Hari Prasad · 意大利
Mobula
Prasad Mobula
倾转机翼 · 概念设计 · 核查 2026-10-02
飞行构型与公司名称
倾转机翼
Propellers: 18 electric ducted fans (EDFs), 6 EDFs located in the wings tilt for VTOL, forward flight and any other type of maneuvering. 10 EDFs are inside the wing for forward flight and are also used for maneuvering. 2 EDFs are in the front of the aircraft used for VTOL flight, forward flight and
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：Hari Prasad
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 2/3 · 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 ↗商载未纳入：单位或条件未能一致解析
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
- 5-7 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: 5-7 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
- 1 pilot (or AI piloting)[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: 1 pilot (or AI piloting)
- 航程（按来源口径）
- 280 km (174 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
Range: 280 km (174 m)
- 巡航速度
- 222-259 km/h (138-161 mph)[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: 222-259 km/h (138-161 mph)
- 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
- 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。
- 载荷
- Unknown[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
Maximum payload weight: Unknown
- 空重
- 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。
- 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
- 电池组[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
动力来源：电池组
核对原文
Power source: Batteries
- 电机
- 18 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: 18 electric motors
- 旋翼／螺旋桨
- 18 electric ducted fans (EDFs), 6 EDFs located in the wings tilt for VTOL, forward flight and any other type of maneuvering. 10 EDFs are inside the wing for forward flight and are also used for maneuvering. 2 EDFs are in the front of the aircraft used for VTOL flight, forward flight and for maneuvering.[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: 18 electric ducted fans (EDFs), 6 EDFs located in the wings tilt for VTOL, forward flight and any other type of maneuvering. 10 EDFs are inside the wing for forward flight and are also used for maneuvering. 2 EDFs are in the front of the aircraft used for VTOL flight, forward flight and for maneuvering.
- 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
- 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。
- 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. The aircraft has no moving wing surfaces when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.[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. The aircraft has no moving wing surfaces when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.
- 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 concept design aircraft[1] 来源 ↗
- 驾驶方式
- 1 pilot (or AI piloting)[1] 来源 ↗
- 座位／载员
- 5-7 passengers[1] 来源 ↗
- 巡航速度
- 222-259 km/h (138-161 mph)[1] 来源 ↗
- 航程
- 280 km (174 m)[1] 来源 ↗
- 最大载荷重量
- Unknown[1] 来源 ↗
- 螺旋桨
- 18 electric ducted fans (EDFs), 6 EDFs located in the wings tilt for VTOL, forward flight and any other type of maneuvering. 10 EDFs are inside the wing for forward flight and are also used for maneuvering. 2 EDFs are in the front of the aircraft used for VTOL flight, forward flight and for maneuvering.[1] 来源 ↗
- 电机
- 18 electric motors[1] 来源 ↗
- 动力来源
- 电池组[1] 来源 ↗
- 机身
- Carbon fiber composite[1] 来源 ↗
- 舷窗
- Larger than conventional windows and a sunroof over the passenger cabin[1] 来源 ↗
- 机翼
- 1 rear high main delta wing with winglets. The designer calls the rear main wing a manta ray wing.[1] 来源 ↗
- 腹鳍/鳍片
- 1 forward ventral fin (that doubles as the front landing gear strut) and 2 rear ventral strakes (that double as the rear landing gear struts)[1] 来源 ↗
- 起落架
- Fixed 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. The aircraft has no moving wing surfaces when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.[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。