Aircraft engine case shock mount

Patent metadata

Field	Value
Publication number	US-10293950-B2
Application number	US-201514951674-A
Country	US
Kind code	B2
Filing date	Nov 25, 2015
Priority date	Sep 19, 2013
Publication date	May 21, 2019
Grant date	May 21, 2019

Abstract

The present disclosure relates to shock mounts for turbine engine components. A shock mount may be used to mount an accessory gearbox to an engine case. The shock mount may allow free thermal expansion, while providing damping and stiffness in response to vibrations. The shock mount may include a cylinder filled with fluid, and a piston telescopically moveable within the cylinder. The piston may be coupled to an orifice plate. The orifice plate may include orifices through which the fluid may flow in response to compression or extension of the shock mount. The interaction of the fluid and the orifice plate may resist rapid compression or extension of the shock mount while allowing relatively slow compression or extension of the shock mount.

First claim

The invention claimed is:

1. A mounting system:
an engine case;
a gearbox having circumferential ends with respect to a longitudinal axis of the engine case;
at least one rigid mount having a side hanger link coupled to one of the circumferential ends of the gearbox and the engine case; and
a shock mount coupled to the gearbox and the engine case, the shock mount comprising a cylinder configured to receive a fluid and a piston configured to telescopically move within the cylinder and change a length of the shock mount.

2. The mounting system of claim 1 , wherein the shock mount is configured to be coupled to the engine case and at least one of the gearbox and an accessory coupled to the gearbox.

3. The mounting system of claim 1 , wherein the shock mount is configured to operate at temperatures up to 1,200° F.

4. The mounting system of claim 1 , wherein the shock mount is configured to displace in response to thermal expansion of the engine case.

5. The mounting system of claim 1 , wherein the shock mount is configured to resist displacement in response to vibration.

6. The mounting system of claim 1 , wherein the shock mount further comprises an orifice plate which slidingly engages the cylinder.

7. The mounting system of claim 1 , wherein the cylinder houses the fluid and the fluid provides stiffness and damping capability to the shock mount.

8. The mounting system of claim 1 , wherein the shock mount contains no spring.

9. The mounting system of claim 1 , wherein the shock mount is coupled to the gearbox via a spherical bearing.

10. The mounting system of claim 1 , wherein a resistance to displacement of the shock mount is proportional to a rate of displacement of the shock mount.

Assignees

• United Technologies Corp

Inventors

• Ronski Mark
• Davis Todd A
• Boratgis Ernest

Classifications

• B64D27/26 Primary

  Operations & Transport · mapped topic

• F05D2260/96

  Preventing, counteracting or reducing vibration or noise · CPC title

• F16F2238/04

  Damper · CPC title

• F02C7/36

  Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title

• B64D2027/262

  Operations & Transport · mapped topic