Composite Swing-Arm EMI/RFI Strain Relief. Light Weight - Corrosion Free - Three-in-One Straight,...
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Transcript of Composite Swing-Arm EMI/RFI Strain Relief. Light Weight - Corrosion Free - Three-in-One Straight,...
Light Weight - Corrosion Free - Three-in-One
Straight, 45 and 90 Degrees
Integrated EMI/RFI Shield Sock
Inspection Window
Self-Locking Coupling Nut
Optional Composite Braid (319-065)
Brown or Black Material Electroless Nickel Shield Termination and Interface
No-Braid Version (627-122) Available Backshell Holding Tool
319-064 Composite Swing-Arm Strain-Relief
Non Corrosive
2000+ Hours Salt Spray Light Weight
40% Lighter than Aluminum 80% Lighter than SST
Vibration Dampening Superior Mechanical Properties Injection Mold Components for
Connectors & Accessories AIR4567, Type I, Grades A&B, Class 2 General Duty -65 to -175 Deg C
Composite Ultem 2300 (PEI)Reinforced with Glass
440-088 and 440-089 Series Shield Sock Parts Were Developed for the F-22 to Accelerate EMI Shield Termination
Assembly Times and Reduce the Weight of Interconnect Cabling
Origin of the Swing-Arm: The F-22 Composite Braid Sock Strain Relief
Electrical Resistance per AS85049, para 3.5.2 / 4.6.3 Vibration per AS85049 para 3.5.4 / 4.6.5.3 Half Sine Shock per AS85049 para 3.5.5 / 4.6.6.2 Transfer Impedance and Shielding Effectiveness Test Report
2004-1 Available From Factory Upon Request
Outstanding Mechanical, Environmental and EMI Performance
F-22 Shield Sock Performance Testing(Test Report No. 08-0204 Available from Factory Upon Request)
(1) Select Straight, 45 or 90 Degree Angle; (2) Insert Wire Bundle; (3) Mark Support Ring Location; (4) Apply Optional Tape Wrap;
(5) Slide Cable Shielding Over Support Ring and Trim to Fit.
EMI Shield Termination Procedure
(6) Evenly Space Shield Pigtails, if any, Around Support Ring;
(7) Slide Backshell Shield Sock Over Support Ring;
(8) Trim and Fold Braid in Place;
(9) Install Band; (10) Wrap Assembly
Area with High Temperature Tape
EMI Shield Termination Procedure
(11) Secure Loose Areas of Shield Sock with Ties or Lacing;
(12) Tighten Backshell to Connector with 600-091 Series Backshell Holding Tool and Torque to 40 to 120 Lbs. (See Catalog Torque Chart).
(13) Tighten Strain-Relief Saddle Bars to Correct Torque: 5.2 lbs Max for #4 Fastener and 10 lbs Max for #6 Fastener.
(14) Use Only Genuine Glenair Tools and Replacement Parts
EMI Shield Termination Procedure
Operates in a similar manner to the F-22 Shield Sock, but offers three-in-one straight, 45° and 90° design for SKU reduction
The Swing-Arm Advantage
The Swing-Arm is perfectly suited for new connector accessory design-ins for the next generation of manned and unmanned
aircraft
Approved for use at: Lockheed Martin Boeing Bell Helicopter Northrop Grumman Bombardier Embraer
Proven Performance Applications
Please see the April 2007 Issue of QwikConnect
Complete Product Overview EMI Shield Assembly Instructions Application References How to Order and Part Number
Development Same-Day Inventory Listing Qualification Test Report Available in Hard Copy or at
www.glenair.com
For More Information