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Pivotal · USA

BlackFly V1

Pivotal BlackFly V1

个人飞行器 · 原型机 · 核查 2026-10-01

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。

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
No 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
520 lb (231.3 kg)
载荷
200 lb (90.7 kg)
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
未公开/未录入
飞行高度
未公开/未录入
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. There are also redundancies in the sub-systems of the aircraft.

全部原始参数

Specifications:

Aircraft type
eVTOL prototype aircraft
Piloting
No pilot
First Flight
August 11, 2014
Maximum cruise Speed (USA)
62 mph (99.78 km/h)
Maximum cruise Speed (Outside USA)
100+ mph (160.93+ km/h)
Range (with 25% reserve in USA)
12+ miles (19.31+ km)
Takeoff run distance
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)
Width
13 ft ,7 in (4.1 m)
Length
13 ft, 5 in (4.08 m)
Height
5 ft (1.52 m)
Empty weight
310 lb (140.6 kg)
Maximum payload
200 lb (90.7 kg)
Maximum takeoff weight
520 lb (231.3 kg)
Propellers
8 propellers
Electric motors
8 electric motors
Power source
Batteries
Fuselage
Epoxy-impregnated carbon fiber
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. There are also redundancies in the sub-systems of the aircraft.