees, the cap extending in thickness from a bottom face towards a top face above the bottom face. The dome includes at least one slot extending between the periphery and the axis of rotation in elevation, each slot passing right through a thickness of the cap by extending in elevation from the bottom face to the top face.

First claim

What is claimed is:

1. A dome for a rotor of a rotorcraft, the dome comprising a cap extending radially and in elevation from a center of the cap on an axis of rotation towards a periphery of the cap and in azimuth over 360 degrees, the cap extending in thickness from a bottom face for facing a hub of the rotor towards a top face above the bottom face, the dome including notches enabling blades to pass therethrough in order to allow the blades to flap;
wherein the dome includes a plurality of slots between the periphery and the axis of rotation in elevation, each slot being distinct from the notches, each slot passing through a thickness of the cap by extending in elevation from the bottom face to the top face, the dome including in azimuth along at least one circular path about the axis of rotation a succession of solid surfaces defined by parts of the top face and two adjacent slots, respectively, of the plurality of slots, the solid surfaces facing an incident air stream so that the incident air stream impacts in succession against a solid surface of the solid surfaces and a slot of the plurality of slots during rotation of the dome about the axis of rotation in elevation, wherein the solid surfaces comprise a plurality of arms extending spanwise from the axis of rotation in elevation towards the periphery, each arm extending in azimuth between two adjacent slots, respectively, of the plurality of slots, each arm presenting an airfoil profile extending in azimuth between a leading edge in the vicinity of one slot of the two adjacent slots, respectively, and a trailing edge in the vicinity of the other slot of the two adjacent slots, respectively.

2. The dome according to claim 1 , wherein the number of the notches is different from the number of the plurality of slots.

3. The dome according to claim 2 , wherein the number of the notches and the number of the plurality of slots are mutually prime.

4. The dome according to claim 1 , wherein at least one arm of the plurality of arms presents a plurality of sections and a twist relationship determining a twist angle for each section of the plurality of sections of the at least one arm each section of the plurality of sections representing a cross-section of the at least one arm in a plane extending in elevation from a trailing edge to a leading edge of the at least one arm and perpendicular to a geometrical stacking line of the arm.

5. The dome according to claim 1 , wherein at least one arm of the plurality of arms presents a width in azimuth that increases from the center of the cap to the periphery of the cap.

6. The dome according to claim 1 , wherein each slot of the plurality of slots extends in a plane including the axis of rotation.

7. The dome according to claim 1 , wherein each slot of the plurality of slots has portions extending in a plane not containing the axis of rotation.

8. The dome according to claim 1 , wherein the dome is for rotation in a particular direction of rotation, each slot of the plurality of slots presenting a convex shape that is convex pointing in the particular direction of rotation of the dome.

9. The dome according to claim 1 , wherein each slot of the plurality of slots presents a width that varies in azimuth.

10. The dome according to claim 1 , wherein each slot of the plurality of slots extends in an annulus of the dome lying between the periphery and the axis of rotation in elevation, the annulus not reaching the periphery and/or the axis of rotation.

11. The dome according to claim 1 , wherein each slot of the plurality of slots opens to the periphery.

12. A rotorcraft rotor having a hub carrying a plurality of blades, wherein the rotor includes a dome according to claim 1 , the blades being unable to penetrate into the plurality of slots.

13. A rotorcraft, wherein the rotorcraft includes at least one rotor according to claim 12 .

14. The dome according to claim 1 , wherein the number of the notches is different from the number of the plurality of slots.

15. A dome for a rotor of a rotorcraft, the dome comprising a cap extending radially and in elevation from a center of the cap on an axis of rotation towards a periphery of the cap and in azimuth over 360 degrees, the cap extending in thickness from a bottom face for facing a hub of the rotor towards a top face above the bottom face, the dome including notches enabling blades to pass therethrough in order to allow the blades to flap;
wherein the dome includes a plurality of slots between the periphery and the axis of rotation in elevation, each slot being distinct from the notches, each slot passing through a thickness of the cap by extending in elevation from the bottom face to the top face, the dome including in azimuth along at least one circular path about the axis of rotation a succession of solid surfaces defined by parts of the top face and two adjacent slots, respectively, of the plurality of slots, the solid surfaces facing an incident air stream so that the incident air stream impacts in succession against a solid surface of the solid surfaces and a slot of the plurality of slots during rotation of the dome about the axis of rotation in elevation, wherein the dome is for rotation in a particular direction of rotation, and each slot of the plurality of slots presents a convex shape that is convex pointing in the particular direction of rotation of the dome.

16. The dome according to claim 15 , wherein the number of the notches is different from the number of the plurality of slots.

17. The dome according to claim 16 , wherein the number of the notches and the number of the plurality of slots are mutually prime.

18. A dome for a rotor of a rotorcraft, the dome comprising a cap extending radially and in elevation from a center of the cap on an axis of rotation towards a periphery of the cap and in azimuth over 360 degrees, the cap extending in thickness from a bottom face for facing a hub of the rotor towards a top face above the bottom face, the dome including notches enabling blades to pass therethrough in order to allow the blades to flap;
wherein the dome includes a plurality of slots between the periphery and the axis of rotation in elevation, each slot being distinct from the notches, each slot passing through a thickness of the cap by extending in elevation from the bottom face to the top face, the dome including in azimuth along at least one circular path about the axis of rotation a succession of solid surfaces defined by parts of the top face and two adjacent slots, respectively, of the plurality of slots, the solid surfaces facing an incident air stream so that the incident air stream impacts in succession against a solid surface of the solid surfaces and a slot of the plurality of slots during rotation of the dome about the axis of rotation in elevation, wherein each slot of the plurality of slots presents a width that varies in azimuth.

19. The dome according to claim 18 , wherein the number of notches is different from the number of the plurality of slots.

20. A dome for a rotor of a rotorcraft, the dome comprising a cap extending radially and in elevation from a center of the cap on an axis of rotation towards a periphery of the cap and in azimuth over 360 degrees, the cap extending in thickness from a bottom face for facing a hub of the rotor towards a top face above the bottom face, the dome including notches enabling blades to pass therethrough in order to allow the blades to flap;
wherein the dome includes a plurality of slots between the periphery and the axis of rotatio

Assignees

• Airbus Helicopters

Inventors

• Alfano David
• Desvigne Damien
• Fukari Raphael

Classifications

• B64C11/14

  Spinners · CPC title

• B64C2027/003

  mounted on rotor hub, e.g. a rotary force generator · CPC title

• B64C7/00 Primary

  Structures or fairings not otherwise provided for · CPC title

• B64C27/32

  Rotors · CPC title

• B64C27/001 Primary

  Vibration damping devices · CPC title