Fitting, crane hook, and crane hook assembly
View Patent ↗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.
1. Apparatus for lifting an aircraft at a lifting location, the apparatus comprising:
a fitting configured to be secured to the aircraft when the aircraft is at the lifting location; and
a crane hook configured to engage the fitting and transmit lifting load to the aircraft via the fitting, the crane hook comprising a shank portion and a hook portion extending from the shank portion,
wherein the fitting comprises a socket or ball with a semi-spherical surface, and the hook portion comprises a ball or socket with a semi-spherical surface configured to engage the semi-spherical surface of the socket or ball on the fitting and transmit lifting load to the aircraft via the fitting.
2. The apparatus of claim 1 wherein the fitting has a first part configured to engage the crane hook; and a second part configured to engage a lowering device.
3. The apparatus of claim 2 wherein the first part of the fitting is pivotally coupled to the second part of the fitting.
4. The apparatus of claim 1 wherein the fitting comprises:
an attachment member configured to be secured to the aircraft; and
a lifting member which is pivotally coupled to the attachment member and configured to be engaged by the crane hook so as to transmit lifting loads from the crane hook to the aircraft.
5. The fitting of claim 4 further comprising a locking member which is movable from a release position to a locking position in which the locking member locks the lifting member in an operative position relative to the attachment member.
6. The fitting of claim 4 wherein the lifting member is reversible with respect to the attachment member.
7. A method of lifting an aircraft at a lifting location, the method comprising:
securing a fitting to the aircraft when the aircraft is at the lifting location;
engaging the fitting with a crane hook;
transmitting lifting load from the crane hook to the aircraft via the fitting; and
removing the fitting from the aircraft,
wherein the fitting comprises a socket or ball with a semi-spherical surface, and the crane hook comprises a ball or socket with a semi-spherical surface which engages the semi-spherical surface of the socket or ball on the fitting and transmits lifting load to the aircraft via the fitting.
8. The method of claim 7 wherein the lifting load is transmitted to a spar of a wing of the aircraft.
9. The method of claim 8 wherein the lifting load is transmitted to the spar by a side stay fitting of a main landing gear.
10. The method of claim 7 further comprising lowering the fitting into position with a lowering device.