Aircraft ski mounting assembly

• US 4,390,151 A
• Filed: 02/20/1981
• Issued: 06/28/1983
• Est. Priority Date: 02/20/1981
• Status: Expired due to Fees

• Current Assignee: Richard J. Schneider
• Original Assignee: Richard J. Schneider
• Inventors: Schneider, Richard J.
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US06/236,205
• Time in Patent Office: 858 Days
• Field of Search: 244/105, 244/108, 244/100 R, 244/101, 280/7.12, 280/7.14, 280/8, 280/13, 280/9, 280/11, 280/10, 280/21 A, 280/25, 280/28, 180/5 R
• US Class Current: 244/108
• CPC Class Codes: B64C 25/52 Skis or runners

Abstract

A ski mounting assembly for an aircraft landing gear having a ski with a pedestal attached to it to be placed on each side of the landing gear wheel and fork, an extended wheel axle to serve as an axle for the wheel, a mounting for the wheel in the landing gear fork and to serve as a pivotable support for the ski by extending through journals in the ski pedestals, a ski attitude control arm pivotably mounted on one end of the extended wheel axle and provided with a clamp to secure the ski attitude control arm to the landing gear fork, a stop attached to the ski attitude arm so as to act against the ski to limit the downward motion of the ski nose and a spring acting between the ski and the ski attitude control arm to urge the ski against the stop.

Claims

1. An aircraft ski mounting assembly for an aircraft landing gear comprising:

a. a ski having toe and heel portions, a bottom surface for contact with a landing surface and a pedestal integral with and protruding from the upper surface of the ski;

b. a ski attitude control arm pivotably attached to said pedestal on an axis transverse to the ski, said arm being operably biased into a generally upright position against a stop limiting the maximum distance between the upper end of the arm and the toe of the ski; and

c. a landing gear attachment means operably secured to said arm whereby the arm may be attached to the terminal end of an aircraft landing gear in a fixed relationship, the biased pivot between arm and ski pedestal thus acting to allow accomodation of the ski to limited changes of attitude between aircraft and landing surface without the ski toe dropping to dig into the landing surface.

2. An aircraft ski mounting assembly as claimed in claim 1 wherein the pivot for said ski attitude control arm may be an extension of the aircraft landing gear wheel axle.

3. An aircraft ski mounting assembly as claimed in claim 1 also comprising a replacement axle for the landing gear wheel for said aircraft, said replacement axle being sufficiently long to extend through said pivot point of said ski attitude control arm whereby the landing load on said ski will be transferred to the landing gear through the replacement axle in shear.

4. An aircraft ski mounting assembly as claimed in claim 1 wherein said ski also comprises a second pedestal attached to the ski upper surface parallel to and spaced sufficiently from the other pedestal to accomodate an aircraft landing gear wheel and strut therebetween, and wherein said assembly also comprises a replacement axle for the landing gear wheel for said aircraft, said replacement axle being sufficiently long to extend through said pivot point of said ski attitude control arm and each of the pedestals whereby said ski is operably attached to said landing gear strut by the replacement axle as a pivot.