Flyg- och rymdteknik
- +Ämnesområden
- +Flyg- och rymdteknik (10)
- Flygplan och rymdfarkoster: allmänt (0)
- +Flyg- och rymdteknik. Material (3)
- +Flyg- och rymdteknik. Fästelement (5)
- Flyg- och rymdteknik. Komponenter (0)
- Flyg- och rymdteknik. Material. Komponenter. Processer (0)
- Konstruktioner och konstruktionselement (0)
- Flyg- och rymdteknik. Motorer och framdrivningssystem (0)
- Flyg- och rymdteknik. Elektrisk utrustning och elektriska system (2)
- Flyg- och rymdteknik. Hydraulsystem och komponenter (0)
- Instrumentering och navigationsutrustning (0)
- Utrustning för flygpassagerare och kabinutrustning (0)
- Marktjänst- och underhållsutrustningar (0)
- Lastanordningar (0)
- System för rymdkommunikation (0)
This document specifies the general characteristics, the conditions for qualification, acceptance and quality assurance, as well as the test programs and groups for threaded ring coupling circular connectors, fire resistant, intended for use in a temperature range from −65 °C to 175 °C continuous or 200 °C continuous according to the classes.
This document specifies the characteristics of screws, pan head, offset cruciform recess, close tolerance normal shank, short thread, in alloy steel, cadmium plated. Classification: 1 100 MPa1/235 °C2.
This document provides a list of removable crimped contacts as specified in the product standards, with wrapped or soldered connections, etc. for use in connectors or other electrical elements of connection. It shows the elements of connection in which they are used.
This document specifies the requirements relating to:
Steel 15CrMoV6 (1.7334)
Air melted
Hardened and tempered
Bars for machining
De ≤ 100 mm
1 080 MPa ≤ Rm ≤ 1 280 MPa
for aerospace applications.
W.nr: 1.7334.
ASD-STAN designation: FE-PL1505.
This document applies to constant-amplitude force-controlled low-cycle fatigue (LCF) testing of metallic materials governed by EN Aerospace standards. The document defines the mechanical properties that need to be determined, the equipment, test pieces, methodology of test and presentation of results.
The document applies to uniaxially loaded tests carried out on plain or notched test pieces under ambient and elevated temperatures. The document does not cover the testing of more complex test pieces, full scale components or structures, although the methodology could well be adopted to provide for such tests.
The purpose of this document is to ensure the comparability and reproducibility of the test results. The document does not cover the evaluation or interpretation of the results.
This document applies to uniaxial strain-controlled low cycle fatigue testing of metallic materials governed by EN aerospace standards. It defines the properties that need to be determined and the terms used in describing the tests and test pieces. It specifies the equipment, the test pieces, the method of testing and the presentation of results. It applies to testing at ambient and elevated temperatures. The purpose of this document is to ensure the comparability and reproducibility of the test results. It does not cover the evaluation or interpretation of the results. This document is restricted to the use of test pieces having a circular cross-section. In some particular cases the practice can be applied to flat test pieces. The major difficulties concern the preparation of the test pieces and their alignment in the grips.
This document specifies the characteristics of self-locking clip nuts in FE-PA2601 (A286) for aerospace applications. Classification: 1 100 MPa /425 °C
This document specifies the characteristics of self-locking silver coated clip nuts in FE PA92HT for aerospace applications. Classification: 1 100 MPa /425 °C
This document specifies the characteristics of screws, pan head, offset cruciform recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated. Classification: 1 100 MPa /235 °C
This document specifies the characteristics of screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated. Classification: 1 100 MPa /315 °C .