FIELD: aircraft engineering.
SUBSTANCE: seat comprises guide frame (1), moving platform (2), vertical and horizontal dampers (3) and (4), respectively, fastening system and strut (7). Platform (2) consists of two expanding parts: shoulder and pelvis parts. Each of the latter comprises adjustable clamps (6). Said parts and height of strut (7) allows adjustment of the "sitting vertex height". Adjustments in the area of pelvis, shoulders and head are performed by arc-like displacement of clamps (6). Moving elements can be locked at preset position by ergonomic eccentric clamps. Axle of damper (3) is shifted towards the zone between head and shoulder. Damper (4) is arranged compactly inside frame (1) and composed, for example, as "male die - female die" type collapsible mechanism.
EFFECT: improved fitting, damping of overloads.
3 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| PROVISION OF OPERATING AND EMERGENT G-TOLERANCE IN SPACECRAFT | 2013 |
|
RU2527615C1 |
| MANNED SPACECRAFT | 2005 |
|
RU2310586C2 |
| HUMAN-OPERATOR DISTRIBUTED PROTECTION METHOD FROM SHOCK OVERLOADS | 2015 |
|
RU2620703C2 |
| MANNED SPACECRAFT | 2001 |
|
RU2220077C2 |
| TRAINING COMPLEX FOR TRAINING SPACECRAFT CREWS FOR ACTIONS AFTER MANNED CAPSULE LANDING ON HEAVING SEA | 2020 |
|
RU2734659C1 |
| DEVICE FOR DELIVERY OF TOURISTS FROM NEAR-MOON ORBIT TO SURFACE OF MOON AND SUBSEQUENT RETURN TO GROUND | 2019 |
|
RU2730700C1 |
| AIRCRAFT SAFETY SEAT | 2011 |
|
RU2500582C2 |
| REUSABLE SPACE TRANSPORTATION SYSTEM FOR ONE-WAY CARGO DELIVERY AND MASS DELIVERY OF TOURISTS FROM LONG ORBIT TO THE LUNAR SURFACE AND FOLLOWING RETURN TO EARTH | 2020 |
|
RU2744844C1 |
| VEHICLE MINEPROOF SEAT | 2011 |
|
RU2489669C1 |
| REUSABLE SPACE TRANSPORTATION SYSTEM FOR MASS DELIVERY FROM NEAR-EARTH ORBIT TO CIRCUMLUNAR ORBIT OF TOURISTS OR PAYLOADS AND SUBSEQUENT RETURN TO EARTH | 2019 |
|
RU2736657C1 |
