Title:
GAS TURBINE ENGINE TERMINAL BLOCK
Document Type and Number:
WIPO Patent Application WO/2021/167002
Kind Code:
A1
Abstract:
This gas turbine engine terminal block is provided with: at least one layer of a conductor which, in a first direction, is overlapped by and in contact with a plurality of terminals of a plurality of electric wires of a plurality of electric components and an electric device; at least two layers of insulators which are stacked in such a way as to sandwich the plurality of terminals and the conductor in the first direction; a stopper which faces the insulator on one end side, positioned on one end side in the first direction among the at least two layers of insulators; and a spring which is disposed between the stopper and the insulator on the other end side, positioned on the other end side in the first direction among the at least two layers of insulator, and which presses the plurality of terminals against the conductor in the first direction.
Inventors:
ARAI ATSUNORI
SAKIMOTO TATEKI
HIROTA HAYATO
OKUWA TATSUYA
MAESATO HIKARU
SAKAMOTO SHO
SAKIMOTO TATEKI
HIROTA HAYATO
OKUWA TATSUYA
MAESATO HIKARU
SAKAMOTO SHO
Application Number:
PCT/JP2021/006117
Publication Date:
August 26, 2021
Filing Date:
February 18, 2021
Export Citation:
Assignee:
KAWASAKI HEAVY IND LTD (JP)
International Classes:
H02K5/22; H01R9/22
Domestic Patent References:
| WO2016203589A1 | 2016-12-22 |
Foreign References:
| JP2009004191A | 2009-01-08 | |||
| US20180254580A1 | 2018-09-06 | |||
| JP2003031280A | 2003-01-31 |
Other References:
See also references of EP 4109720A4
Attorney, Agent or Firm:
ARCO PATENT & TRADEMARK ATTORNEYS (JP)
Download PDF:
Previous Patent: FLANGE COOLING STRUCTURE FOR GAS TURBINE ENGINE
Next Patent: ASSEMBLY STRUCTURE FOR COMPRESSOR OF GAS TURBINE ENGINE
Next Patent: ASSEMBLY STRUCTURE FOR COMPRESSOR OF GAS TURBINE ENGINE