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CURRENT
2017-11-30
Standard
ARP826A
This document covers resolvers which are used to perform coordinate transformations as well as sine and cosine computations. It includes both the categories of compensated and uncompensated resolvers which perform these functions. Linear resolvers are also included because of their similarity to resolvers.
CURRENT
2017-11-30
Standard
AIR34B
The scope of this SAE Aerospace Information Report (AIR) is to present a guide for the determination of probable power output and the effect on the aircraft system that will be experienced when operating three-phase motors with one phase open. Unfortunately, the above subject cannot be resolved by specific rules. Modern aircraft or missile electrical systems are composed of a wide variety of electrical and electronic components. These components react differently under identical impetus due to the latitude of their design. This latidue of design must be allowed wherever possible to the accessory designer due to the various specification requirements. Therefore, it cannot be over-emphasized that the effect on the airplane or missile system, as well as motor operation, of three-phase motors on two-phase power must be thoroughly investigated.
CURRENT
2017-11-30
Standard
ARP497B
In order to ease the equipment design engineer's problem and at the same time provide a basis for more accurate comparable measurements between manufacturer and user, this recommended practice sets up "standard conditions" for design assurance testing and tabulated values which differ from previous publications by requiring the motor to be in a warmed-up condition which approximates its average use temperature. These conditions and the basic tests to which the tabulated characteristics refer are grouped in section 2.2 (Design Assurance) and compose a complete list of defining characteristics of the motor. This recommendation establishes objectives for high performance control motors to be used with aeronautical and associated equipment in protective enclosures or completely within the shell of the aircraft so that they are subjected only to the internal climate conditions of heat, cold, shock, vibration, altitude, and humidity.
CURRENT
2017-10-30
Standard
AS20708/16B
CURRENT
2017-10-30
Standard
AS20708/22B
CURRENT
2017-10-30
Standard
AS20708/17B
CURRENT
2017-10-30
Standard
AS20708/31B
CURRENT
2017-10-30
Standard
AS20708/39C
This specification covers the detail requirements for control transformer synchro, type 19CTB4b, 90 volt, 400 cycle.
CURRENT
2017-10-30
Standard
AS20708/7B
CURRENT
2017-10-30
Standard
AS20708/25B
This specification covers the detail requirements for control transformer synchro, type 16CTB4b, 90 volt, 400 cycle.
CURRENT
2017-08-09
Standard
AS20708/15B
2017-07-18
WIP Standard
ARP6505
This AIR intends to better document and tabulate electrical load dynamics that influence power source capacity, power quality and stabiltiy.
CURRENT
2017-05-25
Standard
AS20708/131B
CURRENT
2017-05-22
Standard
AS20708/139B
CURRENT
2017-05-22
Standard
AS20708/500B
CURRENT
2017-05-18
Standard
AS20708/81B
CURRENT
2017-05-18
Standard
AS20708/94C
This specification covers the detail requirements for 115 volt, 60 and 400 Hz, size 23 synchros (see 6.1).
CURRENT
2017-04-20
Standard
AS20708/70B
CURRENT
2017-04-20
Standard
AS20708/68B
CURRENT
2017-04-20
Standard
AS20708/78B
CURRENT
2017-04-20
Standard
AS20708/76B
CURRENT
2017-04-20
Standard
AS20708/62B
CURRENT
2017-04-19
Standard
AS20708/66B
CURRENT
2017-04-19
Standard
AS20708/79B
CURRENT
2017-04-19
Standard
AS20708/80B
CURRENT
2017-04-18
Standard
AS20708/74B
No Scope Available
CURRENT
2017-04-18
Standard
AS20708/67B
No Scope Available
CURRENT
2017-03-21
Standard
AS20708/46B
CURRENT
2017-03-21
Standard
AS20708/56B
CURRENT
2017-03-21
Standard
AS20708/55B
Viewing 1 to 30 of 185