FIELD: aircraft.
SUBSTANCE: invention relates to aircraft equipment and refers to the flight attendant's chair. Flight attendant's chair is attached to the floor of the aircraft and contains a rotatable backrest and a headrest, each of which contains fillers covered with covers. Seat bottom contains a removable filler and seat dampener with the possibility of absorbing vertical-lateral impact. Chair also contains a tethering system, two dampers with the possibility of energy absorption of the longitudinal-lateral impact.
EFFECT: increase in reliability in the emergency situation, simplification of the design and reduction of the mass-dimension parameters are achieved.
6 cl, 14 dwg
Title | Year | Author | Number |
---|---|---|---|
FLIGHT CREW SEAT (OPTIONS) | 2014 |
|
RU2620443C2 |
CREW SEAT WITH PARACHUTE PAN (VERSIONS) | 2014 |
|
RU2583102C2 |
OPERATOR'S SEATS EARTHQUAKE-PROOF (OPTIONS) | 2017 |
|
RU2668203C1 |
VEHICLE SEAT | 2020 |
|
RU2739092C1 |
ENERGY-ABSORBING HELICOPTER ARMCHAIR K-1 | 2016 |
|
RU2623859C1 |
VEHICLE SEAT WITH ROTARY SUPPORT MECHANISM | 2020 |
|
RU2752434C1 |
SPECIAL-PURPOSE ENERGY ABSORBING SEAT | 2018 |
|
RU2695947C1 |
AIRCRAFT SAFETY SEAT | 2011 |
|
RU2500582C2 |
METHOD OF REVERSIBLE ADAPTATION AND POWER ABSORPTION OF VEHICLE SEAT AND DEVICE FOR IMPLEMENTATION THEREOF | 2018 |
|
RU2699461C1 |
AIRCRAFT CATAPULT SYSTEM | 2013 |
|
RU2540133C1 |
Authors
Dates
2018-06-18—Published
2016-09-13—Filed