NASA · 美国

Tiltwing

NASA Tiltwing

倾转机翼 · 概念设计 · 核查 2026-10-02

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飞行构型与公司名称

倾转机翼

Aircraft type: Passenger eVTOL tilt-wing 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

每项参数附独立出处。厂商声明、目录转述与监管使用限制分别标明；设计目标和历史版本不等于当前实测性能。不同任务条件的航程与载荷请查看引用原文。

资料覆盖与状态依据

可用性能指标 3/3 · 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 ↗

商载含设计目标／上限条件

概念参数，尚不代表已实现性能

订阅本机型报道 RSS →

主要参数与逐项引用

座位／载员: 6 passengers[1] 来源 ↗
目录转述
依据与条件
参数规格；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Capacity: 6 passengers
乘客: 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
驾驶方式: Unknown, possibly piloted or autonomous[1] 来源 ↗
目录转述
依据与条件
参数规格；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Piloting: Unknown, possibly piloted or autonomous
航程（按来源口径）: 86 m (138 km)[1] 来源 ↗
目录转述
依据与条件
参数规格；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Range: 86 m (138 km)
巡航速度: 178 mph (286 km/h)[1] 来源 ↗
目录转述
依据与条件
参数规格；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Cruise speed: 178 mph (286 km/h)
最大速度: 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
最大起飞重量: 6,000 lb (2,722 kg). These weights are estimates and the maximum takeoff weight could be between 6,000-6,750 lb (2,722-3,062 kg) or more. The actual weights, empty weight, payload weight and maximum takeoff would be known once an aircraft was manufactured.[1] 来源 ↗
目录转述 · 设计目标／声明参数
依据与条件
参数规格；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Maximum takeoff weight, estimated: 6,000 lb (2,722 kg). These weights are estimates and the maximum takeoff weight could be between 6,000-6,750 lb (2,722-3,062 kg) or more. The actual weights, empty weight, payload weight and maximum takeoff would be known once an aircraft was manufactured.
载荷: 1,200 lb (544 kg)[1] 来源 ↗
目录转述 · 设计目标／声明参数
依据与条件
参数规格；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Maximum payload weight, estimated: 1,200 lb (544 kg)
空重: 4,800 lb (2,178 kg)[1] 来源 ↗
目录转述 · 设计目标／声明参数
依据与条件
参数规格；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Empty weight, estimated: 4,800 lb (2,178 kg)
长度: 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
翼展: 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
宽度: 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
高度: 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
动力来源: All batteries or a hybrid-electric power source[1] 来源 ↗
目录转述
依据与条件
参数规格；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Power source: All batteries or a hybrid-electric power source
电机: 8 electric motors[1] 来源 ↗
目录转述
依据与条件
参数规格；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Electric motors: 8 electric motors
旋翼／螺旋桨: 8 propellers (6 stationary propellers and 2 tilt-propellers)[1] 来源 ↗
目录转述
依据与条件
参数规格；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Propellers: 8 propellers (6 stationary propellers and 2 tilt-propellers)
续航时间: 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
飞行高度: 10,000 ft (3,048 m)[1] 来源 ↗
目录转述
依据与条件
参数规格；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Cruise altitude: 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. If the aircraft is attempting to land and the tilt-wing does not move to its vertical position, the aircraft can land on a runway, road or field as a conventional airplane. If the aircraft is at rest and emergency flight must take place and the tilt-wing is not moving to the vertical, the aircraft can takeoff conventionally on a runway or a road.[1] 来源 ↗
目录转述
依据与条件
参数规格；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
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. If the aircraft is attempting to land and the tilt-wing does not move to its vertical position, the aircraft can land on a runway, road or field as a conventional airplane. If the aircraft is at rest and emergency flight must take place and the tilt-wing is not moving to the vertical, the aircraft can takeoff conventionally on a runway or a road.
电池容量: 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
充电时间: 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
货舱容积: 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
噪声: 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
旋翼直径: 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。

全部原始参数

参数规格

飞行器类型: Passenger eVTOL tilt-wing concept design aircraft[1] 来源 ↗
驾驶方式: Unknown, possibly piloted or autonomous[1] 来源 ↗
座位／载员: 6 passengers[1] 来源 ↗
巡航速度: 178 mph (286 km/h)[1] 来源 ↗
航程: 86 m (138 km)[1] 来源 ↗
备用巡航功率: 19 minutes[1] 来源 ↗
巡航高度: 10,000 ft (3,048 m)[1] 来源 ↗
空机重量，估算: 4,800 lb (2,178 kg)[1] 来源 ↗
最大载重重量，估计: 1,200 lb (544 kg)[1] 来源 ↗
最大起飞重量，估算: 6,000 lb (2,722 kg). These weights are estimates and the maximum takeoff weight could be between 6,000-6,750 lb (2,722-3,062 kg) or more. The actual weights, empty weight, payload weight and maximum takeoff would be known once an aircraft was manufactured.[1] 来源 ↗
螺旋桨: 8 propellers (6 stationary propellers and 2 tilt-propellers)[1] 来源 ↗
电机: 8 electric motors[1] 来源 ↗
动力来源: All batteries or a hybrid-electric power source[1] 来源 ↗
机身: Carbon fiber composite[1] 来源 ↗
舷窗: Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above[1] 来源 ↗
机翼: 1 main high swept tilt-wing[1] 来源 ↗
尾翼: 1 T-tail[1] 来源 ↗
起落架: Retractable tricycle wheeled landing gear[1] 来源 ↗
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. If the aircraft is attempting to land and the tilt-wing does not move to its vertical position, the aircraft can land on a runway, road or field as a conventional airplane. If the aircraft is at rest and emergency flight must take place and the tilt-wing is not moving to the vertical, the aircraft can takeoff conventionally on a runway or a road.[1] 来源 ↗

补充检索来源

已检索 2026-10-02。下列为候选资料，尚未全部核实；参数依据请查看逐项引用，目录转述不等于厂商独立复核。

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。