- 专利标题: Carriage for rocket launch system
-
申请号: US15627558申请日: 2017-06-20
-
公开(公告)号: US10443976B2公开(公告)日: 2019-10-15
- 发明人: Howard M. Chin , Kimberly A. Carraha
- 申请人: Howard M. Chin , Kimberly A. Carraha
- 代理机构: Walter | Haverfield LLP
- 代理商 D. Peter Hochberg; Sean F. Mellino
- 主分类号: B64G1/00
- IPC分类号: B64G1/00 ; F41F3/06 ; B64G6/00 ; F41F3/04 ; B64G1/64
摘要:
A carriage for use in a rocket launch system for cooperating with an electromotive cableway traction drives conveyed beneath a two axis pivot anchored to the earth, elevated into a co-axial transfer tube leading to three primary tether cables whose weight is offset by balloons. The carriage has traction drives which grip cables from which they derive power and rotate to drive the carriage from the low altitude to the high altitude. The traction drives rotate in the opposite direction as the carriage descends the cable following the launch of a rocket under gravitational force. The kinetic energy of the traction drive is converted to electrical energy which is fed back to the cables during descent of the carriage.
公开/授权文献
- US20170284768A1 CARRIAGE FOR ROCKET LAUNCH SYSTEM 公开/授权日:2017-10-05
信息查询