180 likes | 367 Views
6/22/2004. 2. NG Con Background. Objective: Develop a heavy duty multi-fiber connector Inter- operability and Inter-changeability Use LC technologyLow cost objective $5 target terminusUtilize best engineering practices / features (e.g. 38999, 28876, etc.) to give lowest total ownership cost (T
E N D
1. 6/22/2004 1 Next Generation Heavy Duty Fiber Optic Connector (NG Con) Gair Brown
NSWCDD Code B35
Browngd@nswc.navy.mil
Michael J. Hackert
NAVAIR 4.5.3.3
Michael.Hackert@NAVY.mil
301-342-9124
2. 6/22/2004 2 NG Con Background Objective: Develop a heavy duty multi-fiber connector
Inter- operability and Inter-changeability
Use LC technology
Low cost objective $5 target terminus
Utilize best engineering practices / features (e.g. 38999, 28876, etc.) to give lowest total ownership cost (TOC)
NAVSEA initiated replacement for shipboard applications
Extend to aerospace application both military and commercial
Navy development, specification and qualification support
3. 6/22/2004 3 Participants Wide industry participation including users and suppliers
4. 6/22/2004 4 Progress to Date Stereotypical standards development
Glacial standard follows development
NG Con modern development pace
Supersonic Fast track to develop industry consensus
Quarterly meetings
6/25-26/04 next meeting Annapolis, MD
Shell run-off / selection
3/2-3/04 Annapolis, MD
Terminus run-off / selection
12/9-10/03 Washington, DC
9/4-5/03 Patuxent River, MD
5/6-8/03 Annapolis, MD
2/25-26/03 Washington, DC
11/14-15/02 Dahlgren, VA
5. 6/22/2004 5 Terminus Proposals Souriau
Radial
Delphi
6. 6/22/2004 6 NG Con Terminus
7. 6/22/2004 7 Terminus Comparison
8. 6/22/2004 8 NG Con Shell Draft
9. 6/22/2004 9 NG Con Shell Draft (continued)
10. 6/22/2004 10 Key Benefits Maintainability (reduced TOC)
Significant improvement especially cleaning
Major cost reduction
Reduced weight and space small
Commonality = qualification, training, repair and maintenance, logistics
Air and sea
Military and commercial
True multi vendor development and supply
Modular design
Maximize applicability and interchangeability
Genderless terminus
Accommodate multiple cable designs
11. 6/22/2004 11 Key Features LC performance anticipated
Benefits from commercial development
Pull resistant
Optical continuity maintained
Seal and clip on terminus
Enables visual inspection
Full mate indicator
Tactile objective
Potential tool-less removal
12. 6/22/2004 12 Requirements Inter-changeable Inter-operable parts
Multimode and Single-mode capable (125 mm OD)
Temperature range
Type 1 -40 to +85 degrees C operational
Type 2 - -55 to +125 degrees C operational
Future thermal ranges
55 to +165 degrees C operational (we need to validate 165)
55 to +200 degrees C - operational
Atmospheric sealing
EMI /RFI
Shock and Vibration Naval and aerospace
Keying option on terminus
13. 6/22/2004 13 Assumptions1 Rear release terminus
Removable Alignment Sleeve Retainer (ASR)
Equivalent to standard telecom bushing interchangeable part
Screw holds ASR during shock and vibration
Screw pushes ASR off terminus for removal
ASR preferred position on receptacle
Alignment sequence coarse to fine
Overall shell / keys, alignment pins, alignment sleeves
ASR screw, alignment pins, alignment sleeves, fiber
Designed to avoid end face damage and alignment pin bending
14. 6/22/2004 14 Assumptions2 Plug receptacle connection sealed
No interfacial seal
Optional rear grommet seal / accessory
Anti decoupling built into design
Receptacle and plug termini protrusion same
Implies similar insert dimensioning
Inserts
Design allows removable or integral
Removable inserts are genderless and retained without backshell (modular design)
Bottoming
Insert-to-insert required, shell-to-shell desired
15. 6/22/2004 15 Timeline Weekly teleconferences until 4/14
Additional working teleconferences
4/1 April Boeing commercial meeting
4/14-16 ARINC FOG
4/14 Evening working session
4/27 ARINC AEEC terminus decision
5/7 Shell system design drawings
6/24-25 NG Con meeting (ARINC Annapolis)
16. 6/22/2004 16 Conclusion US Navy is developing this technology
Qualification will be done
Requirements include both shipboard and aerospace
Maintenance and training will be developed
US Navy volume will drive cost reduction
Manufacturers designing the costs out
MANTECH sponsored development likely
17. 6/22/2004 17 Additional Aerospace Requirements Temperature range
-55 - + 125C (current Type II)
-65 - + 200 C (replace two future options)
Low profile rear grommet
Cable types
OC1060, OFS Flightguide, Tensilite
Shock and vibration
38999 Series 3, 1344 Method D (300 G, 300 ms)
Full mate
Visual indicator ring required for fleet maintainers
Backshell utilize 38999 family of backshells
Durability 500 mates / demates
18. 6/22/2004 18 For Further Information Contacts:
Gair Brown NSWC
540-653-1579 BrownGD@nswc.navy.mil
Mark Beranek Navair
301-342-9115 BeranekMW@navair.navy.mil
Mike Hackert NAVAIR
301-342-9124 Michael.Hackert@NAVY.mil