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Pivotal · USA
BlackFly V2
Pivotal BlackFly V2
构型待核实 · 原型机 · 核查 2026-10-01
飞行构型与公司名称
构型待核实
VFS 原始目录分组:个人飞行器。尚无足够资料确定具体布局。
核对构型依据 ↗原始目录分组:个人飞行器 · 个人飞行器属于产品形态,构型另行识别。
中文名称:待核实 · 原名:Pivotal
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 · 原型机 · 目录依据 · 目录阶段,尚未核实批准状态
查看状态依据 ↗订阅本机型报道 RSS →主要参数
- 座位/载员
- 未公开/未录入
- 乘客
- 未公开/未录入
- 驾驶方式
- 1 pilot
- 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
- 510 lb (231.3 kg)
- 载荷
- 未公开/未录入
- 空重
- 310 lb (140.6 kg)
- 长度
- 13 ft, 5 in (4.08 m)
- 翼展
- 未公开/未录入
- 高度
- 5 ft (1.52 m)
- 动力来源
- Batteries
- 电机
- 8 electric motors
- 旋翼/螺旋桨
- 8 propellers
- 续航时间
- Unknown
- 飞行高度
- Unknown
- 安全设计
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. The aircraft has been made with a safety fault-tolerant design. There are also redundancies in the sub-systems and other parts of the aircraft. The aircraft has an emergency ballistic parachute.
全部原始参数
Specifications:
- Aircraft type
- eVTOL passenger prototype aircraft
- Piloting
- 1 pilot
- Maximum pilot height
- 6 ft, 2 in (1.88 m)
- First uncrewed flight
- February 11, 2016
- First crewed flight
- March 19, 2018
- Cruise Speed (USA)
- 62 mph (limited) (99.78 km/h)
- Cruise Speed (outside of USA)
- 80+ mph (128.75+ km/h)
- Range (with 25% reserve in USA)
- 20 miles (32.19 km)
- Flight time
- Unknown
- Cruise altitude
- Unknown
- Width
- 13 ft, 7 in (4.1 m)
- Length
- 13 ft, 5 in (4.08 m)
- Height
- 5 ft (1.52 m)
- Take off run
- 3 ft (0.91 m)
- Landing distance
- 3 ft (0.91 m)
- Maximum climb rate
- 1,000 fpm (5.08 m/s)
- Maximum descent rate
- 1,000 fpm (5.08 m/s)
- Temperature range for safe operations
- 32°F to 86°F (0°C to 30°C)
- Maximum wind speed for safe operations
- 25 mph (40.23 km/h)
- Empty weight
- 310 lb (140.6 kg)
- Maximum payload weight
- 200 lb (90.7 kg)
- Maximum takeoff weight
- 510 lb (231.3 kg)
- Propellers
- 8 propellers
- Electric motors
- 8 electric motors
- Power source
- Batteries
- Fuselage
- Epoxy-impregnated carbon fiber
- Window
- Canopy over cockpit
- Wings
- Fixed tandem wings
- Landing gear
- Lands on the belly of the aircraft. There are also four small fixed struts on the bottom end of each wing to protect the wings from hitting the ground on landing or during takeoff.
- Safety features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. The aircraft has been made with a safety fault-tolerant design. There are also redundancies in the sub-systems and other parts of the aircraft. The aircraft has an emergency ballistic parachute.
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。
公司资料与事件
包括公司融资及其他机型进展,请查看原文确认涉及的具体型号。
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