Tunable vibration isolation system with integrated A-frame architecture for low phase noise radio frequency synthesizers

Patent metadata

Field	Value
Publication number	US-9756751-B1
Application number	US-201615059141-A
Country	US
Kind code	B1
Filing date	Mar 2, 2016
Priority date	Mar 5, 2015
Publication date	Sep 5, 2017
Grant date	Sep 5, 2017

Abstract

A radio frequency (RF) frequency synthesizer includes a chassis housing that holds components of the RF frequency synthesizer. The chassis housing is installable into an instrument cabinet. A pair of mounting brackets are connected to opposing interior sides of the chassis housing and receive an A-Frame assembly which supports vibration sensitive RF circuitry and RF components. The A-Frame assembly is attached to the pair of mounting brackets in the chassis housing and provide a spatial separation between the kinematic inputs and the vibration sensitive RF circuitry and RF components. The A-Frame assembly includes a folded sheet, the folded sheet defining an angle between a first planar region and a second planar region, and may include a planar frame cross-member attached to the first planar region and the second planar region, the planar frame cross-member spanning the angle between the first and second planar regions.

First claim

What is claimed is:

1. A radio frequency (RF) synthesizer comprising: a chassis housing configured to hold components of the RF synthesizer, the chassis housing being installable into an instrument cabinet; at least one mounting bracket connected to at least one interior side of the chassis housing; an A-frame assembly configured to support at least one component of the RF synthesizer, the at least one component being susceptible to vibrational noise, the A-frame assembly being attached to the at least one mounting bracket, wherein the A-frame assembly comprises: at least two planar regions wherein at least one of the at least two planar regions support the at least one component of the RF synthesizer that is sensitive to vibrational noise, wherein the at least two planar regions include a first planar region and a second planar region which contact each other at a common edge to form an angle between the first planar region and the second planar region, and a third planar region defining a frame cross-member attached to the first planar region and the second planar region, the frame cross-member spanning the angle between the first planar region and the second planar region.

2. The RF synthesizer of claim 1 , further comprising at least one heat sink disposed between the at least one planar region and the at least one component of the RF synthesizer, the at least one heat sink being in thermal contact with at least one of the first planar region and the second planar region.

3. The RF synthesizer of claim 1 , wherein the first planar region and the second planar region are defined by a folded sheet of material.

4. The RF synthesizer of claim 3 , further comprising: a bezel defined at the fold in the folded sheet of material; and at least one handle attached to the bezel.

5. The RF synthesizer of claim 1 , further comprising: at least one electromagnetic interference (EMI) shield surrounding the at least one component of the RF synthesizer that is susceptible to vibrational noise.

6. The RF synthesizer of claim 1 , further comprising at least one of: a power supply, a processor board assembly, a 10 MHz circuit assembly, a clock distribution circuit and an alternating current (AC) power filter, installed in the chassis housing and spatially separated from the A-frame assembly.

7. The RF synthesizer of claim 1 , further comprising a passive isolation mount assembly comprising: a base plate configured to support the at least one component of the RF synthesizer susceptible to vibrational noise; and at least one passive isolation mount member between the base plate and one of the at least two planar regions supporting the at least one component of the RF synthesizer susceptible to vibrational noise.

8. The RF synthesizer of claim 7 , wherein the passive isolation mount assembly further comprises: at least one spacer corresponding to each of the at least one passive isolation mount member disposed between the corresponding at least one passive isolation mount member and the base plate.

9. The RF synthesizer of claim 7 , wherein the at least one passive isolation mount member comprises an elastomeric material.

10. The RF synthesizer of claim 1 , further comprising a passive isolation mount assembly comprising: a base plate configured to support the at least one component of the RF synthesizer susceptible to vibrational noise on the frame cross-member; and at least one passive isolation mount member between the base plate and the third planar region.

11. The RF synthesizer of claim 1 , wherein each of the at least two planar regions includes a first surface and a second surface opposite the first surface and the at least one component of the RF synthesizer that is susceptible to vibrational noise is supported on one of the first surface and the second surface.

12. An A-frame assembly for supporting vibration sensitive radio frequency (RF) components comprising: a first planar region; a second planar region, wherein at least one of the first planar region and the second planar region are configured to support at least one of the vibration sensitive RF components, and wherein the first planar region and the second planar region are in contact with one another along a common edge, the common edge defining an angle between the first planar region and the second planar region, and a planar frame cross-member attached to the first planar region and the second planar region, the planar frame cross-member spanning the angle between the first planar region and the second planar region.

13. The A-frame support assembly of claim 12 , wherein the planar frame cross member includes a first planar surface and a second planar surface opposite the first planar surface, wherein one of the first planar surface and the second planar surface supports at least one vibration sensitive RF component.

14. The A-frame support assembly of claim 12 , further comprising: a pair of flanges on opposing ends of the first planar region and the second planar region, the pair of flanges configured to receive at least one fastener for attaching the A-frame support assembly to a pair of mounting brackets of a chassis housing.

15. A method for tuning the spectral response of an assembly configured to support vibration sensitive radio frequency (RF) components, the assembly including a first planar region and a second planar region arranged with respect to one another to define an angle along a common edge of the first planar region and the second planar region, and a third planar region defining a frame cross member attached to the first planar region and the second planar region, the frame cross member spanning the angle defined between the first planar region and the second planar region, the method comprising the steps of: selecting a material for at least one of the first planar region, the second planar region and the third planar region, wherein the spectral response of the assembly is dependent at least in part on the selected material; and selecting a thickness of at least one of the first planar region, the second planar region and the third planar region, wherein the spectral response of the assembly is dependent at least in part on the selected thickness.

16. The method of claim 15 , further comprising the step of: selecting a distance between the vertex of the angle defined between the first planar region and the second planar region and a surface of the third planar region of the frame cross member, wherein the spectral response of the assembly is dependent at least in part on the selected distance.

17. The method of claim 15 , further comprising the step of: selecting the angle defined between the first planar region and the second planar region, wherein the spectral response of the assembly is dependent at least in part on the selected angle between the first planar region and the second planar region.

18. The method of claim 15 , further comprising the step of: selecting the number and position of at least one fastener configured to secure the assembly to a mounting bracket in a chassis housing, wherein the spectral response of the assembly is dependent at least in part on the number and position of the at least one fastener.

Assignees

• Lockheed Corp

Inventors

• Bowker Bryan James

Classifications

• H05K7/14 Primary

  Mounting supporting structure in casing or on frame or rack · CPC title

• H05K9/002

  with localised screening · CPC title

• H05K7/2039

  characterised by the heat transfer by conduction from the heat generating element to a dissipating body (arrangements for increasing/decreasing heat-transfer, e.g. fins details, F28F13/00) · CPC title

• H03L1/00 Primary

  Stabilisation of generator output against variations of physical values, e.g. power supply · CPC title

• F16F15/00 Primary

  Suppression of vibrations in systems ({damping of non-rotary systems using inertia effect F16F7/10; prevention or isolation of vibrations in machine tools B23Q11/0032; suppression of driveline vibrations in hybrid vehicle transmissions B60W30/20} ; vehicle seat suspension devices B60N2/50; {methods or devices for protecting against, or damping of, acoustic waves, e.g. sound G10K11/16}); Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion ({vibration absorbing or balancing means for aircraft propellers B64C11/008, for rotorcraft rotors B64C27/001} ; testing static and dynamic balance of machines or structures G01M1/00) · CPC title