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SAE AIR 1168/6 : 2011

Current

Current

The latest, up-to-date edition.

Aircraft Fuel Weight Penalty Due to Air Conditioning(STABILIZED Jul 2011)

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

25-07-2011

€187.36
Excluding VAT

SECTION 3H - CHARACTERISTICS OF EQUIPMENT COMPONENTS
1 INTRODUCTION
  1.1 Scope
  1.2 Nomenclature
2 PUMPS
  2.1 Nomenclature
  2.2 General Considerations
  2.3 Types of Pumps
  2.4 Fundamental Considerations
  2.5 Performance of Pumps
  2.6 Sizing Techniques
  2.7 Selection of Pump Type
  2.8 References
3 FANS
  3.1 Nomenclature
  3.2 General Considerations
  3.3 Types of Fans
  3.4 Fundamental Considerations
  3.5 Fan Performance
  3.6 Selection and Sizing of a Fan
  3.7 Fan Application
  3.8 References
4 COMPRESSORS
  4.1 Nomenclature
  4.2 General Considerations
  4.3 Types of compressors
  4.4 Fundamental Considerations
  4.5 Compressors Performance
  4.6 Dynamic Compressor Control Methods
  4.7 Application of Accessory Compressors in Flight
       Vehicles
  4.8 References
5 TURBINES
  5.1 Nomenclature
  5.2 General Considerations
  5.3 Turbine Types
  5.4 Turbine Fundamentals
  5.5 Performance Effects
  5.6 General Comparison of Axial and Radial Turbine Types
  5.7 Partial Admission
  5.8 Variable Nozzle
  5.9 Multistaging
  5.10 Generalized Turbine Performance Maps
  5.11 References
6 JET PUMPS
  6.1 Nomenclature
  6.2 General Considerations
  6.3 Jet Pump Theory
  6.4 Jet Pump Types
  6.5 Jet Pump Performance
  6.6 References
7 VALVES
  7.1 Nomenclature
  7.2 General Considerations
  7.3 Valves Types
  7.4 Valve Performance and Sizing
  7.5 Valve Actuation
  7.6 Valve Weights
  7.7 References
8 HEAT EXCHANGERS
  8.1 Nomenclature
  8.2 General Considerations
  8.3 Basic Relationships for Heat Exchanger Design
       Definition
  8.4 Types of Heat Exchangers and Their Operating
       Characteristics
  8.5 Heat Exchanger Pressure Losses
  8.6 Compact Airborne Heat Exchangers
  8.7 Heat Exchanger Design Procedure
  8.8 References
9 REFERENCES
SECTION 3J -EQUIPMENT COOLING SYSTEM DESIGN (AIRCRAFT,
            MISSILES)
1 INTRODUCTION
  1.1 Scope
  1.2 Nomenclature
2 DEFINITION OF THE VEHICLE AND ITS MISSION
  2.1 Vehicle Operational Envelope
  2.2 Ground Operations and Bench Checkout Requirements
  2.3 Moisture Content
  2.4 Ram Air Characteristics
  2.5 Bleed Air Characteristics
  2.6 Characteristics of Other Available Power Sources
  2.7 System Weight Penalty Factor Evaluation Techniques
3 DEFINITION OF THE EQUIPMENT COOLING PROBLEM
  3.1 Required Data
  3.2 Total Equipment Cooling Load
4 CHARACTERISTICS OF COOLING SYSTEM ELEMENTS
  4.1 Air Temperature Changes
5 REFERENCES
SECTION 3K - TEMPERATURE CONTROL SYSTEM DESIGN
1 INTRODUCTION
  1.1 Scope
  1.2 Nomenclature
2 TYPES OF TEMPERATURE CONTROL SYSTEMS
  2.1 General Considerations
  2.2 Types of Temperature Controls
  2.3 Temperature Control Classifications
3 SYSTEM COMPONENTS AND DESCRIPTIONS
  3.1 Temperature Sensors
  3.2 Controllers
  3.3 Valves
  3.4 Temperature Selectors and Pressure Transducers
4 DYNAMIC ANALYSIS
  4.1 General Considerations
  4.2 Mathematical Model
  4.3 Composition of the Mathematical Model
  4.4 Equipment Gain
  4.5 Effect of Heat Loads of Equipment Gain
  4.6 Compartment Gain
  4.7 Typical Personnel Compartment Analysis and Design
5 REFERENCE

This section relates the engineering fundamentals and thermophysical property material of the previous sections to the airborne equipment for which thermodynamic considerations apply.

Committee
AC-9
DocumentType
Standard
Pages
223
ProductNote
STABILIZED VERSION IS NOW AVAILABLE
PublisherName
SAE International
Status
Current

SAE AIR 5661A : 2017 COMPARTMENT DECOMPRESSION ANALYSIS
SAE ARP 89 : 2012 AIRCRAFT COMPARTMENT AUTOMATIC TEMPERATURE CONTROL SYSTEM

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