Removable struts for vibration isolation device mounting system

Patent metadata

Field	Value
Publication number	US-10967962-B2
Application number	US-201816019826-A
Country	US
Kind code	B2
Filing date	Jun 27, 2018
Priority date	Jun 27, 2018
Publication date	Apr 6, 2021
Grant date	Apr 6, 2021

Abstract

A strut assembly for a vibration isolation device is disclosed, comprising a piston spindle; a first elastomeric member and a second elastomeric member bonded to the piston spindle and in contact with an upper housing and a lower housing, respectively; a first strut support and a second strut support attached to or integral with the upper housing and the lower housing, respectively; a first strut spindle and the second strut support configured to be placed in the first strut support and the second strut support, respectively; and one or more removable struts configured to be engaged to the first strut spindle and to the second strut spindle, wherein at least one of the first or second strut spindles is removable such that the one or more struts can be replaced without breaking a bonding of the first elastomeric member, the second elastomeric member, or both.

First claim

What is claimed is:

1. A strut assembly for a vibration isolation device comprising:
a piston spindle;
a first elastomeric member bonded to the piston spindle;
a second elastomeric member bonded to the piston spindle;
an upper housing in contact with the first elastomeric member;
a lower housing in contact with the second elastomeric member;
a first strut support attached to, or integral with, the upper housing;
a second strut support attached to, or integral with, the lower housing;
a first strut spindle configured to be placed in the first strut support;
a second strut spindle configured to be placed in the second strut support; and
one or more removable struts configured to be engaged at a first end to the first strut spindle and at a second end to the second strut spindle, without engagement of the first end to the first strut support or engagement of the second end to the second strut support, wherein at least one of the first or second strut spindles is removable such that the one or more struts can be replaced without breaking a bonding of the first elastomeric member, the second elastomeric member, or both.

2. The assembly of claim 1 , wherein the first elastomeric member or the second elastomeric member comprises rubber, plastics, composites, or layered materials.

3. The assembly of claim 1 , wherein the first elastomeric member is bonded to the piston spindle or the second elastomeric member is bonded to the piston spindle using an elastomer-to-substrate adhesive, and wherein the first elastomeric member or the second elastomeric member is molded and adhered to the piston spindle during a vulcanization process or bonded using a post-vulcanization process.

4. The assembly of claim 1 , wherein the one or more removable struts is configured to be threaded or slotted at a first end to the first strut spindle and configured to be threaded or slotted at a second end to the second strut spindle.

5. The assembly of claim 1 , wherein the one or more removable struts further comprise one or more surfaces on at least a portion of the strut to be engaged by a wrench.

6. A method of replacing a strut of a vibration isolation device, the method comprising:
providing the vibration isolation device comprising:
a piston spindle;
a first elastomeric member bonded to the piston spindle;
a second elastomeric member bonded to the piston spindle;
an upper housing in contact with the first elastomeric member;
a lower housing in contact with the second elastomeric member;
a first strut support attached to or integral with the upper housing;
a second strut support attached to or integral with the lower housing; and
one or more struts removably configured to be engaged at a first end to the first strut spindle and at a second end to the second strut spindle, without engagement of the first end to the first strut support or engagement of the second end to the second strut support;

placing a first strut spindle in the first strut support;
placing a second strut spindle in the second strut support;
engaging a first end of at least one of the one or more struts to the first strut spindle;
engaging a second end of the at least one of the one or more struts to the second strut spindle; and
removing the at least one of the one or more struts and installing a replacement strut without breaking a bonding of the first elastomeric member, the second elastomeric member, or both.

7. The method of claim 6 , wherein the first elastomeric member or the second elastomeric member comprises rubber, plastics, composites, or layered materials.

8. The method of claim 6 , wherein the first elastomeric member is bonded to the piston spindle or the second elastomeric member is bonded to the piston spindle using an elastomer-to-substrate adhesive, and wherein the first elastomeric member or the second elastomeric member is molded and adhered to the piston spindle during a vulcanization process or bonded using a post-vulcanization process.

9. The method of claim 6 , wherein the strut is threaded or slotted at a first end to the first strut spindle and threaded or slotted at a second end to the second strut spindle.

10. The method of claim 6 , wherein the one or more removable struts further comprise one or more surfaces on at least a portion of the strut to be engaged by a wrench.

11. A method of removing a strut from a vibration isolation device, the method comprising:
providing the vibration isolation device comprising:
a piston spindle;
a first elastomeric member bonded to the piston spindle;
a second elastomeric member bonded to the piston spindle;
an upper housing in contact with the first elastomeric member;
a lower housing in contact with the second elastomeric member;
a first strut support attached to or integral with the upper housing;
a second strut support attached to or integral with the lower housing;
a first strut spindle configured to be placed in the first strut support;
a second strut spindle configured to be placed in the second strut support; and
one or more removable struts engaged at a first end to the first strut spindle and engaged at a second end to the second strut spindle, without engagement of the first end to the first strut support or engagement of the second end to the second strut support;
applying a load to displace either the first elastomeric member or the second elastomeric member without breaking a bond of the first elastomeric member, the second elastomeric member, or both with the piston spindle;
disengaging the first end of the strut and the first strut spindle or disengaging the second end of the strut and the second strut spindle, without breaking a bonding of the first elastomeric member, the second elastomeric member, or both with the piston spindle; and
extracting the strut from the vibration isolation device without breaking the bond of the first elastomeric member, the second elastomeric member, or both with the piston spindle.

12. The method of claim 11 , wherein the first elastomeric member or the second elastomeric member comprises rubber, plastics, composites, or layered materials.

13. The method of claim 11 , wherein the first elastomeric member is bonded to the piston spindle or the second elastomeric member is bonded to the piston spindle using an elastomer-to-substrate adhesive, and wherein the first elastomeric member or the second elastomeric member is molded and adhered to the piston spindle during a vulcanization process or bonded using a post-vulcanization process.

14. The method of claim 11 , wherein the strut is threaded or slotted at a first end to the first strut spindle and threaded or slotted at a second end to the second strut spindle.

15. The method of claim 11 , wherein the one or more removable struts further comprise one or more surfaces on at least a portion of the strut to be engaged by a wrench.

16. A rotorcraft comprising:
a fuselage;
one or more engines; and
a vibration isolation device coupled to the fuselage, the vibration isolation device comprising:
a piston spindle;
a first elastomeric member bonded to the piston spindle;
a second elastomeric member bonded to the piston spindle;
an upper housing in contact with the first elastomeric member;
a lower housing in contact with the second elastomeric member;
a first strut support attached to or integral with the upper housing;
a second strut support attached to or integral with the lower housing;
a first strut spindle configured to be placed in the first strut support;
a second strut spindle configured to be placed in the second strut support; and

Assignees

• Bell Helicopter Textron Inc

Inventors

• Wiinikka Mark
• Hemmen Scott
• Green Nathan P
• Blake James

Classifications

• B64D27/402

  comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant · CPC title

• 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

• F16F13/085

  characterised by features of plastics springs; Attachment arrangements · CPC title