UNLIMITED FREE
ACCESS TO THE WORLD'S BEST IDEAS

SUBMIT
Already a GlobalSpec user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your GlobalSpec Experience

Select Your Free Newsletters

Industry Newsletters

Select Your Free Product Alerts

Finish!
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

NPFC - MIL-PRF-7115

CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR

inactive
Buy Now
Organization: NPFC
Publication Date: 11 July 2012
Status: inactive
Page Count: 51
scope:

This specification establishes the general requirements for converters that convert electrical power in aircraft from nominal 115/200 volts alternating current (AC), 400 Hertz (Hz), AC three-phase, aircraft electrical systems power to nominal 28 volt regulated and non-regulated direct current (DC) power.

intended Use:

The items described herein are intended for use on aircraft to convert three-phase, 115/200 volts, 400 Hz AC power to nominal 28 volt Regulated/Non-regulated DC power. Converters typically... View More

Document History

MIL-PRF-7115
May 19, 2020
Converters, Aircraft, General Specification for
A description is not available for this item.
MIL-PRF-7115
May 13, 2015
CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR
The items described herein are intended for use on aircraft to convert three-phase, 115/200 volts, 400 Hz AC power to nominal 28 volt Regulated/Non-regulated DC power. Converters typically are used...
MIL-PRF-7115
July 11, 2012
CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR
The items described herein are intended for use on aircraft to convert three-phase, 115/200 volts, 400 Hz AC power to nominal 28 volt Regulated/Non-regulated DC power. Converters typically are used...
MIL-C-7115
March 14, 1994
CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-C-7115F
September 18, 1992
CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR
This specification covers the general requirements for devices which convert from a nominal 115/200 Volt, 400 Hertz, 3-phase, alternating current (ac) (see 6.4.1) aircraft electrical system to...
MIL-C-7115
September 18, 1992
CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-C-7115E
July 8, 1983
CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-C-7115
July 8, 1983
CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-C-7115D SUPP 1
March 10, 1970
CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-C-7115
October 11, 1968
CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-C-7115B NOTICE 2
October 14, 1963
CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-C-7115C
September 25, 1962
CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
View Less
View All

References

This document references:
NASM14151 - WASHER, FLAT, ROUND, CORROSION RESISTING STEEL (FOR ELECTRICAL APPLICATIONS)
Published by AIA/NAS on July 31, 2012
A description is not available for this item.
This document references:
NASM35338 - WASHER, LOCK-SPRING, HELICAL, REGULAR (MEDIUM) SERIES
Published by AIA/NAS on December 19, 2014
A description is not available for this item.
This document references:
NASM35650 - NUT, PLAIN, HEXAGON, UNF-2B
Published by AIA/NAS on April 28, 2017
A description is not available for this item.
This document references:
NASM90415 - NUT, SELF-LOCKING, STEEL, 160 KSI, 450 °F, 12 POINT, CAPTIVE WASHER
Published by AIA/NAS on November 22, 2011
A description is not available for this item.
This document references:
JEDEC JESD 471 - Symbol and Label for Electrostatic Sensitive Devices
Published by JEDEC on February 1, 1980
Purpose It is the purpose of this Standard to provide a distinctive symbol and label to be used to identify those solid state device that require handling. The symbol or label should be used at the...
This document is referenced by:
AFGS-87219 - ELECTRICAL POWER SYSTEMS, AIRCRAFT
Published by NPFC on October 23, 2012
This specification establishes the performance requirements and verifications for electric power subsystems (EPS) for aerospace vehicles, including aircraft, helicopters, and missiles.
This document is referenced by:
DEF STAN 00-970: VOL 2: PT 0-3 - Design and Airworthiness Requirements for Service Aircraft Volume 2 - Rotorcraft Book 1 (Parts 0 to 3)
Published by MODUK on July 31, 1984
SCOPE OF REQUIREMENTS The Defence Standard includes within its scope, requirements and recommendations which arise from the operational function of Service Rotorcraft. It covers the following main...
View Less
View All
Advertisement