Aircraft angle of attack indicator

Information

  • Patent Grant
  • D731333
  • Patent Number
    D731,333
  • Date Filed
    Monday, July 15, 2013
    11 years ago
  • Date Issued
    Tuesday, June 9, 2015
    9 years ago
  • US Classifications
    Field of Search
    • US
    • D10 67
    • D12 174
    • 073 1780R0
    • 073 1780T0
    • 073 866300
    • 340 945000
    • 340 951000
    • 340 967000
    • 340 971000
    • 340 974000
    • 701 004-006
    • 701 018000
    • CPC
    • B64D43/00
    • G01C23/005
    • G01P3/62
  • International Classifications
    • 1004
    • Term of Grant
      14Years
Abstract
Description

The file of this patent contains a least one drawing in which elements of the design include color. Elements embodied with color are represented by black and white cross-hatching for the colors green, yellow, red and white.



FIG. 1 is a front drawing of the aircraft angle of attack indicator in which an airfoil element represents an optimal landing approach angle of attack condition.



FIG. 2 is a front drawing of the aircraft angle of attack indicator in which the airfoil element, in an alternative position, indicates a sub-optimal landing approach angle of attack condition.



FIG. 3 is a front drawing of the aircraft angle of attack indicator in which the airfoil element, in an alternative position, indicates an excessive and cautionary landing approach angle of attack condition yet an acceptable flight angle of attack condition; and,



FIG. 4 is a front drawing of the aircraft angle of attack indicator in which the airfoil element, in an alternative position, indicates a stall angle of attack condition.


Claims
  • The ornamental design for the aircraft angle of attack indicator, as shown and described.
US Referenced Citations (2)
Number Name Date Kind
D288412 Nunes Feb 1987 S
8421649 Marstall et al. Apr 2013 B2