Aircraft structures are also required to be designed to withstand the limit load multiplied by a ` saGety factor ( 1 . 5 ) without failure for at least three seconds.
12.
The front safety belts incorporate pretensioners to better position the occupant during a crash and force limiters that work in conjunction with the front airbags to limit loads on the chest.
13.
Also, since working materials into the plastic range can lead to permanent deformation of the structure, additional analyses may be required at limit load to ensure no detrimental permanent deformations occur.
14.
Strength requirements are specified in terms of limit loads ( the maximum loads to be expected in service ) and ultimate loads ( limit loads multiplied by prescribed factors of safety ).
15.
Strength requirements are specified in terms of limit loads ( the maximum loads to be expected in service ) and ultimate loads ( limit loads multiplied by prescribed factors of safety ).
16.
Unrestricted by the rule that limits load widths to 12 to 14 feet when trucks travel on interstate roads, Capsys ships units that are 18 feet wide, 10 { feet high and 37 feet long.
17.
Like all aircraft structures, the tail was designed to function even if it was subjected to 50 percent more force than its " limit load, " the highest load that it was expected to see in its lifetime.
18.
The normal load factor on a plane in straight and level flight would be about 1 G . The safety board said those loads were " well in excess " of the certified limit load for that kind of plane.
19.
In aeronautics, "'limit load "'( LL ) is the maximum load factor authorized during flight, Mathematically, limit load is LL = LLF x W, where LL = limit load, LLF = limit load factor, and W = weight of the aircraft.
20.
In aeronautics, "'limit load "'( LL ) is the maximum load factor authorized during flight, Mathematically, limit load is LL = LLF x W, where LL = limit load, LLF = limit load factor, and W = weight of the aircraft.
