Boundary Layer Turbine

Design Rationale

Drawings by Dan Granett, Granett Engineering:

This is an external combustion engine with proven efficiencies of 25% for un-optimized models with steam (Rice, Warren, Transactions of the ASME, Journal of Engineering and Power, January 1965, pp. 28-36). A working fluid spins this turbine by means of surface friction. When the disk spacing is small (on the scale of a millimeter), energy transfer from the working fluid to the disks can be efficient. Design rationale:

Working fluid (such as steam) enters tangentially to the disks through a nozzle:

Bearings must be protected from the working fluid with a shaft seal seal:

Working fluid must be prevented from escaping past the outer disks so that it can transfer its energy effectively to all the disks. To do this, we put in a ring seal: