Title:
SIMULATOR FOR AIRCRACT
Document Type and Number:
WIPO Patent Application WO/2023/127957
Kind Code:
A1
Abstract:
A simulator (100) for aircrafts comprises: a control stick (10) turnable about an axial center (X1) in both directions; and a reaction force generation unit (20) having a tension spring (26) that is displaced by turning of the control stick (10) and that generates a steering reaction force for the control stick (10). The reaction force generation unit (20) further has: a transmission member (22) that is connected to the control stick (10) and turns together with the control stick (10); a first arm (23) that, upon turning of the control stick (10) in one direction and transmission of the turning through the transmission member (22), turns about an axial center (X2) and displaces the tension spring (26); and a second arm (24) that, upon turning of the control stick (10) in the other direction and transmission of the turning through the transmission member (22), turns about the axial center (X2) and displaces the tension spring (26).
Inventors:
MURATA YOSHIO
KOMATSU SEIJI
KURACHI OSAMU
NISHIMURA HIROFUMI
KOBAYASHI TAKUMI
YOSHITANI SHINICHI
SHIMIZU YUKI
KAWABE YUJI
OSAKI KOHEI
TAKADA KIYOSHIRO
KOMATSU SEIJI
KURACHI OSAMU
NISHIMURA HIROFUMI
KOBAYASHI TAKUMI
YOSHITANI SHINICHI
SHIMIZU YUKI
KAWABE YUJI
OSAKI KOHEI
TAKADA KIYOSHIRO
Application Number:
PCT/JP2022/048630
Publication Date:
July 06, 2023
Filing Date:
December 28, 2022
Export Citation:
Assignee:
KAWASAKI HEAVY IND LTD (JP)
International Classes:
G09B9/28; G05G5/03
Domestic Patent References:
| WO2021261596A1 | 2021-12-30 |
Foreign References:
| US5727188A | 1998-03-10 | |||
| JPH05265585A | 1993-10-15 | |||
| US20090189024A1 | 2009-07-30 | |||
| JP2002014736A | 2002-01-18 | |||
| US10724632B1 | 2020-07-28 | |||
| JP2011175630A | 2011-09-08 |
Attorney, Agent or Firm:
TERAZONO Kenichi et al. (JP)
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