Ways to join thin components in a secure way and quick to unfasten

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SUMMARY

This discussion focuses on secure fastening methods for thin aerospace components, specifically a cylindrical lip and barrel configuration. The user seeks a solution that allows for quick unfastening at a single bottom location, avoiding traditional bolt joining and adhesive bonding due to space constraints. Participants suggest using threaded inserts, such as "Jack Nuts" or "Hollow Wall Sleeves," to create a reliable connection without compromising the thin structure of the components. The conversation emphasizes the importance of material selection and structural integrity in aerospace applications.

PREREQUISITES
  • Understanding of aerospace component design and requirements
  • Familiarity with fastening techniques for thin materials
  • Knowledge of threaded inserts and their applications
  • Basic principles of structural load mitigation
NEXT STEPS
  • Research "Jack Nuts" and their installation techniques for thin panels
  • Explore the use of "Hollow Wall Sleeves" in aerospace applications
  • Investigate alternative fastening methods for non-circular components
  • Study structural integrity assessments for thin aerospace components
USEFUL FOR

Aerospace engineers, mechanical designers, and anyone involved in the assembly and maintenance of thin structural components in aerospace applications.

theoster
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Hi guys/gals,

I am looking for ways to securely fasten components together for aerospace applications and in ways that can be quickly unfastened if replacement is required.

I have two main components, (1) a cylindrical (non-circular cross-section) lip in front of (2) a cylindrical barrel (non-circular as well). Two additional components attach at the (3) top and (4) bottom that provide structural support and load mitigation.

All are connected at the interface between the lip and the barrel, though there is space limitation at the higher half, so bolt joining (1) with (3) is not possible. Also, bonding (1)-(3) with adhesives is not preferred. Preferably, the joint should be fastened-unfastened at one (the bottom) location. The components are very thin as well.

I am looking forward to any answer.

Thanks,
T. S.
 
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Welcome to PF.

1. How thin is very thin?
2. What sort of dimensions?
3. What is the operating temperature range?
4. What is the material, metal, plastic or composite?
5. Is there a pressure differential, or it this a structural surface?

It would really help if you could attach a sketch or image that shows the four components assembled together.
 
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Does it have to hold pressure, or just the shape ??
Tangential, but I was faced with re-assembling under-sink back-board in-situ after repairing waste pipe where it ran through wall.

Said pipe gnawed by rats within wall would you believe ?? Took ~15 mins to replace the push-fit pipe, many miserable months to dry out then re-instate the rest...

For the panel's thick bracing, I could use threaded inserts, mending plates with 4x2 holes and allen-keyed bolts. Inserts placed before sawing. For the thin panel, I used metal 'winged' inserts that, spread by recommended tool, gripped panel and provided a threaded hard-point. "Jack Nuts - Screw Anchor - Spider Nut - Hollow Wall Sleeve - Steel, 25, M5"
Then simpler mending plates and more allen-keyed bolts to stitch seam...
See pic collage...
IMGP0328_10combo.jpg
 
Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming up shortly, I'll be following up afterwards to see how it all goes. :smile: https://blogs.nasa.gov/spacex/

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