Vibration isolation device mounting system

Patent metadata

Field	Value
Publication number	US-10703465-B2
Application number	US-201815942030-A
Country	US
Kind code	B2
Filing date	Mar 30, 2018
Priority date	Mar 30, 2018
Publication date	Jul 7, 2020
Grant date	Jul 7, 2020

Abstract

A mounting system for a vibration isolation device comprises a support structure having an opening disposed therein, the opening having a concave recess; a thin elastomeric component attached to a surface of the concave recess; and a spherical elastomeric bearing disposed in the opening and attached to the thin elastomeric component, the spherical elastomeric bearing having a beveled upper portion, a middle portion and a beveled lower portion configured to engage the vibration isolation devices.

First claim

What is claimed is:

1. A mounting system for a vibration isolation device comprising:
a support structure having an opening disposed therein, the opening having a concave recess;
a thin elastomeric component attached to a surface of the concave recess; and
a spherical elastomeric bearing disposed in the opening and attached to the thin elastomeric component, the spherical elastomeric bearing having a beveled upper portion, a middle portion and a beveled lower portion configured to engage the vibration isolation device.

2. The mounting system of claim 1 , wherein:
the thin elastomeric component comprises a thin layer of rubber bonded to the surface of the concave recess; or
the support structure comprises a bipod mount.

3. The mounting system of claim 1 , wherein the thin elastomeric component is radially stiff but allows for angular misalignment.

4. The mounting system of claim 1 , further comprising a clevis coupled to the support structure for mounting an engine.

5. The mounting system of claim 1 , wherein:
the vibration isolation device comprises an upper housing and a lower housing, wherein the lower housing comprises a beveled upper portion and a lower portion;
the beveled upper portion of the spherical elastomeric bearing and the beveled upper portion of the lower housing of the vibration isolation device are configured to engage one another;
the middle portion of the spherical elastomeric bearing and the lower portion of the lower housing of the vibration isolation device are sized and configured to allow the lower portion of the lower housing of the vibration isolation device to be inserted into and slid through the spherical elastomeric bearing; and
an attachment device secures the lower portion of the lower housing of the vibration isolation device to the spherical elastomeric bearing.

6. The mounting system of claim 5 , wherein the attachment device comprises:
a cylindrical wedge disposed around the lower portion of the lower housing of the vibration isolation device and inserted between the beveled lower portion of the spherical elastomeric bearing and the lower portion of the lower housing of the vibration isolation device;
a cylindrical flange coupled to the lower portion of the lower housing of the vibration isolation device below the cylindrical wedge; and
a set of compression screws installed through holes in the cylindrical flange that engage the cylindrical wedge.

7. The mounting system of claim 6 , further comprising a gap between the cylindrical flange and the cylindrical wedge, wherein a distance of the gap indicates whether the compression screws have been properly tightened.

8. The mounting system of claim 6 , wherein the compression screws are safety wired.

9. The mounting system of claim 6 , further comprising one or more anti-rotation components attached to the cylindrical flange that engage a bottom of the vibration isolation device.

10. A vibration isolation system comprising:
a vibration isolation device comprising an upper housing and a lower housing, wherein the lower housing comprises a beveled upper portion and a lower portion;
a support structure having an opening disposed therein, the opening having a concave recess;
a thin elastomeric component attached to a surface of the concave recess;
a spherical elastomeric bearing disposed in the opening and attached to the thin elastomeric component, the spherical elastomeric bearing having a beveled upper portion, a middle portion and a beveled lower portion;
the beveled upper portion of the spherical elastomeric bearing and the beveled upper portion of the lower housing of the vibration isolation device are configured to engage one another;
the middle portion of the spherical elastomeric bearing and the lower portion of the lower housing of the vibration isolation device are sized and configured to allow the lower portion of the lower housing of the vibration isolation device to be inserted into and slid through the spherical elastomeric bearing; and
an attachment device secures the lower portion of the lower housing of the vibration isolation device to the spherical elastomeric bearing.

11. The vibration isolation system of claim 10 , wherein:
the thin elastomeric component comprises a thin layer of rubber bonded to the surface of the concave recess; or
the support structure comprises a bipod mount.

12. The vibration isolation system of claim 10 , wherein the thin elastomeric component is radially stiff but allows for angular misalignment.

13. The vibration isolation system of claim 10 , wherein the attachment device comprises:
a cylindrical wedge disposed around the lower portion of the lower housing of the vibration isolation device and inserted between the beveled lower portion of the spherical elastomeric bearing and the lower portion of the lower housing of the vibration isolation device;
a cylindrical flange coupled to the lower portion of the lower housing of the vibration isolation device below the cylindrical wedge; and
a set of compression screws installed through holes in the cylindrical flange that engage the cylindrical wedge.

14. The vibration isolation system of claim 13 , further comprising a gap between the cylindrical flange and the cylindrical wedge, wherein a distance of the gap indicates whether the compression screws have been properly tightened.

15. The vibration isolation system of claim 13 , wherein the compression screws are safety wired.

16. The vibration isolation system of claim 13 , further comprising one or more anti-rotation components attached to the cylindrical flange that engage a bottom of the vibration isolation device.

17. The vibration isolation system of claim 10 , wherein:
the support structure is mounted on a roof beam; and
the upper portion of the vibration isolation device is coupled to a pylon structure.

18. The vibration isolation system of claim 10 , further comprising a clevis coupled to the support structure for mounting an engine.

19. A vibration isolation system for a rotorcraft comprising:
a first roof beam and a second roof beam coupled to an airframe of the rotorcraft;
a forward cross member coupled to the first roof beam and the second roof beam;
an aft cross member coupled to the first roof beam and the second roof beam;
a first support structure coupled to the first roof beam in a forward position;
a second support structure coupled to the first roof beam in an aft position;
a third support structure coupled to the second roof beam in a forward position;
a fourth support structure coupled to the second roof beam in an aft position;
each support structure having an opening disposed therein, the opening having a concave recess, a thin elastomeric component attached to a surface of the concave recess, and a spherical elastomeric bearing disposed in the opening and attached to the thin elastomeric component, the spherical elastomeric bearing having a beveled upper portion, a middle portion and a beveled lower portion;
a vibration isolation device for each support structure comprising an upper housing and a lower housing, wherein the lower housing comprises a beveled upper portion and a lower portion;
wherein the beveled upper portion of the spherical elastomeric bearing and the beveled upper portion of the lower housing of the vibration isolation device are configured to engage one another;
wherein the middle portion of the spherical elastomeric bearing and the lower portion of the lower housing of the vibration isolation device are sized and configured t

Assignees

• Bell Helicopter Textron Inc

Inventors

• Smith Michael
• Griffin Maurice

Classifications

• B64C27/001 Primary

  Vibration damping devices · CPC title

• B64C2027/002

  mounted between the rotor drive and the fuselage · CPC title

• F16F13/24

  the central part of the unit being supported by one element and both extremities of the unit being supported by a single other element, i.e. double acting mounting · CPC title

• F16F1/393 Primary

  with spherical or conical sleeves · CPC title