Aircraft landing-gear step

Information

  • Patent Grant
  • D1009762
  • Patent Number
    D1,009,762
  • Date Filed
    Thursday, January 3, 2019
    5 years ago
  • Date Issued
    Tuesday, January 2, 2024
    11 months ago
  • US Classifications
    Field of Search
    • US
    • D12 1- 4
    • D12 161
    • D12 319-345
    • D12 400
    • D12 159
    • D12 160
    • D12 190
    • D12 196
    • D12 203
    • D21 436-453
    • CPC
    • B64C27/20
    • B64C2201/024
    • B64C2201/104
    • B64C2201/021
    • B64C2201/141
    • B64C25/52
  • International Classifications
    • 1207
    • Term of Grant
      15Years
Abstract
Description


FIG. 1 a bottom perspective view of the aircraft landing-gear step.



FIG. 2 is a front elevational view of the landing-gear step as configured in FIG. 1.



FIG. 3 is a rear elevational view of the landing-gear step as configured in FIG. 1.



FIG. 4 is a left side elevational view of the landing-gear step as configured in FIG. 1.



FIG. 5 is a right side elevational view of the landing-gear step as configured in FIG. 1.



FIG. 6 is a top plan view of the landing-gear step as configured in FIG. 1.



FIG. 7 is a bottom plan view of the landing-gear step as configured in FIG. 1.



FIG. 8 is a top perspective view of the aircraft landing-gear step shown in an environment of use.



FIG. 9 is an oblique view of the left landing-gear step, the door being configured in a closed position.



FIG. 10 is a front elevational view of the landing-gear step as configured in FIG. 9.



FIG. 11 is a rear elevational view of the landing-gear step as configured in FIG. 9.



FIG. 12 is a left side elevational view of the landing-gear step as configured FIG. 9.



FIG. 13 is a right side elevational view of the landing-gear step as configured in FIG. 9.



FIG. 14 is a top plan view of the landing-gear step as configured in FIG. 9.



FIG. 15 is a bottom plan view of the landing-gear step as configured in FIG. 9; and,



FIG. 16 is an oblique view of the landing-gear step as configured in FIG. 9.


The broken lines shown in FIGS. 1-7 and 9-15 illustrate portions of the aircraft landing-gear step that form no part of the claimed design; the additional broken lines shown in FIGS. 8 and 16 are for purposes of illustrating environmental subject matter only and forms no part thereof. The right side not shown is understood to be a mirror image of the left side shown in FIGS. 1-8 and 9-16.


Claims
  • The ornamental design for an aircraft landing-gear step, as shown and described.
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