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[信息] HSP“太阳能皮肤”,量子时代飞机

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 楼主| 发表于 2017-5-26 21:28:45 | 显示全部楼层

量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机

 楼主| 发表于 2017-5-26 21:30:48 | 显示全部楼层
How is the HSP “Solar Skin”?
            • Engines
The HSP “Solar Skin” would be equipped with 8 oversize Hybrid Engines (HEPJE), capable to produce  a big amount of power thrust. A Superconducting Motor at High temperature as a principal engine, assisted by an Ultra High-Bypass section, that will “feed” 3 independent Plasma Chambers producing a “rocket push” in order to  obtain a powerful thrust. The Plasma Chamber will mix little amounts of Hydrogen Fuel via airplane’s tanks with “air” via Ultra High-Bypass, both components will be burned at very high temperature (Plasma) and expelled with a thrust like a “rocket”. The HEPJE Engine would have 3 electromagnetic rings and a subchassis made of a combination of ceramic, gold & titanium materials in order to keep in the core (Superconducting Motor) a stable temperature of function & isolate it from the high temperature of the Plasma Chambers.
On the maneuvers of Take-off & Landing, the front engine’s thrusts are redirected to down side of the plane in order to create a “Harrier Jump jet” that reduces significantly the track distance to do those operations. The HSP “Solar Skin” could be equipped with a system based of two Rocket Engines (Hydrogen fuel -LH2-)  in both sides of the plane, together with the Hybrid Engines, could redirect all the “front thrust”, in order to create a vertical “high thrust” to reduce to only approximately two hundred meters the distance to Take-off & Landing.
The HSP “Solar Skin”  would be equipped with a “Thrust vectoring system” located on the rear nozzles and under the plane. Part of those nozzles (top side) could move 45 degrees, redirecting the engine exhaust to down side of the plane and creating a high pressure inside Engine’s duct. Together with this vectoring system, the rear nozzle would  have a special duct on the bottom side that could redirect part of the engine exhaust at 90 degrees under the plane, in order to create a “Harrier jump jet”, it would be possible because the duct would act as a escape valve when the pressure exhaust would go up.
6 Duct Systems under the Airplane’ fuselage have the function to act like a V/STOL (Harrier Jump Jet ) system.
            • Fly Controls
The HSP “Solar Skin” supplies the rudder device (change yaw, side to side) by two adjustable airflow ducts, that redirect the pass of it in order to change the yaw. These ducts are part of the same CO2 harvest system.
The Wind Generator duct is also used to control the vortex flows generated on the rear part of the Airplane’ fuselage. This would have a “special angle”/diffuser  (top side) to redirect the forward air flow at high speed.
In the maneuver of approach to the airport, the HSP “Solar Skin” would fly in a “Gliding flight” with the engines in a “stand-by mode” and the wind generators working at 100%, generating big amounts of electric Energy and controlling the descent. The airplane could have a Glide Ratio (E) of approximately 17.3 (calculated by CFD software).

量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机


 楼主| 发表于 2017-5-26 21:31:30 | 显示全部楼层

量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机

 楼主| 发表于 2017-5-26 21:31:55 | 显示全部楼层

量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机

 楼主| 发表于 2017-5-26 21:32:20 | 显示全部楼层

量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机

 楼主| 发表于 2017-5-26 21:32:49 | 显示全部楼层

量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机

 楼主| 发表于 2017-5-26 21:51:51 | 显示全部楼层
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93d1c041611121.5900cc186693a.jpg
 楼主| 发表于 2017-5-26 21:54:25 | 显示全部楼层
How is the HSP “Solar Skin”?
            • Engines
The HSP “Solar Skin” would be equipped with 8 oversize Hybrid Engines (HEPJE), capable to produce  a big amount of power thrust. A Superconducting Motor at High temperature as a principal engine, assisted by an Ultra High-Bypass section, that will “feed” 3 independent Plasma Chambers producing a “rocket push” in order to  obtain a powerful thrust. The Plasma Chamber will mix little amounts of Hydrogen Fuel via airplane’s tanks with “air” via Ultra High-Bypass, both components will be burned at very high temperature (Plasma) and expelled with a thrust like a “rocket”. The HEPJE Engine would have 3 electromagnetic rings and a subchassis made of a combination of ceramic, gold & titanium materials in order to keep in the core (Superconducting Motor) a stable temperature of function & isolate it from the high temperature of the Plasma Chambers.
On the maneuvers of Take-off & Landing, the front engine’s thrusts are redirected to down side of the plane in order to create a “Harrier Jump jet” that reduces significantly the track distance to do those operations. The HSP “Solar Skin” could be equipped with a system based of two Rocket Engines (Hydrogen fuel -LH2-)  in both sides of the plane, together with the Hybrid Engines, could redirect all the “front thrust”, in order to create a vertical “high thrust” to reduce to only approximately two hundred meters the distance to Take-off & Landing.
The HSP “Solar Skin”  would be equipped with a “Thrust vectoring system” located on the rear nozzles and under the plane. Part of those nozzles (top side) could move 45 degrees, redirecting the engine exhaust to down side of the plane and creating a high pressure inside Engine’s duct. Together with this vectoring system, the rear nozzle would  have a special duct on the bottom side that could redirect part of the engine exhaust at 90 degrees under the plane, in order to create a “Harrier jump jet”, it would be possible because the duct would act as a escape valve when the pressure exhaust would go up.
6 Duct Systems under the Airplane’ fuselage have the function to act like a V/STOL (Harrier Jump Jet ) system.
            • Fly Controls
The HSP “Solar Skin” supplies the rudder device (change yaw, side to side) by two adjustable airflow ducts, that redirect the pass of it in order to change the yaw. These ducts are part of the same CO2 harvest system.
The Wind Generator duct is also used to control the vortex flows generated on the rear part of the Airplane’ fuselage. This would have a “special angle”/diffuser  (top side) to redirect the forward air flow at high speed.
In the maneuver of approach to the airport, the HSP “Solar Skin” would fly in a “Gliding flight” with the engines in a “stand-by mode” and the wind generators working at 100%, generating big amounts of electric Energy and controlling the descent. The airplane could have a Glide Ratio (E) of approximately 17.3 (calculated by CFD software).

量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机


 楼主| 发表于 2017-5-26 21:55:02 | 显示全部楼层

量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机

 楼主| 发表于 2017-5-26 21:55:23 | 显示全部楼层

量子时代飞机

量子时代飞机


量子时代飞机

量子时代飞机

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