SAE ARP265

Airfoil Shapes - Dimensioning of Turbine Engine .

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Standard:
  • ARP265
Revised:
  • 1952-02-01
Revision:
  • Historical. Access the latest revision: ARP265A
Issuing:
  • E-25 General Standards For Aerospace And Propulsion Systems
Scope:

This Aeronautical Recommended Practice provides a standard method for locating and dimensioning the airfoil portions of parts such as blades, and vanes. This method will apply to blades, or vanes with or without a base. The forms of attachment are varied; therefore, the blade bases shown in the following figures are for illustration only. All dimensions and notes shown pertaining to the common functional point, line or plane are considered to be applied to a datum, on or off the part, irrespective of the form of attachment.

History:
StandardPublishedRevisionStatus
ARP265A1959-02-01LatestCancelled
ARP2651952-02-01HistoricalRevised
AKA:
  • SAE ARP 265
Sector:
  • Aerospace
Topic:
  • Gas turbines

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