Search Results

Standard

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

2020-09-22

CURRENT

ARP4402A

This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.

Standard

Eddy Current Inspection of Circular Holes in Nonferrous Metallic Aircraft Engine Hardware

2019-10-14

CURRENT

AS4787A

This SAE Aerospace Standard (AS) establishes minimum requirements for eddy current inspection of circular holes in nonferrous, metallic, low conductivity (less than 5% IACS) aircraft engine hardware with fasteners removed.

Technical Paper

Ice Thickness and Particle Size from an Eddy Current Deicer

1994-02-01

940117

This paper details the icing wind tunnel test results of a new eddy current repulsion deicing system (EDS). There are only a trio of in-flight, anti-icing or deicing systems used on aircraft.

Technical Paper

Pulsed Eddy Current Inspections of Aircraft Structures in Support of Holistic Damage Tolerance

2003-09-08

2003-01-2916

Pulsed eddy current (PEC) inspection methods have been developed to address these needs, and this paper presents the results of a signal processing technique developed to characterize material loss in a two-layer structure from PEC data.

Standard

Determination of Aluminum Alloy Tempers Through Electrical Conductivity Measurement (Eddy Current)

2006-07-24

CURRENT

ARP891B

This recommended practice establishes a procedure for checking the tempers of aluminum alloys through eddy current conductivity measurements and defines criteria for acceptance or rejection.

Standard

Conductivity Standard - Eddy Current: Type of Aluminum Alloy Temper Testing Equipment

2002-12-16

CURRENT

AS915

Standard

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

2013-06-11

HISTORICAL

ARP4402

This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.

Standard

Determination of Aluminum Alloy Tempers Through Electrical Conductivity Measurement (Eddy Current)

2002-04-17

HISTORICAL

ARP891A

This recommended practice establishes a procedure for checking the tempers of aluminum alloys through eddy current conductivity measurements and defines criteria for acceptance or rejection.

Standard

DETERMINATION OF ALUMINUM ALLOY TEMPERS THROUGH ELECTRICAL CONDUCTIVITY MEASUREMENT (EDDY CURRENT)

1967-01-01

HISTORICAL

ARP891

This recommended practice establishes a procedure for checking the tempers of aluminum alloys through eddy current conductivity measurements and defines criteria for acceptance or rejection.

Standard

Eddy Current Inspection of Circular Holes in Nonferrous Metallic Aircraft Engine Hardware

2013-06-11

HISTORICAL

AS4787

This SAE Aerospace Standard (AS) establishes minimum requirements for eddy current inspection of circular holes in nonferrous, metallic, aircraft engine hardware with fasteners removed.

Technical Paper

Large Eddy Breakup Devices as Low Reynolds Number Airfoils

1986-10-01

861769

LEBU drag reduction is shown to be an extremely sensitive function of device micro-geometry at the low Reynolds numbers of all current investigations, and by analogy with conventional low-Reynolds number airfoil testing, the conclusion is drawn that the full potential for LEBU drag reduction must be explored at chord Reynolds numbers of 300,000 and above.

Event

Attend - Innovations in Mobility: Aerospace Digital Summit

2023-09-23

Innovations in Mobility: Aerospace Digital Summitaerospace mobility leaders convene leverage cutting-edge technology, design, develop safety measures, integrate current regulations, suggest future policies, expand markets, diversify revenue streams.

Event

Exhibit & Sponsor - Innovations in Mobility: Aerospace Digital Summit

2023-09-23

Innovations in Mobility: Aerospace Digital Summit aerospace mobility leaders convene leverage cutting-edge technology, design, develop safety measures, integrate current regulations, suggest future policies, expand markets, diversify revenue streams.

Event

Request Info - Exhibit & Sponsor - Innovations in Mobility: Aerospace Digital Summit

2023-09-23

Innovations in Mobility: Aerospace Digital Summit aerospace mobility leaders convene leverage cutting-edge technology, design, develop safety measures, integrate current regulations, suggest future policies, expand markets, diversify revenue streams.

Standard

Fuse, Current Limiter Type, Aircraft

2023-03-27

CURRENT

AS5372A

This specification covers the requirements for current limiter type fuses for use in aircraft primary electrical power systems conforming to MIL-STD-704.

Technical Paper

Detached Eddy Simulation on a Swept Hybrid Model in the IRT

2015-06-15

2015-01-2122

As they can be useful in robustly and accurately predicting large separation regions and capturing flow unsteadiness, a Detached Eddy Simulation (DES) approach has been adopted for simulating the flow over these large high-lift wing sections.

Technical Paper

Spacelab ECLS Current Status

1982-02-01

820884

This paper describes the major ECLS functions with particular respect to the current Flight Unit hardware status. It also includes recent design modifications, improvements, and adaptations resulting from Spacelab qualification and integration.

Technical Paper

Current Problems in Airline Engines

1935-01-01

350083

AN outline of some current problems in aircraft engines with particular reference to the types used for main-line scheduled-transport operations is presented, it being limited so far as possible to a consideration of the conventional four-stroke gasoline-engine.

Standard

Document for 270 Voltage Direct Current (270 V DC) System

2017-11-30

CURRENT

ARP4729A

This SAE Aerospace Recommended Practice (ARP) provides technical design and application information related to the generation, distribution, control, and utilization of aircraft 270 V DC electrical power systems and support equipment. This document also provides references and definitions to permit comparisons of various electrical systems and components.

Standard

TS341 Test for Electrical Connectors Contact Resistance at Rated Current

1987-10-01

CURRENT

TS341-1

This technical specification document describes tests that certain parts may be required to meet. For example, this tech spec applies to ESC30. To view suppliers qualified against this standard, visit https://ts200.sae-itc.org/.