IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0730474
(2000-12-06)
|
발명자
/ 주소 |
- Robert Raymond Boyd
- Dimitri David Thomas
|
출원인 / 주소 |
- Lockheed Martin Corporation
|
대리인 / 주소 |
Lockheed Martin Corporation
|
인용정보 |
피인용 횟수 :
8 인용 특허 :
6 |
초록
▼
A Space Elevator for transporting a payload from one point to another in outer space, includes a first structure, located at a first relatively fixed, non-zero orbital distance from the surface of the earth, for receiving payloads, a second structure, located at a second relatively fixed orbital dis
A Space Elevator for transporting a payload from one point to another in outer space, includes a first structure, located at a first relatively fixed, non-zero orbital distance from the surface of the earth, for receiving payloads, a second structure, located at a second relatively fixed orbital distance from the surface of the earth, for receiving payloads, where the second distance is greater than the first distance, a third structure located near the center of gravity of the combined apparatus providing a platform for storing and/or processing payloads, and a payload transporting apparatus disposed between and interconnecting the first and third and second and third structural means.
대표청구항
▼
1. A space elevator for transporting a payload from one point to another in outer space, comprising:a first structural means, located at a first substantially fixed orbital distance from the surface of the earth, for receiving payloads, a second structural means, located at a second substantially fi
1. A space elevator for transporting a payload from one point to another in outer space, comprising:a first structural means, located at a first substantially fixed orbital distance from the surface of the earth, for receiving payloads, a second structural means, located at a second substantially fixed orbital distance from the surface of the earth, for receiving payloads, said second distance being greater than said fist distance, no portion of said elevator is attached to the earth's surface, and payload-transporting means disposed between and interconnecting said first and said second structural means, said payload-transporting means includes cable means extending between said first and said second structural means, said cable means comprising lifting cables and load cables, wherein said lifting cables comprise a lower strength, less dense, material than said load cables, and a housing supported by said cable means for traveling along said cable means, said housing being capable of moving said payload between said first and said second structural means, said housing further includes a drive motor for propelling said housing along said lifting cables.
이 특허에 인용된 특허 (6)
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Hoyt Robert P. ; Forward Robert L., Alternate interconnection hoytether failure resistant multiline tether.
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Hoyt Robert P. ; Forward Robert L., Failure resistant multiline tether.
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Hoyt Robert P. ; Forward Robert L., Failure resistant multiline tether.
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Pearson David B. (Raritan NJ), Load measuring apparatus for an elevator car.
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Richter Utz,CHX ; Liebetrau Christoph,CHX, Modular construction for elevators.
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Hoyt Robert P. ; Forward Robert L., Planar hoytether failure resistant multiline tether.
이 특허를 인용한 특허 (8)
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Sainct, Herve Roland; Roser, Xavier; Martinot, Vincent, Method for lightening the weight of fuel stowed onboard during an interplanetary mission.
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Stone, William C.; Hogan, Bartholomew P., Non-line-of-sight optical power transfer system for launching a spacecraft into low earth orbit.
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Talent, David L.; Cheung, Ken C. K.; Nishimoto, Daron L., Phenomenological orbital debris impact risk assessment model and software.
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Chin, Howard M.; Carraha, Kimberly A., Rocket launch system and supporting apparatus.
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Im, Sunstar, Sky/space elevators.
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Dula, Arthur McKee, Space launch apparatus.
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Semiz, Muhamed, Structure with space applications and methods of construction thereof.
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Stone, William C., System for emergency crew return and down-mass from orbit.
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