FIELD: machine building.
SUBSTANCE: longitudinal cargo fixing device (100) in aircraft, equipped with fixing unit (9), which is attached under aircraft floor, contains fixing latch (11) connected with load and connected with rod mechanism located inside fixing unit (9). Fixing latch (11) moves towards cargo ejection during flight. Rod mechanism is formed by fixing unit (9), acting as fixed rod, driven lever (12), pivotally connected to second hinge (2), and driven pusher (10) hingedly connected to first hinge (1). Both hinges (1, 2) are attached to fixing unit (9). Articulated joints displace rod mechanism to define locked, engaged and released positions for device (100). Driven lever (12) comprises curvilinear profile (121) on surface. Curved profile (121) interacts with driven roller (18) coupled with electromechanical linear drive (29) by drive rod (17). Safety trigger for lengthwise fixing device (100) is also described.
EFFECT: group of inventions is aimed at cargo release without risk of fixation.
27 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| VEHICLE WITH REPLACEABLE BODY FOR TRANSPORTATION OF AGRICULTURAL CARGOES | 2011 |
|
RU2479448C1 |
| HATCH COVER ASSEMBLY UNIT OF FLYING VEHICLE THERMOSTATING SYSTEM | 1999 |
|
RU2158215C1 |
| FLYING VEHICLE DOOR | 2005 |
|
RU2300483C1 |
| TROLLEY-BUS AUTOMATIC POLE RETRIEVER | 2001 |
|
RU2209143C1 |
| LANDING GEAR UP LOCAL | 1992 |
|
RU2076827C1 |
| EXOSKELETON COXOFEMORAL HINGE MODULE | 2023 |
|
RU2818620C1 |
| WORKING LOAD SEPARATION DEVICE | 2015 |
|
RU2648522C2 |
| LONGITUDINAL CONVEYER | 0 |
|
SU1447736A1 |
| CARGO GRIPPER | 0 |
|
SU1787924A1 |
| LONGITUDINAL CONVEYER | 0 |
|
SU1316954A1 |
