Device for the bearing harmonization of an airborne load

Claim 2

In a system for releasably suspending a load from an aircraft, having a housing structure carried by the aircraft, a pair of longitudinally spaced hooks within said housing and pivotally movable between a position engaging the load for the suspension thereof and a position releasing said load, and link means connected to said hooks for controlling the pivotal movement thereof, the improvement which consists of a device for adjusting in a horizontal plane the position of the suspended load, said device comprising: (i) a screw engaging a tapped hole formed through a side wall of said housing structure along a transverse horizontal axis, (ii) a supporting block rigid with said screw and on which are pivoted one of said hooks and a bell crank linkage controlling the pivotal movement of said hook, and (iii) means for locking said supporting block in relation to the housing structure, rotation of said screw causing a transverse movement in an horizontal plane of said one hook.

Claim 3

In a system for releasably suspending a load from an aircraft, having a housing structure carried by the aircraft, a pair of longitudinally spaced hooks within said housing and pivotally movable between a position engaging the load for the suspension thereof and a position releasing said load, and link means connected to said hooks for controlling the pivotal movement thereof, the improvement which consists of a device for adjusting in a horizontal plane the position of the suspended load, said device comprising: (i) a socket movable in a longitudinal slot of said housing structure, (ii) a rotatable member having a cylindrical upper part rotatably engaged through said socket and a cylindrical lower part eccentric in relation to said upper part; (iii) a supporting block secured for translation to said lower part and on which are pivoted one of said hooks and a bell crank linkage controlling the pivotal movement of said hook, said hook being a double hook adapted to co-act with a saddle member of the load, (iv) a transversely disposed packing strip rigid with said supporting block and guided in a groove transversely formed in said housing structure, and (v) means for locking said rotatable member in relation to the housing structure, rotation of said rotatable member causing a transverse movement in an horizontal plane of said one hook.

Claim 4

In a system for releasably suspending a load from an aircraft, having a housing structure carried by the aircraft, a pair of longitudinally spaced hooks within said housing and pivotally movable between a position engaging the load for the suspension thereof and a position releasing said load, and link means connected to said hooks for controlling the pivotal movement thereof, the improvement which consists of a device for adjusting in a horizontal plane the position of the suspended load, said device comprising: (i) a socket movable in a longitudinal slot of said housing structure, (ii) a rotatable member having a cylindrical upper part rotatably engaged through said socket and a cylindrical lower part eccentric in relation to said upper part; (iii) a supporting block secured for translation to said lower part and on which are pivoted one of said hooks and a bell crank linkage controlling the pivotal movement of said hook, said hook being a double hook adapted to co-act with a saddle member of the load, (iv) a transversely disposed packing strip rigid with said supporting block and guided in a groove transversely formed in said housing structure, and (v) means for locking said rotatable member in relation to the housing structure, rotation of said rotatable member causing a transverse movement in an horizontal plane of said one hook.

Claim 5

A system, as claimed in claim 2, wherein said supporting block also carried symmetrical lateral bearing arms for ensuring wedging of the load.

Claim 6

A system, as claimed in claim 2, wherein said cylindrical lower part of said rotatable member has a lower extension in the form of a centering stud adapted to be inserted in an upper cavity of said load saddle.

Claim 7

System, as claimed in claim 2, wherein an additional hook is pivoted to said supporting block, said additional hook co-acting with said one hook and being adpated to carry a load equipped with standard rings.

Claim 8

A system, as claimed in claim 4, wherein said centering stud is provided with a longitudinally slidable member adapted for being inserted into said saddle upper cavity in such a manner that the movement of said slidable member permits an easy insertion thereof into said saddle cavity when a transverse movement of said centering stud has taken place.

Claim 9

A system, as claimed in claim 6, wherein said slidable member has a toroidal shape the external diameter of which corresponds with the internal diameter of the saddle cavity for easy insertion of said slidable member into said cavity with minimal clearance.

Claim 10

A system, as claimed in claim 7, wherein the slidable member has an elongated aperture with parallel longitudinal sides in contact by relatively large surfaces with external longitudinal sides of a prismatic part of the centering stud adapted to pass through said aperture.

Claim 11

A system, as claimed in claim 4, wherein a second centering stud is associated with the other hook of said pair of hooks, said second centering stud being provided with a longitudinally slidable member adapted for being inserted into a corresponding saddle cavity in such a manner that the movement of said slidable member permits easy insertion thereof into said corresponding saddle cavity when a transverse movement of the lower part of the rotatable member has taken place.

Claim 12

A system, as claimed in claim 9, wherein said slidable member has a toroidal shape the external diameter of which corresponds with the internal diameter of the corresponding saddle cavity for easy insertion of said slidable member into said corresponding cavity with minimal clearance.

Claim 13

A system, as claimed in claim 10, wherein said slidable member has an elongated aperture with parallel longitudinal sides in contact by relatively large surfaces with external longitudinal sides of a rectangular sectioned part of the second centering stud adapted to pass through said aperture.