FIELD: aircraft engineering.
SUBSTANCE: aircraft warning system includes a control unit with a master calculator, air speed sensors, alerting means, a vertical g-load sensor, an air speed signal divider, trailing edge flaps position sensors, an angle of attack sensor, roll and pitch angles sensors all connected in a certain manner.
EFFECT: improved safety of flights and simplification of training in piloting are provided.
9 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| STALLING WARNING SYSTEM | 2017 |
|
RU2653414C1 |
| SIDESLIP PREVENTION SYSTEM | 2020 |
|
RU2759370C1 |
| AERODYNAMIC SURFACE AND AIRFRAME OF AIRCRAFT | 2017 |
|
RU2667410C1 |
| FRAMEWORK | 2016 |
|
RU2646691C2 |
| WING WITH AERODYNAMIC CURTAIN | 2016 |
|
RU2646686C2 |
| FRAMEWORK | 2016 |
|
RU2645522C1 |
| ELECTRONIC ARTIFICIAL HORIZON | 2017 |
|
RU2664789C1 |
| AIRCRAFT CONTROL SYSTEM | 2016 |
|
RU2630567C1 |
| INTELLIGENT SYSTEM OF CREW SUPPORT | 2013 |
|
RU2541902C2 |
| SMART CREW SUPPORT SYSTEM | 2015 |
|
RU2598130C1 |
