Patent ID: 11884407
Assignee: MINEBEA MITSUMI IN.
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 8:
9. A flight device comprising:
an aircraft body unit;
a thrust force generation section comprising a propeller and a motor configured to rotate the propeller;
a parachute;
a parachute accommodation section configured to accommodate the parachute;
at least one flying body including a flying main body section connected to the parachute, and
a gas generating device configured to generate gas;
an ejection section configured to hold the flying body and eject the held flying body;
a lead wire configured to ignite the gas generating device;
a flight control section configured to control the thrust force generation section;
an abnormality detection section configured to detect an abnormality during flying; and
a fall control section configured to cause the flying body to be ejected from the ejection section in response to detection of the abnormality,
wherein:
the thrust force generation section is connected to the aircraft body unit,
the thrust force generation section is configured to generate a thrust force,
the flying body main body section is engaged with the ejection section,
the gas generating device is disposed in an internal space defined by the ejection section and the flying body main body section, and
the lead wire is led out from the internal space in a different direction from an ejection direction of the flying body in a state with one end of the lead wire connected to the gas generating device.