FIELD: aeronautical engineering; hydraulic braking systems. SUBSTANCE: aircraft braking system includes two pressure-reducing valves; each valve is provided with control member; valve inlet is connected with hydraulic accumulator of hydraulic power supply source and its outlet is connected with respective hydraulic braking cylinder of LH or RH main undercarriage leg. Control device of braking system is made in form of handle with two hinged pushers located on both sides relative to its plane of symmetry. Each pusher is engageable with respective control member of pressure-reducing valve. EFFECT: enhanced efficiency. 4 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT LANDING GEAR WHEEL BRAKING SYSTEM | 1994 |
|
RU2102283C1 |
| HELICOPTER CHASSIS WHEEL BRAKING DEVICE | 2019 |
|
RU2710993C1 |
| HYDRAULIC SYSTEM | 1994 |
|
RU2092390C1 |
| APPARATUS FOR BRAKING THE WHEELS OF HELICOPTER LANDING GEAR | 2021 |
|
RU2777342C1 |
| HELICOPTER LANDING GEAR WHEEL BRAKING SYSTEM | 2023 |
|
RU2796557C1 |
| AIRCRAFT UNDERCARRIAGE WHEELS BRAKE SYSTEM | 2014 |
|
RU2554050C1 |
| AIRCRAFT HYDRAULIC SYSTEM | 1994 |
|
RU2092391C1 |
| AIRCRAFT HYDRAULIC SYSTEM | 2010 |
|
RU2455197C1 |
| CRANE CAR CHASSIS | 2018 |
|
RU2684838C1 |
| AIRCRAFT FRONT SUPPORT TURN CONTROL SYSTEM | 1994 |
|
RU2086472C1 |
