Internally damped crossbar assembly having a slip plate damper

Patent metadata

Field	Value
Publication number	US-11524636-B2
Application number	US-201916721792-A
Country	US
Kind code	B2
Filing date	Dec 19, 2019
Priority date	Dec 19, 2019
Publication date	Dec 13, 2022
Grant date	Dec 13, 2022

Abstract

A crossbar system for facilitating isolation of a sensor assembly from external vibrations of a support structure. The crossbar system comprises first and second crossbar assemblies and a payload mount, Each of the first and second crossbar assemblies comprises a crossbar segment and a slip plate damper. Each crossbar segment comprises a payload mount interface at a first end of the crossbar assembly and a first support structure interface at a second end of the crossbar assembly. Each slip plate damper is disposed about the crossbar segment and is slidably coupled to the crossbar segment to constrain movement in two lateral degrees of freedom and to facilitate movement in a longitudinal degree of freedom, Each slip plate damper comprises a second support structure interface at the second end of the crossbar assembly. The payload mount is coupled to the payload mount interfaces of the first and second crossbar assemblies.

First claim

What is claimed is:

1. A crossbar system for isolating of a sensor assembly from external vibrations of a support structure, the crossbar system comprising:
first and second crossbar assemblies, each comprising:
a crossbar segment comprising a payload mount interface at a first end of the crossbar assembly and a first support structure interface at a second end of the crossbar assembly opposing the first end;
a slip plate damper disposed about the crossbar segment and slidably coupled to the crossbar segment to constrain movement in two lateral degrees of freedom and to facilitate movement in a longitudinal degree of freedom, the slip plate damper comprising a second support structure interface at the second end of the crossbar assembly; and

a payload mount coupled to the payload mount interfaces of the first and second crossbar assemblies, the payload mount operable to support a sensor assembly.

2. The crossbar system of claim 1 , wherein each crossbar assembly further comprises a flexible plate supported by the respective crossbar segment of each crossbar assembly, wherein the flexible plate defines the support structure interface of each crossbar segment.

3. The crossbar system of claim 1 , wherein each slip plate damper comprises a plurality of elongate plates extending from the second support structure interface, and wherein the crossbar segment comprises an elongate bar extending between the payload mount interface and the second support structure, wherein the plurality of elongate plates are arranged about the elongate bar.

4. The crossbar system of claim 3 , wherein each of the elongate plates of the plurality of elongate plates comprises a plurality of axially spaced holes, and wherein the elongate bar comprises a plurality of axially spaced slots corresponding to the plurality of axially spaced holes of an elongate plate.

5. The crossbar system of claim 4 , wherein each crossbar assembly further comprises a plurality of fasteners biasing each of the elongate plates towards the elongate bar.

6. The crossbar system of claim 3 , wherein the elongate bar has a length greater than a length of each of the plurality of elongate plates.

7. A crossbar assembly for facilitating isolation of a sensor assembly from external vibrations of a payload system mount on a vehicle, the crossbar assembly comprising:
a crossbar segment comprising a payload mount interface at a first end of the crossbar assembly and a first support structure interface at a second end of the crossbar assembly opposing the first end; and
a slip plate damper disposed about the crossbar segment and slidably coupled to the crossbar segment to constrain movement in two lateral degrees of freedom and to facilitate movement in a longitudinal degree of freedom, the slip plate damper comprising a second support structure interface at the second end of the crossbar assembly,
wherein the first support structure interface facilitates longitudinal movement of the crossbar segment relative to a support structure, and
wherein the second support structure interface dampens movement of the crossbar segment relative to the support structure.

8. The crossbar assembly of claim 7 , further comprising a flexible plate supported by the crossbar segment, the flexible plate defining the support structure interface.

9. The crossbar assembly of claim 7 , further comprising at least one fastener, wherein the crossbar segment further comprises a plurality of axially spaced slots and the slip plate damper further comprises a corresponding plurality of holes, and each fastener extends through a hole of the plurality of holes and a corresponding slot of the plurality of axially spaced slots.

10. The crossbar assembly of claim 7 , wherein the crossbar segment comprises an elongate bar and the slip plate damper comprises a plurality of elongate plates.

11. The crossbar assembly of claim 10 , wherein the elongate bar has a square cross section and the plurality of elongate plates comprises four elongate plates.

12. The crossbar assembly of claim 11 , wherein the second support structure interface comprises a lateral extension of an elongate plate of the plurality of elongate plates.

13. The crossbar assembly of claim 8 , wherein the crossbar segment comprises an axial protrusion configured to interface with a complementary aperture of the flexible plate.

14. The crossbar assembly of claim 13 , wherein the axial protrusion has a keyed profile and the aperture has a complementary keyed profile that facilitates rotational coupling of the crossbar segment and the flexible plate.

15. The crossbar assembly of claim 7 , wherein the slip plate damper is slidably coupled to the crossbar segment using at least one fastener operable to bias the slip plate damper towards the crossbar segment.

16. A payload system mount comprising:
a base structure;
a support structure rotatably coupled to the base structure;
a crossbar system supported by the support structure, the crossbar system comprising:
a payload mount;
first and second crossbar assemblies, each comprising:
a crossbar segment comprising a payload mount interface at a first end of the crossbar assembly and a first support structure interface at a second end of the crossbar assembly opposing the first end;
a slip plate damper disposed about the crossbar segment and slidably coupled to the crossbar segment to constrain movement in two lateral degrees of freedom and to facilitate movement in a longitudinal degree of freedom, the slip plate damper comprising a second support structure interface at the second end of the crossbar assembly; and

a sensor assembly coupled to the payload mount, the sensor assembly comprising at least one sensor.

17. The payload system mount of claim 16 , wherein each crossbar assembly further comprises a flexible plate supported by the crossbar segment, the flexible plate defining the support structure interface.

18. The payload system mount of claim 16 , wherein each first slip plate damper comprises a plurality of elongate plates extending from the second support structure interface and the crossbar segment comprises an elongate bar extending from the first payload mount interface, wherein the plurality of elongate plates are arranged about the elongate bar.

19. The payload system mount of claim 18 , wherein each of the elongate plates of the plurality of elongate plates comprise a plurality of axially spaced holes and the elongate bar comprises a plurality of axially spaced slots corresponding to the plurality of axially spaced holes of an elongate plate.

20. The payload system mount of claim 19 , wherein each crossbar segment further comprises a plurality of fasteners biasing each of the elongate plates towards the elongate bar.

Assignees

• Raytheon Co

Inventors

• Miller Kirk A
• Thomas Sean G

Classifications

• G01D11/10

  Elements for damping the movement of parts · CPC title

• F16F7/08 Primary

  with friction surfaces rectilinearly movable along each other (F16F7/01 takes precedence {; one of the members being a spring F16F13/02}) · CPC title

• G03B15/006

  Apparatus mounted on flying objects · CPC title

• F16F15/02

  Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems ({F16F15/005 takes precedence } ; layered products B32B; suppression of vibration in ships B63; {relieving load on bearings, using magnetic means F16C39/06}) · CPC title

• G03B17/561

  Support related camera accessories · CPC title