POWER GENERATING DEVICE FOR AIRCRAFT - KAWASAKI HEAVY IND LTD

Title:

POWER GENERATING DEVICE FOR AIRCRAFT

Document Type and Number:

WIPO Patent Application WO/2016/143331

Kind Code:

A1

Abstract:

A power generating device for aircraft is provided with: an input shaft by which the driving force of the engine is transmitted; a transmission that is arranged in parallel with the input shaft; a generator that is arranged in parallel with the input shaft and the transmission, and is driven by the output from the transmission; a power transmission mechanism that is arranged on one end side, in the axial direction, of the input shaft and transmits the output from the transmission to the generator; and a casing that has a mounting part on the one end side, in the axial direction, of the input shaft. The transmission has: an input unit to which is inputted the rotational driving force from the input shaft, said input unit being provided to the other end side, in the axial direction, of the input shaft; and an output unit that outputs the gear-shifted rotational driving force to the power transmission mechanism, said output unit being provided to the one end side, in the axial direction, of the input shaft. The power transmission mechanism has an internal space, into which the input shaft is inserted.

Inventors:

TANAKA KENICHIRO
IMAI HIDEYUKI
FUJII ISAO
GOI TATSUHIKO

Application Number:

PCT/JP2016/001257

Publication Date:

September 15, 2016

Filing Date:

March 08, 2016

Export Citation:

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Assignee:

KAWASAKI HEAVY IND LTD (JP)

International Classes:

B64D41/00; F01D15/10; F02C7/00; F02C7/32; F02C7/36; F16H1/06; F16H15/38; F16H57/023; H02K7/116; H02K7/18

Domestic Patent References:

WO2012137843A1

2012-10-11

Foreign References:

JPS645183B2	1989-01-30
US5201798A	1993-04-13
JP2001158400A	2001-06-12

Other References: