首页> 外国专利> METHOD Changing the angle of the Earth's axis to the plane of its orbit around the Sun.

METHOD Changing the angle of the Earth's axis to the plane of its orbit around the Sun.

机译:方法改变地球轴相对于围绕太阳的轨道平面的角度。

摘要

1.method u0438u0437u043cu0435u043du0435u043du0438u00a0 inclination of the axis to the plane of its orbit around the earth u0432u0440u0430u0449u0435u043du0438u00a0 sun u0437u0430u043au043bu044eu0447u0430u044eu0449u0438u0439u0441u00a0 daily long-term impact on the earth's surface n u0430u043fu0440u0430u0432u043bu0435u043du043du043eu0439 to the center of the vertical force that develops u0442u00a0u0433u043eu0432u0430u00a0 installation, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 orderwhat u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 one-time short-term daily impact on the earth's surface, at least one fixed u0442u00a0u0433u043eu0432u043eu0439 installation at the time of u043fu0435u0440u043fu0435u043du0434u0438u043au0443u043b u00a0u0440u043du043eu0441u0442u0438 plane u043fu0440u043eu0445u043eu0434u00a0u0449u0435u0439 through geographical pole of earth, in which is located u0432u0435u0440u0442u0438u043au0430u043bu044cu043du0430u00a0 power u0432u043eu0437u0434u0435u0439u0441u0442u0432u0438u00a0, vertical to the earth's orbit p u043bu043eu0441u043au043eu0441u0442u0438, in which is located the u0432u0440u0430u0449u0435u043du0438u00a0 landahead of midnight in the northern hemisphere and southern hemisphere on u0430u0441u0442u0440u043eu043du043eu043cu0438u0447u0435u0441u043au043eu043cu0443 u043fu043eu043bu0434u043du00a0 ahead of time for 1 / 4 of the earthly days.;2. method for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 1, so that a single brief daily impact on the earth's surface u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 within no more than 2 minutes.;3. method for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 1, so that a single brief daily impact on the earth's surface u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 ahead of time u0432u043au043bu044eu0447u0435u043du0438 design u00a0 at 1 / 2 length of its u0432u043au043bu044eu0447u0435u043du0438u00a0.
机译:1.方法 u0438 u0437 u043c u0435 u043d u0435 u043d u0438 u00a0轴相对于其绕地球轨道平面的倾斜度 u0432 u0440 u0430 u0449 u0435 u043d u043d u0438 u00a0太阳 u0437 u0430 u043a u043b u044e u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0每天对地球表面的长期影响n u0430 u043f u0440 u0430 u0432 u043b u0435 u043d u043d u043e u0439至产生 u0442 u00a0 u0433 u043e u0432 u0430 u00a0安装, u043e u0442 u043b u0438 u0447 u0430 u044e u0449的垂直力的中心 u0438 u0439 u0441 u00a0顺序 u043f u0440 u043e u0438 u0437 u0432 u043e u0434 u00a0 u0442对地面每天一次的短期短期影响,至少有一个固定的 u0442 u00a0在安装 u043f u0435 u0440 u043f u0435 u043d u0434 u0438 u043a u0443 u043b u00a0 u0440 u043a u0443 u043b u00a0 u0440 u043d u043e u0441 u0442 u0438飞机穿过地球的地理极点 u043f u0440 u043e u0445 u043e u0434 u00a0 u0449 u0435 u0439位于 u0432 u0435 u0440 u0442 u0438 u043a u0430 u043b u044c u043d u0430 u00a0电源 u0432 u043e u0437 u0434 u0435 u0439 u0441 u0442 u0432 u0438 u00a0,到地球轨道p u043b u043e u0441 u043a u043e u0441 u0442 u0438,其中位于 u0432 u0440 u0430 u0449 u0435 u043d u0438 u00a0位于北半球午夜之前和南半球位于 u0430 u0441 u0442 u0440 u043e u043d u043e u043c u043c u0438 u0447 u0435 u0441 u043a u043e u043e u043c u0443 u043f u043e u043e u043b u0434 u043d u0040尘世的1/4的时间; 2。 u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0 1的方法,这样每天对地球表面的影响短暂一次 u043e u0441 u0441 u0443 u0449 u0435 u0441 u0442 u0432 u043b u00a0 u044e u0442在不超过2分钟的时间内; 3。 u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0 1的方法,这样每天对地球表面的影响短暂一次 u043e u0441 u0441 u0443 u0449 u0435 u0441 u0442 u0432 u043b u00a0 u044e u0442提前 u0432 u043a u043b u044e u0447 u0435 u043d u0438将 u00a0设计为 u0432 u043a u043a u043b 的长度1 u044e u0447 u0435 u043d u0438 u00a0。

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