Rotor

Patent metadata

Field	Value
Publication number	US-12479753-B2
Application number	US-202017641067-A
Country	US
Kind code	B2
Filing date	Sep 9, 2020
Priority date	Sep 10, 2019
Publication date	Nov 25, 2025
Grant date	Nov 25, 2025

Abstract

A rotor for a fiberising apparatus includes a rotor housing; a first and second bearing assembly, wherein each bearing assembly has at least two ball bearings, each seated in a respective bearing seat; a substantially horizontal shaft rotatably mounted between the first bearing assembly and the second bearing assembly; and a plurality of resilient dampers arranged in an annular ring, wherein each resilient damper is releasably connected at a first end to the bearing seat and is releasably connected at a second end to the inner wall of the rotor housing.

First claim

The invention claimed is:

1 . A rotor for a fiberising apparatus comprising:
a rotor housing; a first bearing assembly and a second bearing assembly, wherein each bearing assembly comprises at least two ball bearings, each seated in a respective bearing seat; a substantially horizontal shaft rotatably mounted between the first bearing assembly and the second bearing assembly; a plurality of resilient dampers arranged in an annular ring, wherein each resilient damper is connected and held at a first end to the bearing seat and connected and held at a second end to an inner wall of the rotor housing; and wherein each resilient damper comprises a threaded screw for releasable connection to the bearing seat and each resilient damper comprises a threaded aperture for releasable connection with a screw through the rotor housing.

2 . The rotor according to claim 1 , wherein each resilient damper is a frustum, or wherein each resilient damper is frustoconical.

3 . The rotor according to claim 1 , wherein the plurality of resilient dampers comprise frustoconical resilient dampers.

4 . The rotor according to claim 3 , wherein each resilient damper has a greater diameter at the damper face adjacent to the inner wall of the rotor housing and a lesser diameter at the damper face adjacent to the bearing seat.

5 . The rotor according to claim 1 , wherein each resilient damper is any of a rubber damper, a silicone damper, a neoprene rubber damper.

6 . The rotor according to claim 1 , wherein the plurality of resilient dampers is adapted for a working rotation speed of the rotor of between about 4000 RPM and 13000 RPM.

7 . The rotor according to claim 1 , wherein a base wall thickness of the rotor housing is greater than an upper wall thickness of the rotor housing.

8 . The rotor according to claim 1 , wherein the rotor housing has a base wall thickness about 5 mm greater than an upper wall thickness of the rotor housing.

9 . The rotor according to claim 1 , wherein the internal profile of the rotor housing is asymmetric.

10 . The rotor according to claim 1 , wherein each bearing seat is substantially cylindrical, the rotor housing is substantially cylindrical and the central axis of the bearing seat is offset from the central axis of the rotor housing.

11 . The rotor according to claim 1 , wherein each resilient damper has a Shore A hardness of about 55.

12 . The rotor according to claim 1 wherein a stiffness of the plurality of resilient dampers arranged in an annular ring is between about 5·10 5 to about 10 6 N/m.

13 . The rotor according to claim 1 , wherein the plurality of resilient dampers comprises between about 10 and about 24 frustoconical resilient dampers arranged annularly.

14 . The rotor according to claim 1 , wherein the plurality of resilient dampers are equidistant from each other around a substantially annular bearing assembly.

15 . The rotor according to claim 1 , wherein at least one of the at least two ball bearings of the first and second bearing assembly is a hybrid angular ball bearing.

16 . The rotor according to claim 1 , wherein the inner diameter of at least one of the at least two ball bearings of the first and second bearing assembly is between about 60 mm and about 75 mm.

17 . The rotor according to claim 1 , wherein at least one of the at least two ball bearings of the first and second bearing assembly is made of a ceramic material.

18 . The rotor according to claim 1 , wherein at least one of the at least two ball bearings of the first and second bearing assembly is a hybrid angular ball bearing and a distance between the at least two ball bearings is about 20 mm.

