BASIC PARTS TO THE HIGH SPEED PULSE FIRED TURBINE

This is a flow through device containing turbine style generators for compression of air and the extrapolation of energy. This is a timed pulse engine generating a combustion cycle by using a revolving valve to initiate and control loading of the combustion chamber with air/ a sealed chamber for explosion of the fuel air mixture,/ and a timed port opening for energy transference into the vanes of the propulsion turbine. There are no reciprocating parts. The basic arrangement is a turbine initiating the sequence by compressing air, as is common to all fuel/air thermal engines. That compressed air is injected into a stationary combustion chamber, where fuel is injected and ignition occurs. The heated air is then directed through the exhaust port into the impulse or energy vanes of the second turbine. Primary to the machine is the rotating valve.

The valve uses a timed alignment of revolving parts to close the exhaust port and open the intake port, the chamber is then sealed by the revolution of those parts, and combustion of the fuel air mixture occurs. Expansion is allowed to occur and the alignment of the valve directs the energy turbine to consume that expansion as the power cycle, and rotate the shaft. The cycle pattern is therefore the same basic relationship as a common 4 cycle piston engine. The valves themselves are either produced in direct association with the turbine wheels using alignment and direction to allow the valving to be integrated into the wheel itself/ or gearing creates a valving disk which then functions independently or with the compression turbine itself. The valving disk is a hollow cylindrical shape with ports on one side, and complimentary ports at the top of the rotating cylinder which then align with the combustion chamber [ this to allow transference of energy impulse to create a minimum effect upon the bearing arrangement.] Side alignment is also useful but transference of energy should be directed at the outer edge of the energy turbine anyway. The same is allowed for a disk valve in the exhaust side. The compression turbine may be powered independently, in unison with the exhaust turbine, or by bleeding the combusted air back into the compression turbine. Careful work regarding the location of the bleeders, will result in reintroduction of the most suitable fuel by-products for the ignition cycle to refine. This is then a cycling flow through, thermal engine where valving can either occur on the edges of the turbines, or be geared to operate within a specific range for dedicated work.

Primary to the use of rotating disks is the sealed surface & each of these valving arrangements uses primary or critical clearance, with labyrinth seals or vanes, and on the top surfaces a rotary engine style "wiper blade" in conjunction with labyrinth seals. Labyrinth seals are essentially "like a zipper, at the edge,only where the surfaces do not touch/ or perhaps like a set of stacked bricks from top to bottom which then create a zigzag pattern. They rotate within themselves. A wiper blade variation would be to introduce to "boomerang patterns in line with each other/ the first in line with the compression source has an opening in the middle of it to compress air and small circular openings at each side to redirect the compression of air/ the second attempts to close the area and redirect the turbulence created by the first. Lubrication for the engine is as is common to all turbines.