IP Library Granted Patent US 10,167,989
Granted Patent B2
US 10,167,989 · App. 15/064,392 · Granted Jan 1, 2019

Multidirectionally deflectable mounting apparatus and method

Inventor: Bruno J. Desrochers (Ramona, CA)
Assignee: NORTHROP GRUMMAN SYSTEMS CORPORATION
F16M5/00B60K8/00F01D25/28
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Quick Facts
Patent No.
US 10,167,989
App. No.
15/064,392
Granted
Jan 1, 2019
Kind
B2
Abstract

A multidirectionally deflectable engine mounting apparatus includes a laterally oriented base surface and a longitudinally extending elongate shaft having a laterally oriented shaft flange. The shaft flange is longitudinally adjacent to the base surface. A resilient washer is located directly longitudinally between the base surface and the shaft flange. A top plate includes a plate aperture. The shaft extends longitudinally through the plate aperture. The top plate is attached directly to the base surface with the resilient washer and the shaft flange located longitudinally between the base surface and at least a portion of the top plate.

Claims (14)

1. A mounting system, comprising:

a first multidirectionally deflectable engine mounting apparatus; and

a second multidirectionally deflectable engine mounting apparatus;

wherein each of the first and second multidirectionally deflectable engine mounting apparatuses includes

a base having a base surface and an undersurface, the base surface substantially located in a lateral plane,

an elongate shaft having a proximal shaft end and a distal shaft end, the proximal and distal shaft ends being longitudinally spaced from one another, the shaft having a laterally oriented shaft flange encircling the proximal shaft end, the shaft flange having a proximal shaft flange surface and a distal shaft flange surface, the proximal and distal shaft flange surfaces each being laterally extending,

a resilient washer located directly between the base surface and the proximal shaft flange surface, and

a contoured top plate including a distally raised center portion and a laterally oriented outer plate rim concentric to the center portion, the center portion having a plate aperture surrounding the shaft, the plate rim being connected directly to the base surface, and the shaft flange and the resilient washer both being located entirely proximal to the center portion and lateral to the plate rim, such that the shaft flange and the resilient washer are covered by the top plate and attached to the base surface thereby,

wherein the resilient washer is configured to be compressed under deflection pressure applied laterally to the shaft, compression of the resilient washer being configured to cause a biasing force equal and opposite to the deflection pressure to re-center the shaft when the deflection pressure is removed;

wherein the second multidirectionally deflectable engine mounting apparatus is oriented in mirrored longitudinal opposition to the first multidirectionally deflectable engine mounting apparatus such that the undersurface of the base of the first multidirectionally deflectable engine mounting apparatus is in direct contact with the undersurface of the base of the second multidirectionally deflectable engine mounting apparatus, and the proximal shaft ends of the first and second multidirectionally deflectable engine mounting apparatuses are located adjacent one another, with both the proximal shaft ends of the first and second multidirectionally deflectable engine mounting apparatuses being concurrently longitudinally interposed between the distal shaft ends of the first and second multidirectionally deflectable engine mounting apparatuses.

2. The mounting system of claim 1 , wherein the resilient washer of the first multidirectionally deflectable engine mounting apparatus is an elastomeric washer.

3. The mounting system of claim 1 , wherein the shaft of the first multidirectionally deflectable engine mounting apparatus defines a longitudinally oriented shaft lumen placing the proximal and distal shaft ends of the first multidirectionally deflectable engine mounting apparatus into fluid communication.

4. The mounting system of claim 3 , wherein the shaft lumen of the first multidirectionally deflectable engine mounting apparatus is substantially coaxial with an aperture in the base of the first multidirectionally deflectable engine mounting apparatus.

5. The mounting system of claim 1 , wherein the shaft flange of the first multidirectionally deflectable engine mounting apparatus is tapered in a lateral direction, having a maximum longitudinal thickness at the shaft of the first multidirectionally deflectable engine mounting apparatus and a minimum longitudinal thickness at a farthest lateral extent from the shaft of the first multidirectionally deflectable engine mounting apparatus.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 9, 2016
From: DESROCHERS, BRUNO J.
To: NORTHROP GRUMMAN SYSTEMS CORPORATION
Reel/Frame 037933/0220 →
Continuity (1)
Related Publication 20170261149A1 · Sep 14, 2017