IP Library Granted Patent US 8,393,601
Granted Patent B2
US 8,393,601 · App. 12/286,972 · Granted Mar 12, 2013

Vibration isolation fastener insert

Inventor: Manuel Loret de Mola (Jupiter, FL)
Assignees: Applied Concepts Aircraft Solutions, Inc.; The Young Engineers, Inc.
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,393,601
App. No.
12/286,972
Granted
Mar 12, 2013
Kind
B2
Abstract

A vibration isolation fastener insert comprising: a rigid cylindrical hub having an externally extending flange and a through longitudinal opening to receive a fastener. An elastomeric bushing around the hub has a slot therein receiving the external flange. An upper housing is disposed around the side of the bushing and has a flange over the top of the bushing. A lower housing is disposed around the external side of the upper housing and has a flange extending below a lower surface of the bushing.

Claims (36)

1. A vibration isolation fastener insert adapted to be snugly received in a hole in a panel, comprising:

a rigid generally cylindrical hub having upper and lower longitudinal ends and a radially outward extending annular flange having an outer side surface and opposing upper and lower surfaces, and a central longitudinal through opening adapted to receive a fastener element;

an annular elastomeric bushing snugly carried or formed around said hub and having an inner annular slot therein receiving and completely enclosing the outer side surface and upper and lower surfaces of said radially extending flange;

a first housing having a cylindrical sidewall adapted to axially extend through the hole in said panel, and an annular upper flange extending radially outward to abut an upper surface of said panel;

a second housing having a cylindrical sidewall adapted to axially extend through the hole in said panel, and an annular lower flange extending radially outward to engage an inner surface of said hole;

said upper and lower flanges each having a central through opening generally aligned with said longitudinal opening;

the cylindrical sidewall of said first housing being disposed around and receiving a side surface of said bushing, and said upper flange extending radially inwards and abutting said upper surface of said bushing; and

the cylindrical sidewall of said second housing disposed around and receiving an external surface of the cylindrical sidewall of said first housing, and said lower flange extending radially inward and abutting said lower surface of said bushing.

2. A vibration isolation fastener insert adapted to be snugly received in a hole in a panel, comprising:

a rigid generally cylindrical hub having upper and lower longitudinal ends and a radially outward extending annular flange having an outer side surface and opposing upper and lower surfaces, and a central longitudinal through opening adapted to receive a fastener element;

an annular elastomeric bushing snugly carried or formed around said hub and having an inner annular slot therein receiving and completely enclosing the outer side surface and upper and lower surfaces of said radially extending flange;

a first housing having a cylindrical sidewall adapted to axially extend through the hole in said panel, and an annular upper flange extending radially outward to abut an upper surface of said panel;

a second housing having a cylindrical sidewall adapted to axially extend through the hole in said panel, and an annular lower flange extending radially outward to engage an inner surface of said hole;

said upper and lower flanges each having a central through opening generally aligned with said longitudinal opening;

the cylindrical sidewall of said first housing being disposed around and receiving a side surface of said bushing, and said upper flange extending radially inwards and abutting said upper surface of said bushing, and having potting holes therein disposed to allow potting material to be introduced therethrough and around an outside of the insert; and

the cylindrical sidewall of said second housing disposed around and receiving an external surface of the cylindrical sidewall of said first housing, and said lower flange extending radially inwards and abutting said lower surface of said bushing.

3. A panel assembly having a hole, and received in said hole a vibration isolation fastener insert comprising:

a rigid generally cylindrical hub having upper and lower longitudinal ends and a radially outward extending annular flange having an outer side surface and opposing upper and lower surfaces, and a central longitudinal through opening adapted to receive a fastener element;

an annular elastomeric bushing snugly carried or formed around said hub and having an inner annular slot therein receiving and completely enclosing the outer side surface and upper and lower surfaces of said radially extending flange;

a first housing having a cylindrical sidewall axially extending through the hole in said panel, and an annular upper flange extending radially outward and abutting an upper surface of said panel;

a second housing having a cylindrical sidewall axially extending through the hole in said panel, and an annular lower flange extending radially outward and engaging an inner surface of said hole;

said upper and lower flanges each having a central through opening generally aligned with said longitudinal opening;

the cylindrical sidewall of said first housing being disposed around and receiving a side surface of said bushing, and said upper flange extending radially inwards and abutting said upper surface of said bushing; and

the cylindrical sidewall of said second housing disposed around and receiving an external surface of the cylindrical sidewall of said first housing, and said lower flange extending radially inwards and abutting said lower surface of said bushing.

4. The panel assembly of claim 3 wherein the panel is honeycomb.

5. The panel assembly of claim 3 wherein said vibration isolation fastener insert is swaged into said panel.

6. A panel assembly having a hole, and received in said hole a vibration isolation fastener insert comprising:

a rigid generally cylindrical hub having upper and lower longitudinal ends and a radially outward extending annular flange having an outer side surface and opposing upper and lower surfaces, and a central longitudinal through opening adapted to receive a fastener element;

an annular elastomeric bushing snugly carried or formed around said hub and having an inner annular slot therein receiving and completely enclosing the outer side surface and upper and lower surfaces of said radially extending flange;

a first housing having a cylindrical sidewall axially extending through the hole in said panel, and an annular upper flange extending radially outward and abutting an upper surface of said panel;

a second housing having a cylindrical sidewall axially extending through the hole in said panel, and an annular lower flange extending radially outward and engaging an inner surface of said hole;

said upper and lower flanges each having a central through opening generally aligned with said longitudinal opening;

the cylindrical sidewall of said first housing being disposed around and receiving a side surface of said bushing, and said upper flange extending radially inwards and abutting said upper surface of said bushing, and having potting holes therein disposed to allow potting material to be introduced therethrough and around an outside of the insert; and

the cylindrical sidewall of said second housing disposed around and receiving an external surface of the cylindrical sidewall of said first housing, and said lower flange extending radially inwards and abutting said lower surface of said bushing.

7. The panel assembly of claim 6 wherein the panel is honeycomb.

8. The panel assembly of claim 6 wherein said vibration isolation fastener insert is potted into said panel.

Assignments (5)
RELEASE OF SECURITY INTEREST IN PATENT RIGHTS RECORDED AT REEL/FRAME: 056538/0813 Recorded Jan 13, 2026
From: ROYAL BANK OF CANADA
To: THE YOUNG ENGINEERS, INC.
Reel/Frame 074132/0866 →
PATENT SECURITY AGREEMENT Recorded Jan 13, 2026
From: THE YOUNG ENGINEERS, INC.; NOVARIA HOLDINGS, LLC
To: HPS INVESTMENT PARTNERS, LLC, AS COLLATERAL AGENT
Reel/Frame 074330/0606 →
SECURITY INTEREST Recorded Jun 14, 2021
From: THE YOUNG ENGINEERS, INC.
To: ROYAL BANK OF CANADA
Reel/Frame 056538/0813 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 7, 2014
From: APPLIED CONCEPTS AIRCRAFT SOLUTIONS, INC.
To: LORET DE MOLA, MANUEL
Reel/Frame 032841/0911 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 4, 2008
From: DE MOLA, MANUEL LORET
To: APPLIED CONCEPTS AIRCRAFT SOLUTIONS, INC.; YOUNG ENGINEERS, THE, INC.
Reel/Frame 021694/0377 →
Continuity (1)
Related Publication 20100086377A1 · Apr 8, 2010