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NASA · USA
Tiltrotor
NASA Tiltrotor
倾转旋翼 · 概念设计 · 核查 2026-10-01
飞行构型与公司名称
倾转旋翼
Aircraft type: Passenger eVTOL tilt-rotor concept design aircraft
核对构型依据 ↗原始目录分组:矢量推力
中文名称:待核实 · 原名:NASA
下列为 VFS 目录披露的参数,包含设计目标及历史版本信息。目录阶段不等于适航或量产状态;不同任务条件的航程与载荷不能直接当作同一条件下的性能。
资料覆盖与状态依据
可用性能指标 0/3 · 概念设计 · 目录依据 · 目录阶段,尚未核实批准状态
查看状态依据 ↗概念参数,尚不代表已实现性能
订阅本机型报道 RSS →主要参数
- 座位/载员
- 6 passengers
- 乘客
- 未公开/未录入
- 驾驶方式
- Unknown, possibly piloted or autonomous
- 航程(按来源口径)
- 未公开/未录入
- 巡航速度
- 未公开/未录入
- 最大速度
- 未公开/未录入
- 最大起飞重量
- 未公开/未录入
- 载荷
- 未公开/未录入
- 空重
- 未公开/未录入
- 长度
- 未公开/未录入
- 翼展
- 未公开/未录入
- 高度
- 未公开/未录入
- 动力来源
- All batteries or a hybrid-electric power source
- 电机
- 2 (or possibly 4) electric motors (more electric motors increase the redundancy of the aircraft)
- 旋翼/螺旋桨
- 2 main rotorblades (6 blades are on each main rotorblade)
- 续航时间
- 未公开/未录入
- 飞行高度
- 10,000 ft (3,048 m)
- 安全设计
- Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL tilt-rotor concept design aircraft
- Piloting
- Unknown, possibly piloted or autonomous
- Capacity
- 6 passengers
- Cruise speed for best endurance, estimated
- 149 mph (240 km/h) using a turbine engine power source
- Cruise speed for best endurance, estimated
- 137 mph (221 km/h) using a battery powered power source
- Cruise speed for best range, estimated
- 196 mph (315 km/h) using a turbine engine power source
- Cruise speed for best range, estimated
- 192 mph (309 km/h) using a battery powered power source
- Maximum speed, estimated
- 235 mph (378 km/h) using a turbine engine power source
- Maximum speed, estimated
- 245 mph (394 km/h) using a battery powered power source
- Reserve cruise power
- 20 minutes
- Cruise altitude
- 10,000 ft (3,048 m)
- Empty weight, estimated
- 3,100 lb (1,406 kg) using a turbine engine power source. 5,853 lb (2,655 kg) using a battery powered power source.
- Maximum payload weight, estimated
- 1,200 lb (544 kg)
- Maximum takeoff weight, estimated
- 4,300 lb (1,950 kg) using a turbine engine power source. 7,053 lb (3,199 kg) using a battery powered power source)
- Propellers
- 2 main rotorblades (6 blades are on each main rotorblade)
- Electric motors
- 2 (or possibly 4) electric motors (more electric motors increase the redundancy of the aircraft)
- Power source
- All batteries or a hybrid-electric power source
- Fuselage
- Carbon fiber composite
- Windows
- Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above
- Wings
- 1 main high wing
- Tail
- 1 V tail
- Landing gear
- Retractable tricycle wheeled (bogies - each landing gear has two wheels) landing gear
- Safety features
- Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.
明确提及本机型的报道
暂无明确匹配的公开报道;通用或重名型号不会自动关联。
目录参数变化记录
从保存的目录刷新快照比较,资料修改不等于实机性能发生变化。
暂无已保存的版本变化,后续目录刷新将保留快照。