moltenmetal- your last comment brings up a good point about how locking of threaded fasteners is approached from a reliability standpoint in industries like aerospace.
As I understand it, the helical split lock washer works by creating an axial preload on the bolt/nut when it it compressed below its free height. And if this axial preload force produces sufficient friction at the thread contacts to prevent any relative movement/loosening, then it does provide some thread locking function. But unfortunately, the amount of axial preload force produced by the typical helical split lock washer, even when fully compressed, is often not sufficient to prevent loosening of a bolt/nut, especially if the joint is subject to any vibration or dynamic loading.
In aerospace, threaded fastener installations where the bolt/nut is loaded in tension often require a single fault tolerance level of reliability for the fastener locking function, which basically means each fastener must employ two separate methods of securing the threads. One common approach used to meet the single fault tolerance requirement is through a combination of using controlled installation torque to create fastener preload, and using a locking feature like a deformed section of the internal threads on the nut/insert that will continue to maintain a locking function after the loss of preload. Since a split helical washer will lose its locking function once it is no longer compressed, it is not considered a suitable form of thread locking device for aerospace applications.
Interesting topic.
Terry