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Ultrahigh-altitude aerospace tower and implementation method
The invention provides an ultrahigh altitude aerospace tower and an implementation method. The ultrahigh altitude aerospace tower comprises a tower body 1, inhaul cables 2, a tower top platform 3, a lifting system and a control system. Wherein the tower body 1 can be annularly arranged (figure 1) or radially arranged (figure 2), and the tower body 1 is composed of a hollow thin-wall tank 4, connecting discs 6 (figure 5 and figure 7) in different forms corresponding to the tower body 1, cables 5 and lifting systems 7 and 8; wherein the hollow thin-wall tank 4 is made of fiber reinforced resin, and reinforced fibers can be one or any combination of carbon fibers, aramid fibers and glass fibers; the hollow thin-wall tank 4 is provided with an inflation port and an exhaust port, and the air pressure in the hollow thin-wall tank 4 is controlled by a control system in real time; the gas in the cylinder can be hydrogen, helium or air; the rocket launcher can be used for launching rockets or aircrafts to replace first-level rockets, and management in the fields of flight launching, space tourism and air and space is achieved.
本发明提供一种超高海拔空天塔及实现方法,包括:塔身1、拉索2、塔顶平台3、提升系统、控制系统;其中塔身1组成型式可为环型布置(图1)或辐射形布置(图2),塔身1由空心薄壁罐4,与塔身1形式对应的不同形式的连接盘6(图5、图7),揽索5,提升系统7和8组成;其中空心薄壁罐4由纤维增强树脂制作而成,增强纤维可以是碳纤维、芳纶、玻璃纤维其中一种或其任意组合;空心薄壁罐4上设有充气口与排气口,空心薄壁罐4内气压由控制系统实时控制;筒内气体可为氢气、氦气或空气;本发明可用于火箭或飞行器的发射、代替一级火箭、发航、太空旅游、空天领域的管理。
Ultrahigh-altitude aerospace tower and implementation method
The invention provides an ultrahigh altitude aerospace tower and an implementation method. The ultrahigh altitude aerospace tower comprises a tower body 1, inhaul cables 2, a tower top platform 3, a lifting system and a control system. Wherein the tower body 1 can be annularly arranged (figure 1) or radially arranged (figure 2), and the tower body 1 is composed of a hollow thin-wall tank 4, connecting discs 6 (figure 5 and figure 7) in different forms corresponding to the tower body 1, cables 5 and lifting systems 7 and 8; wherein the hollow thin-wall tank 4 is made of fiber reinforced resin, and reinforced fibers can be one or any combination of carbon fibers, aramid fibers and glass fibers; the hollow thin-wall tank 4 is provided with an inflation port and an exhaust port, and the air pressure in the hollow thin-wall tank 4 is controlled by a control system in real time; the gas in the cylinder can be hydrogen, helium or air; the rocket launcher can be used for launching rockets or aircrafts to replace first-level rockets, and management in the fields of flight launching, space tourism and air and space is achieved.
本发明提供一种超高海拔空天塔及实现方法,包括:塔身1、拉索2、塔顶平台3、提升系统、控制系统;其中塔身1组成型式可为环型布置(图1)或辐射形布置(图2),塔身1由空心薄壁罐4,与塔身1形式对应的不同形式的连接盘6(图5、图7),揽索5,提升系统7和8组成;其中空心薄壁罐4由纤维增强树脂制作而成,增强纤维可以是碳纤维、芳纶、玻璃纤维其中一种或其任意组合;空心薄壁罐4上设有充气口与排气口,空心薄壁罐4内气压由控制系统实时控制;筒内气体可为氢气、氦气或空气;本发明可用于火箭或飞行器的发射、代替一级火箭、发航、太空旅游、空天领域的管理。
Ultrahigh-altitude aerospace tower and implementation method
一种超高海拔空天塔及实现方法
LIU ZIZHONG (Autor:in)
28.07.2023
Patent
Elektronische Ressource
Chinesisch
IPC:
F41B
WEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE
,
Waffen zum Verschießen von Geschossen ohne Verwendung von Explosiv- oder Treibladungen
/
B64F
GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT
,
Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen
/
B66B
Aufzüge
,
ELEVATORS
/
E04H
Gebäude oder ähnliche Bauwerke für besondere Zwecke
,
BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES
/
F41F
APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS
,
Vorrichtungen zum Abschießen von Geschossen oder Flugkörpern aus Rohren, z.B. Geschütze
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