The basic jigger mechanism was used very widely, for a range of machines across dockyards, warehouses, railway yards and engineering workshops. They were even to be found in theatres, lifting the stage curtains.
Cranes The first application of jiggers had been for Armstrong's first hydraulic crane and this remained an important application for them. A distinctive type of crane was the warehouse wall crane or 'whip'. The ram was mounted vertically on an outside wall with a small jib or fixed pulley above it. The space available by external mounting allowed the use of long cylinders and very long lifts, spanning several floors.
Portable winches ,
Liverpool Many dockyards used small portable jiggers mounted on wheeled carriages. These could be moved around the quays as needed, and plumbed into outlets in the hydraulic mains with screwed pipe unions. They were used as portable
winches for all manner of tasks. A typical task would be winching bales out of the hold of a ship, up a sloping gangway. Bales of bulk products such as
jute or
cotton were made too large and heavy for dockers to lift by hand, and the jigger appeared at a time when cranes were still only in limited numbers.
Lifts Jiggers were also used for
freight lifts in warehouses and factories. These were not accepted for passenger carrying though, until 1854 and
Elisha Otis' invention of the safety brake, to prevent the carriage falling if the hoisting cable were to break.
Catapult launch British
aircraft carriers of World War II used a form of pneumatic-hydraulic jigger to power their
aircraft catapults. The catapults had a travel and an 8:1 pulley ratio, requiring a power cylinder. One side of the cylinder was connected to a manifold of a dozen high-pressure compressed air bottles. Power for launching was supplied by the compressed air. The other side was filled with hydraulic fluid. When the launch valve was triggered, the hydraulic fluid pressure dropped rapidly as fluid was vented into an unpressurised catch tank. The piston was forced rapidly from the air end to the hydraulic end, pulling the crosshead and the jigger pulleys and drawing the launch trolley forwards. The average acceleration for an aircraft was 1
g, with a peak of 2.5 g. After launching, the piston was decelerated within the cylinder by a conical protrusion entering a narrow choke ring, and the hydraulic resistance increasing as the flow area reduced. Hydraulic fluid was then pumped from the catch tank by an electric pump and back into the cylinder under pressure. The cylinder was double-ended, with a piston rod and jigger at each end, and the catapult was retracted by the hydraulic pressure forcing the piston backwards, and re-compressing the air reservoirs. == See also ==