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王金豹 2026年01月16日 08:01:35
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Vol. 1 14--00--1 REV 56, Jan 31/03 HYDRAULIC POWER Table of Contents Flight Crew Operating Manual CSP A--013 MASTER CHAPTER 14 -- HYDRAULIC POWER Page TABLE OF CONTENTS 14--00 Table of Contents 14--00--1 INTRODUCTION 14--10 Introduction 14--10--1 SYSTEMS 1 AND 2 14--20 Hydraulic Systems No.1 and No.2 14--20--1 Engine Driven Pumps 14--20--4 AC Motor Pumps (ACMP) 14--20--4 Hydraulic Shutoff Valves 14--20--5 Reservoir 14--20--5 Accumulator 14--20--5 System Circuit Breakers 14--20--8 SYSTEM 3 14--30 Hydraulic System No.3 14--30--1 AC Motor Pumps 14--30--3 System Circuit Breakers 14--30--6 LIST OF ILLUSTRATIONS INTRODUCTION Figure 14--10--1 Hydraulic Systems Diagram 14--10--2 Figure 14--10--2 Hydraulic Systems Overview 14--10--3 SYSTEMS 1 AND 2 Figure 14--20--1 Hydraulic Systems 1 and 2 Schematic 14--20--2 Figure 14--20--2 Hydraulic Control Panel 14--20--4 Figure 14--20--3 Systems 1 and 2 -- Synoptic Page 14--20--6 Figure 14--20--4 Systems 1 and 2 -- EICAS Indications 14--20--7 SYSTEM 3 Figure 14--30--1 Hydraulic System 3 -- Schematic 14--30--2 Figure 14--30--2 Hydraulic Control Panel 14--30--3 Figure 14--30--3 System 3 -- Synoptic Page 14--30--4 Figure 14--30--4 System 3 -- EICAS Indications 14--30--5 REV 56, Jan 31/03 Vol. 1 14--00--2 HYDRAULIC POWER Table of Contents Flight Crew Operating Manual MASTER CSP A--013 THIS PAGE INTENTIONALLY LEFT BLANK Vol. 1 14--10--1 REV 56, Jan 31/03 HYDRAULIC POWER Introduction Flight Crew Operating Manual CSP A--013 MASTER 1. INTRODUCTION Hydraulic power is provided by three independent systems designated No.1, No.2 and No.3. All systems operate at a nominal pressure of 3000 psi (20,685 kPa) and use synthetic hydraulic fluid “Skydrol”. WARNING Skydrol is highly corrosive and can produce severe skin and eye irritation. Systems 1 and 2 are serviced by ground service panels located in the aft equipment compartment. System 3 is serviced by a ground service panel located on the right side of the fuselage, aft of the wing root. Each system has two hydraulic pumps; a main pump (A) for normal power and a backup pump (B) for supplementary power. System No.1 and 2 main pumps are engine driven pumps (EDP’s). System 1 EDP (1A) is driven by the left engine and system 2 EDP (2A) is driven by the right engine. System 1 and 2 backup pumps (1B and 2B) are electrical AC motor pumps (ACMP’s). Both hydraulic pumps for system No.3 are ACMP’s. In system No.3, the main pump (3A) normally runs continuously, while the backup pump (3B) is available during periods of high flow requirements. The hydraulic systems supply power to operate the rudder, elevators, ailerons, spoilerons, flight spoilers, ground spoilers, wheel brakes, nosewheel steering and landing gear extension and retraction. The rudder, elevators and ailerons are powered by more than one hydraulic system to prevent loss of critical flight controls. During a total AC power failure in flight, pump 3B will be automatically powered by the air driven generator (ADG) when it is deployed. This will provide hydraulic pressure to the landing gear, brakes and nosewheel steering and also provides backup hydraulic pressure to the primary flight controls. REV 56, Jan 31/03 Vol. 1 14--10--2 HYDRAULIC POWER Introduction Flight Crew Operating Manual MASTER CSP A--013 Hydraulic Systems Diagram Figure 14---10---1 LEFT SPOILERON RUDDER LEFT AND RIGHT ELEVATORS NO. 1 SYSTEM AC MOTOR PUMP (1B) ENGINE DRIVEN PUMP (1A) LEFT AND RIGHT OUTBOARD GROUND SPOILERS LEFT AND RIGHT AILERON RUDDER LEFT AND RIGHT ELEVATORS LEFT AND RIGHT INBOARD BRAKES MAIN AND NOSE LANDING GEAR NOSEWHEEL STEERING RIGHT AILERON RUDDER LEFT AND RIGHT ELEVATORS LEFT AND RIGHT FLIGHT SPOILERS MLG DOWNLOCK ASSIST ACTUATORS LEFT AND RIGHT INBOARD GROUND SPOILERS LEFT AND RIGHT OUTBOARD BRAKES NO. 3 SYSTEM AC MOTOR PUMP (3B) NO. 2 SYSTEM AC MOTOR PUMP (2B) ENGINE DRIVEN PUMP (2A) AC MOTOR PUMP (3A) LEFT AILERON LEFT AND RIGHT FLIGHT SPOILERS LEFT AND RIGHT SPOILERONS RIGHT SPOILERON Vol. 1 14--10--3 REV 56, Jan 31/03 HYDRAULIC POWER Introduction Flight Crew Operating Manual CSP A--013   www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:Bombardier_CRJ_00-Hydraulic_Power

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