19 . The rotor according to claim 1 , wherein the clearance between each bearing seat and an inner surface of the inner wall of the rotor housing is about 14 mm.

20 . The rotor according to claim 1 , wherein the at least two ball bearings of the first and second bearing assembly are hybrid angular ball bearings and wherein the at least two hybrid angular ball bearings are spaced apart by an inner axial spacer ring and an outer axial spacer ring; wherein a width of the outer axial spacer ring is less than a width of the inner axial spacer ring.

21 . The rotor according to claim 1 , wherein the at least two ball bearings of the first and second bearing assembly are hybrid angular ball bearings, wherein the at least two hybrid angular ball bearings are spaced apart by an inner axial spacer ring and an outer axial spacer ring and wherein the width of the outer axial spacer ring is between about 16 μm and 61 μm less than the width of the inner axial spacer ring.

22 . The rotor according to claim 1 , wherein a relationship between the substantially horizontal shaft diameter (D shaft ) and the substantially horizontal shaft length (L shaft ) is defined as: D shaft (L shaft )≥0.12*L shaft −32 mm for a range of substantially horizontal shaft lengths between about 101 mm and 1325 mm and for a range of substantially horizontal shaft diameters greater than or equal to 20 mm and for a stiffness of the plurality of resilient dampers arranged in an annular ring of less than or equal to 3*10 6 N/m.

23 . The rotor according to claim 1 , wherein the outer cross-sectional diameter of the substantially horizontal shaft is about 100 mm; the substantially horizontal shaft has a bearing seat diameter of about 70 mm; the total length of the substantially horizontal shaft is about 955 mm; and wherein a length of the substantially horizontal shaft between a centre-point of the first bearing assembly and a centre-point of the second bearing assembly is about 590 mm.

24 . The rotor according to claim 1 , wherein the weight of each bearing seat is less than or equal to 3 kg.

25 . A fiberising apparatus comprising a set of at least three rotors according to claim 1 , wherein each rotor is mounted for rotation about a different substantially horizontal axis and arranged such that, when the rotors are rotating, melt poured on to the periphery of the first rotor in the set is thrown successively onto the periphery of each of the subsequent rotors and fibres are thrown off from the rotors.

26 . The rotor according to claim 1 , wherein each of the resilient dampers comprises a central axis which extends radially of the shaft.

27 . The rotor according to claim 1 , wherein each resilient damper is releasably fixed at a first end to the bearing seat and releasably fixed at a second end to the inner wall of the rotor housing.

28 . A rotor for a fiberising apparatus comprising:
a rotor housing; a first bearing assembly and a second bearing assembly, wherein each bearing assembly comprises at least two ball bearings, each seated in a respective bearing seat; a substantially horizontal shaft rotatably mounted between the first bearing assembly and the second bearing assembly; and a plurality of resilient dampers arranged in an annular ring, wherein each resilient damper is connected at a first end to the bearing seat and connected at a second end to an inner wall of the rotor housing; and wherein each resilient damper comprises a threaded screw for releasable connection to the bearing seat.

29 . A rotor for a fiberising apparatus comprising:
a rotor housing; a first bearing assembly and a second bearing assembly, wherein each bearing assemb

Assignees

• Rockwool As

Inventors

• Sørensen Jens Jørren
• Rosenberg Gorm

Classifications

• F16F15/12

  using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon ({F16F15/14} , F16F15/16 take precedence) · CPC title

• C03B37/055 Primary

  by projecting onto and spinning off the outer surface of the rotating body · CPC title

• F16F15/08 Primary

  with rubber springs {(grommet- or bushing-type resilient mountings F16F1/3732, F16F1/38); with springs made of rubber and metal (arrangement of internal-combustion or jet-propulsion units B60K5/12; mounting of propulsion plants on vessels B63H21/30; mounting of vehicle drivers' cabs B62D33/0604)} · CPC title