Click Here to
Order this information in Print

Click Here to
Order this information on CD-ROM

Click Here to
Download this information in PDF Format

 

Click here to make tpub.com your Home Page

Page Title: FASTENERS (SPECIAL)
Back | Up | Next

Click here for a printable version

Google


Web
www.tpub.com

Home


   
Information Categories
.... Administration
Advancement
Aerographer
Automotive
Aviation
Combat
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion
USMC
   
Products
  Educational CD-ROM's
Printed Manuals
Downloadable Books

   
Back
ALLOY 5056 RIVETS
Up
Aviation Structural Mechanic (H&S) 3&2 - How airplanes are built and how to maintain them
Next
Jo-Bolt  Fasteners

Figure 2-5.—Sectional view of rivnut showing head and end designs. Hi-shear  rivets  are  identified  by  code  numbers similar  to  the  solid  rivets.  The  size  of  the  rivet  is measured in increments of thirty-seconds of an inch for the diameter and sixteenths of an inch for the grip length.  For  example,  an  NAS  1055-5-7  rivet  would  be a hi-shear rivet with a countersunk head. Its diameter would be 5/32 of an inch and its maximum grip length would be 7/16 of an inch. The collars are identified by a basic code number and a dash number that correspond to the diameter of the rivet. An A before the dash number indicates an aluminum alloy collar. The NAS528-A5 collar would be  used  on  a  5/32-inch-diameter  rivet  pin.  Repair procedures involving the installation or replacement of  hi-shear  rivets  generally  specify  the  collar  to  be used. Rivnuts The  rivnut  is  a  hollow  rivet  made  of  6063 aluminum alloy, counterbored and threaded on the inside. They are manufactured in two head styles, flat and countersunk, and in two shank designs, open and closed  ends.  See  figure  2-5.  Each  of  these  rivets  is available in three sizes: 6-32, 8-32, and 10-32. These numbers indicate the nominal diameter and the actual number of threads per inch of the machine screw that fits into the rivnut. Open-end rivnuts are the most widely used, and are  recommended  in  preference  to  the  closed-end type.  However,  in  sealed  flotation  or  pressurized compartments, the closed-end rivnut must be used. FASTENERS (SPECIAL) Fasteners  on  aircraft  are  designed  for  many different  functions.  Some  are  made  for  high-strength requirements,  while  others  are  designed  for  easy installation and removal. Lock-Bolt Fasteners Lock-bolt   fasteners   are   designed   to   meet high-strength  requirements.  Used  in  many  structural applications, their shear and tensile strengths equal or exceed  the  requirements  of  AN  and  NAS  bolts. The lock-bolt pin, shown in view A of figure 2-6, consists of a pin and collar. It is available in two head styles: protruding and countersunk. Pin retention is accomplished by swaging the collar into the locking grooves  on  the  pin. The   blind   lock   bolt,   shown   in   view   B   of figure 2-6, is similar to the self-plugging rivet shown in figure 2-3. It features a positive mechanical leek for pin retention. Hi-Lok Fasteners The  hi-lok  fastener,  shown  in  figure  2-7,  com- bines the features of a rivet and a bolt and is used for high-strength,   interference-free   fit   of   primary structures.  The  hi-lok  fastener  consists  of  a  threaded pin and threaded locking collar. The pins are made of Figure 2-6.—Lock bolts. 2-4

Privacy Statement - Press Release - Copyright Information. - Contact Us - Support Integrated Publishing