In general, combustion gas, which actuates the gas turbine contains a large amount of air,approximately 4 times the theoretical amount. By conventional technology, heat energy is consumed and nearly 80% of the compressed air is circulated and discharged, resulting in a tremendous loss in efficiency. By using 100% or the compressed air for combustion and

increasing the compression ratio and fuel combustion mass by 400%　through heat exchange including supercritical overheated steam (impossible pressure ratio in air compression), reduce heating value used by gas turbine among supply heating value, increase air plane promotion efficiency and gas turbine heat efficiency by around 300%,increase power generation efficiency by about 200% by driving all moving blade steam turbine by overheated steam including supercritical which was gained through heat exchange so that combustion gas temperature becomes lower than the turbine heat resistance boundary temperature (japanese patent No. 2604636), or changing inefficient screw promotion to steam, water, and air ship bottom jet floating promotion to triple ship promotion speed, and reduce CO2 discharge by half.

*i.e. As shown in figure 9, 10, and 11, mount the generator , or turm over　compressor, or tum over gas turbine or steam gas turbine in the middle. As shown in figure 11, curve it to make it bigger, and as shown in figure 12, by making a water cooling jacket of a combustor spiral welding structure including a conduit tube 1 to elevate pressure it is possible ti use the gas turbine combustor as a heat exchanger, which has beenenlarged and pressyre-elevated.Therefore, conventional output can be maintained even though 100% of the compressed air is　used for combustion. The quadrupled fuel combustion mass reduces the heat value of gas turbine to the lower limit.Higher the pressure ratio and a higher gas turbine heat efficiency results. Withfuel combustion of the same heating value,the bigger the pressure ratio is, the higher the temperature increases. ln addition to that, when gas temperature at the turbine inlet is 700℃ or 1000℃, heat exchange improves, enabling increased heat nefficiency of the supercharging boiler cycle and gas turbine cycle to the limit.　Therefore, discharge loss by pressure ratio increases and reduction of heat exchanger exhaust heat temperature can be greatly reduced.

*High temperature and air compression unnecessary for combustion are harmful to gas turbine, and blade cooling should be unnecessary. It is the best to compress and heat water which expands in atmospheric　pressure by 170000% and is easily compressed.

*i.e. As shown in figure 11, 13, and 14, with an all-moving blade,relative peripheral velocity is almost doubled and small sized output can be achieved at a constant　allowable stress.Or by doubling rotatingradius and relatiive peripheral velocity between moving　blades,greater output, more than 4 times of ratio output, can be achieved. Or by tripling rotating radius and doubling relative peripheral velocity between moving blades, even greater output, 9 times of ratio output, can be achieved. Furthermore,with the relative peripheral velocity between moving blades with conventional technology, allowable stressdrops to almost one fourth because peripheral velocity can be halved. lnexpensive　turbine or compressor can be produced by casting turbine blades andcompressor blades in a circle.

(3) Reduce CO2 discharges in half with power transmission by rolling contact.
Gears used to transmit power lose heat through friction because the power transmission surface slips on the gear surface. ln order to transmit large amounts of　power or very high speed power, a large lubrication oil cooler and friction are necessary, but are not very practical.　 However, if magnetic friction power transmission 14 is used, power transmission by rolling contact is possible as shown in figure 15 and a more preferable form of power transmission using water cooling instead of oil can be achieved. ln addition, various convex and concave surfaces for increasing friction can be made smaller and magnetic power can be adjusted in either direction. Therefore, the clutch can be deleted or its weight can be greatly reduced. By realizing practical use of various kind of all-moving blade steam turbine and all-moving blade gas turbine, CO2 emissions can be halved from fossil fuel power generation equipment or fossil fuel ship promtion equipment.
*i.e. Various types of power transmission including normal speed change and reversal rotation mainly use gearing. The gear surfaces require a slip gearing surface, which　intum requires a big load,and it needs lubrication oil, friction heat loss is very large,big power transmission including high speed rotation is not good for resistance against abrasion. ln order to put various all-moving blade turbines into practical use, it is inevitable to use magnetic friction power transmission 14 which can transmit large amounts of power most efficiently through rolling contact. By using various magnetic friction cars instead of various gearing, mount flat irregular cars instead of flat gearing cars, helical irregular cars instead of helical gear, double helical irregular cars instead of double helical gear to power transmission surfaces, as a magnetic frction car and magnetic frction equipment (magnetic friction power transmission 14), various magnetic friction power transmission 14 consists of well-known various qearing power transmission, magnetic friction power decelerating transmission, magnetic friction power reversal transmission and magnetic friction speed change gear. This is a complete rotary engine.　　　　

If you agree to the above Tanigawa's pollution reduction theory, refer to PCT international number PCT/JP 97/2250, international application date: june 27,1997,and cooperate with me including joint patent application. In japanese system, we do not do a study which large companies participate in the middle, and I am in trouble because the study of CO2 reduction internal combustion engine can be a suitable target.
So I hope that this can be guided by the U.S.A. as motor revolution by asking President Clinton including Vice President Gore. This invention started from Japanese patent No. 2604636 all moving blade steam turbine, applied on January 22,1990.