Potrebujeme váš súhlas na využitie jednotlivých dát, aby sa vám okrem iného mohli ukazovať informácie týkajúce sa vašich záujmov. Súhlas udelíte kliknutím na tlačidlo „OK“.
AUXILIARY POWER SYSTEM CONSIDERATIONS FOR ADVANCED MILITARY AIRCRAFT
Automaticky preložený názov:
Pomocné napájanie Systémové požiadavky pre moderné vojenských lietadiel
NORMA vydaná dňa 1.6.1993
Označenie normy: SAE AIR1603
Dátum vydania normy: 1.6.1993
Kód tovaru: NS-477142
Krajina: Americká technická norma
Kategória: Technické normy SAE
This document provides a brief description of the auxiliary power equipment that is available with enough description and pertinent comments to enable an engineer to make logical preliminary selection of the appropriate equipment for advanced military aircraft programs. The information has been kept as brief as possible to include the maximum amount of equipment in a relatively short document. It is not intended to replace textbook design analysis or detailed information available from the equipment suppliers.
The document describes auxiliary power equipment. Auxiliary power is defined as follows: "Those elements of secondary power [defined as all aircraft nonpropulsive power generation and transmission] related to main engine bleed air and shaft power extraction or power generation separate from the main engines. Included are engine bleed air systems, remote engine driven gearboxes, engine starting systems, auxiliary power units, and emergency power systems." Additional definitions may be found in ARP906A which is the source of this definition.
Some closely related systems which are not discussed in detail, include thermal management, environmental control, electrical, and hydraulic systems.
SUBJECT TAXONOMY: Parts and Components, Ignition systems, Gas turbines, Hybrid engines, Hydraulic systems, Pneumatic systems, Auxiliary power units
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard
Posledná aktualizácia: 2024-08-01 (Počet položiek: 2 341 429)
© Copyright 2024 NORMSERVIS s.r.o.