Sunday, February 20, 2011

Heat Treatment Of carbon Steel

Heat treatment is a series of operations involving the heating and cooling of steel in the solid state. Its purpose is to change the mechanical properties of the steel so that it will be harder, stronger or more resistant to impact. It can also make a steel softer and more ductile.

No single heat treatment can produce all these characteristics. Some properties may be improved at the expense of others eg. when being hardened a steel may become ‘brittle’.

Heat treatments are normally carried out by heating and cooling the steel. The temperature to which the steel is heated and the rate of cooling is most important.
Plain high carbon steels can be:

  • ANNEALED
  • NORMALISED
  • HARDENED
  • TEMPERED
Annealing
This is a softening heat treatment. In general terms the steel is heated to its upper critical point and then ‘allowed to cool very slowly in the furnace’.

Normalising
This is a form of heat treatment in which the steel is heated to its upper critical point and ‘allowed to cool slowly in still air’. Normalising restores the crystalline structure and relieves stresses in the steel.

Hardening
This is a heat treatment whereby steel is made hard and brittle by heating to the upper critical point and immediately quenching in water or oil.

Tempering
This is a heat treatment process in which some of the hardness is removed from the steel to increase its toughness and decrease its brittleness. After hardening, the steel is reheated to a fairly low temperature (below the lower critical point) then quenched in water.

The temperature depends on the purpose of the tool. The higher the tempering temperature, the less the hardness but the greater the toughness. Thus the purpose of the tool or article must be considered.
The temperature required may be judged from the temper colours which appear on the bright surface of steel which is heated slowly.

Friday, February 18, 2011

Aircraft Fasteners

The word FASTENER is used to describe all of the various types of fastening device used in the construction of an aeroplane. This is because the meanings of the words BOLT and SCREW for example, may be interpreted differently by separate organisations.

A bolt is an externally threaded fastener designed for insertion through holes in the assembled parts. Bolts usually have a plain (unthreaded) portion on the shank. A bolt is normally intended to be tightened or released by turning or torquing the nut.
 A screw is an externally threaded fastener capable of being screwed into preformed threads in the assembled parts. It is normally intended to be tightened or released by turning or torquing the head. A screw has a fully threaded shank. Certain types of screw such as self tapping screws and woodscrews form a thread when they are screwed into place.

A standard fastener comprises of a threaded portion, a head and sometimes a plain shank or grip.  Between the shank and the thread is a small tapered transition zone.  Between the shank and the head is stress relieving fillet radius.
A fastener will be defined by a number of features which are given in detail in it’s specification.  These include it’s Thread Form, Shank Diameter, Head Style, Grip Length, Material, Surface Finish and Locking Facilities.

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