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GB/T 23419-2009 English PDF

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GB/T 23419-2009: Aircraft -- Four-wheel-drive tow tractors -- Performance requirements factors for design
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GB/T 23419-2009English234 Add to Cart 3 days [Need to translate] Aircraft -- Four-wheel-drive tow tractors -- Performance requirements factors for design Valid GB/T 23419-2009

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Basic data

Standard ID GB/T 23419-2009 (GB/T23419-2009)
Description (Translated English) Aircraft -- Four-wheel-drive tow tractors -- Performance requirements factors for design
Sector / Industry National Standard (Recommended)
Classification of Chinese Standard V57
Classification of International Standard 49.100
Word Count Estimation 12,151
Date of Issue 2009-03-23
Date of Implementation 2009-11-01
Adopted Standard ISO 7717-1985, IDT
Regulation (derived from) National Standard Approved Release Bulletin No. 4, 2009 (No. 144)
Issuing agency(ies) General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China, Standardization Administration of the People's Republic of China
Summary This standard specifies the design and evaluation needs to consider four-wheel driving tractor performance requirements of the various elements of the aircraft. It also provides design parameters tables and illustrative design case (see Appendix A). This standard does not detail the design specifications. Involves only performance requirements. This standard applies to all-wheel drive tractor aircraft design.

GB/T 23419-2009: Aircraft -- Four-wheel-drive tow tractors -- Performance requirements factors for design


---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
Aircraft. Four-wheel-drive tow tractors. Performance requirements factors for design ICS 49.100 Vp 57 National Standards of People's Republic of China GB/T 23419-2009/ISO 7717. 1985 Four-wheel drive tractor aircraft design performance requirements (ISO 7717. 1985, IDT) Posted 2009-03-23 2009-11-01 implementation Administration of Quality Supervision, Inspection and Quarantine of People's Republic of China Standardization Administration of China released

Foreword

This standard is equivalent to using ISO 7717. 1985 "Aircraft --- --- wheel drive tractor design performance requirements" (in English). This standard is equivalent translation ISO 7717. 1985. For ease of use, this standard made the following editorial changes. a) "this International Standard" be replaced by "this standard"; b) use a decimal point instead of a decimal comma ",". ","; c) Remove the preface to international standards; d) international standard "example 3.10" as an information appendix. Appendix A of this standard is an informative annex. The standard proposed by China Civil Aviation Administration. The standard by the China Civil Aviation Administration of Aviation Safety Technology Center. This standard was drafted. China CAAC Airport Department. The main drafters of this standard. high days. GB/T 23419-2009/ISO 7717. 1985 Four-wheel drive tractor aircraft design performance requirements

1 Scope

This standard specifies the design and evaluation of the four to be considered when the aircraft tractor driving performance requirements of the various elements. It also provides a set Count parameter tables and illustrative design case (see Appendix A). This standard did not elaborate design specifications relate only to performance requirements. This standard applies to four-wheel drive tractor aircraft design. Design Elements 2 In determining the aircraft tractor performance requirements, they should consider and evaluate these design elements. 2.1 Characteristics of Aircraft Parameters to be considered are as follows. a) size; b) the number of landing gear and wheels; c) traction connection point; d) total weight, empty weight and wheel weight distribution; Under e) following the direction of the initial motion, aircraft breakaway force as a percentage of the weight of the aircraft. 1) a straight line; 2) turning; f) under different road surface conditions uniform motion aircraft rolling resistance accounts for a percentage of the weight of the aircraft. 1) horizontal surface; 2) slope; g) aircraft turning radius; h) aircraft towing device angle limit; i) at the following load direction, aircraft towing strength of the device. 1) a straight line forward or backward; 2) minimum intensity direction; j) thrust engine idle condition. Airport Environment 2.2 Parameters to be considered are as follows. a) required by the maximum gradient; b) through the minimum speed runway and taxiways needed; c) aircraft parking requirements. 1) with terminal nose or parallel inward; 2) and other aircraft spacing; 3) distance to other fixed objects; 4) distant parking berthing needs; d) Ping Station, pavement strength and surface condition of taxiway, runway and taxiway of; e) of roads, bridges, interchanges, etc. by limiting; f) aircraft maintenance area, the parking area to the terminal, is expected to draw distance and freight routes between the floor; g) through the station site, the maximum approach angle taxiway, runway and taxiway and turn angle. GB/T 23419-2009/ISO 7717. 1985

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