Gunhard shock isolation system

• US 7,404,324 B2
• Filed: 08/19/2005
• Issued: 07/29/2008
• Est. Priority Date: 08/19/2005
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Braman, Todd L., Grossman, Owen, Hovland, Erik J.
• Primary Examiner(s): Kwok; Helen C.
• Application Number:
  US11/161,878
• Publication Number:
  US 20070074570A1
• Time in Patent Office: 1,075 Days
• Field of Search: 734/93, 734/31, 735/040.4, 735/041.2, 735/140.1, 735/141.6, 735/141.8, 188378-380
• US Class Current: 73/493
• CPC Class Codes: F16F 15/08 with rubber springs grommet- or bushing-type resilient mountings F16F1/3732, F16F1/38; with springs made of rubber and metal arrangement of internal-combustion or jet-propulsion units B60K5/12; mounting of propulsion plants on vessels B63H21/30; mounting of vehicle drivers' cabs B62D33/0604
• CPC Class Codes: G01C 21/166 Mechanical, construction or arrangement details of inertial navigation systems

Abstract

An inertial measurement unit (IMU) is provided that includes a container that defines a cavity. A sensor suit or ISA having a housing is provided in the container of the IMU. A dampening material is provided between the housing of the ISA and the container of the IMU. The dampening material may be applied by coating, spraying, or dipping, or may be separately molded and then inserted, if desired. A sway space may also be provided between the ISA and the IMU container.

Claims

1. An inertial measurement unit (IMU) comprising:

a container;

a sensor suite having a housing with at least one inertial sensor;

at least one isolator coupled between the container and the sensor suite, wherein the at least one isolator provides sway space between the sensor suite and the container; and

a dampening material applied to at least a portion of the housing.

2. The IMU of claim 1 wherein the housing has an outer surface and the dampening material is applied to at least a portion of the outer surface of the housing.

3. The IMU of claim 1 wherein at least one MEMS inertial sensor is included on a printed wiring assembly (PWA) of the sensor suite.

4. The IMU of claim 1 wherein the sensor suite has at least one retaining ring for retaining the PWA within the housing, wherein at least a portion of the retaining ring has the dampening material applied thereto.

5. The IMU of claim 1 further comprising one or more supports for supporting the PWA within the housing, wherein the dampening material is applied to at least a portion of at least one of the one or more supports.

6. The IMU of claim 1 wherein the dampening material is rubber.

7. The IMU of claim 6 wherein the rubber has a thickness of at least 0.002 inches.

8. An inertial measurement unit (IMU) comprising:

an IMU container having a cavity with cavity defining walls;

a sensor suite having a housing with outer walls, the housing having at least one inertial sensor therein and separated from the IMU container by sway space; and

a dampening material provided between the outer walls of the housing and the cavity defining walls of the IMU container, wherein the dampening material attenuates external forces experienced at the sensor suite as the sensor suite reduces the sway space and engages an adjacent portion of the IMU container during a high impact event.

9. The IMU of claim 8 wherein the dampening material is applied to at least a portion of the outer walls of the housing of the sensor suite.

10. The IMU of claim 8 wherein the dampening material is applied to at least a portion of the cavity defining walls of the IMU container.

11. The IMU of claim 8 wherein the dampening material is applied to at least a portion of the outer walls of the housing and to at least a portion of the cavity defining walls of the IMU container.

12. An inertial measurement unit (IMU) comprising:

a container having a cavity there between;

a sensor suite situated inside the cavity of the container; and

a sway space situated between at least a portion of the sensor suite and at least a portion of the container.

13. The IMU of claim 12 wherein the sway space is in the range of 0.001 inches to 0.3 inches.

14. The IMU of claim 12 wherein the sensor suite includes a housing with an outer surface, and wherein a dampening material is applied to at least a portion of the outer surface of the housing.

15. The IMU of claim 14 wherein the dampening material is rubber.

16. The IMU of claim 12 farther comprising:

one or more upper o-rings; and

one or more lower o-rings;

wherein the one or more upper o-rings and the one or more lower o-rings help provide the sway space between the housing of the sensor suite and the container of the IMU.

17. The IMU of claim 12 farther comprising one or more bolts to secure the o-rings between a housing of the sensor suite and the container of the IMU.

18. A method of dampening an inertial measurement unit (IMU) having a container that defines a cavity, the method comprising:

providing an inertial sensor assembly (ISA) in the cavity, the ISA having a housing with an outer surface;

providing a sway space between the outer surface of the housing of the ISA and the container of the IMU to separate the housing of the ISA from the container of the IMU; and

providing a dampening material between at least a portion of the outer surface of the housing of the ISA and the container of the IMU, wherein the dampening material attenuates external forces experienced at the sensor suite as the sensor suite substantially eliminates the sway space to engage an adjacent portion of the container of the IMU during a high impact event.

19. The method of claim 18 wherein the dampening material is provided by coating, spraying, or dipping the dampening material onto at least a portion of the outer surface of the housing of the ISA.

20. The method of claim 19 wherein the dampening material is applied with a thickness in the range of at least 0.002 inches.

21. The method of claim 18 wherein the dampening material is provided by molding the dampening material over at least a portion of the outer surface of the housing of the ISA.

22. The method of claim 21 wherein the dampening material is molded to a thickness of at least 0.010 inches.

23. The method of claim 18 wherein the dampening material is provided by assembling a dampening material element onto at least a portion of the outer surface of the housing of the ISA.