Patent · US Active

Fitting, crane hook, and crane hook assembly

US8313131B2 · kind B2 · utility

2Cited by
25References
10Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 14, 2008
Grant dateNov 20, 2012
Priority date
Expiry dateMay 18, 2029

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T403/32631
  • WIPO fieldHandling
  • WIPO sectorMechanical engineering

Abstract

A method of lifting an aircraft at a lifting location, the method comprising: securing a fitting (10) to the aircraft when the aircraft is at the lifting location; engaging the fitting with a crane hook (100); transmitting lifting load from the crane hook to the aircraft via the fitting; and removing the fitting from the aircraft. A fitting (10) for transmitting lifting loads from a crane hook (100) to an item, the fitting comprising: an attachment member (11) configured to be secured to the item; and a lifting member (12) which is pivotally coupled to the attachment member and configured to be engaged by the crane hook (100) so as to transmit lifting loads from the crane hook to the item. A crane hook (100) with a ball-and-socket connection is provided. The crane hook has an attachment link (106) having a first pivot point (107) attached to the hook forward of its center of gravity, and a second pivot point (109) configured to be lifted by a crane, —and a biasing system which applies a biasing force to the attachment link causing the attachment link to rotate about the first pivot-point whereby the second pivot point moves towards the rear of the hook when the hook is unloaded.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.