Aircraft electrical network for electrically powered propulsorsCitation formats

Standard

Aircraft electrical network for electrically powered propulsors. / Apsley, Judith (Inventor); Smith, Alexander C. (Inventor); Manolopoulos, Charalampos (Inventor); Edwards, Huw (Inventor).

IPC No.: B64D 27/24 (2006.01). Patent No.: GB2539547.

Research output: Patent

Harvard

Apsley, J, Smith, AC, Manolopoulos, C & Edwards, H 2017, Aircraft electrical network for electrically powered propulsors, Patent No. GB2539547, IPC No. B64D 27/24 (2006.01).

APA

Apsley, J., Smith, A. C., Manolopoulos, C., & Edwards, H. (2017). IPC No. B64D 27/24 (2006.01). Aircraft electrical network for electrically powered propulsors. (Patent No. GB2539547).

Vancouver

Apsley J, Smith AC, Manolopoulos C, Edwards H, inventors. Aircraft electrical network for electrically powered propulsors. B64D 27/24 (2006.01). 2017 Jun 14.

Author

Apsley, Judith (Inventor) ; Smith, Alexander C. (Inventor) ; Manolopoulos, Charalampos (Inventor) ; Edwards, Huw (Inventor). / Aircraft electrical network for electrically powered propulsors. IPC No.: B64D 27/24 (2006.01). Patent No.: GB2539547.

Bibtex

@misc{aacb24d818a2468b8e3d1f6e7b552d79,
title = "Aircraft electrical network for electrically powered propulsors",
abstract = "An electrical network for an aircraft. The aircraft includes at least one variable pitch propulsor. The electrical network includes a wound field synchronous AC electrical generator having a wound rotor driven by an internal combustion engine. The network further includes a voltage regulator configured to regulate output voltage of the electrical generator by regulating rotor winding magnetic field strength, and a synchronous AC drive motor coupled to a respective variable pitch propulsor and provided with power from the output of the electrical generator.",
author = "Judith Apsley and Smith, {Alexander C.} and Charalampos Manolopoulos and Huw Edwards",
year = "2017",
month = "6",
day = "14",
language = "English",
type = "Patent",
note = "GB2539547; B64D 27/24 (2006.01)",

}

RIS

TY - PAT

T1 - Aircraft electrical network for electrically powered propulsors

AU - Apsley, Judith

AU - Smith, Alexander C.

AU - Manolopoulos, Charalampos

AU - Edwards, Huw

PY - 2017/6/14

Y1 - 2017/6/14

N2 - An electrical network for an aircraft. The aircraft includes at least one variable pitch propulsor. The electrical network includes a wound field synchronous AC electrical generator having a wound rotor driven by an internal combustion engine. The network further includes a voltage regulator configured to regulate output voltage of the electrical generator by regulating rotor winding magnetic field strength, and a synchronous AC drive motor coupled to a respective variable pitch propulsor and provided with power from the output of the electrical generator.

AB - An electrical network for an aircraft. The aircraft includes at least one variable pitch propulsor. The electrical network includes a wound field synchronous AC electrical generator having a wound rotor driven by an internal combustion engine. The network further includes a voltage regulator configured to regulate output voltage of the electrical generator by regulating rotor winding magnetic field strength, and a synchronous AC drive motor coupled to a respective variable pitch propulsor and provided with power from the output of the electrical generator.

M3 - Patent

M1 - GB2539547

ER -