Aerospace - Impulse Testing of Hydraulic Components
- Aerospace Standard
Technical changes have been made including adding a section on scatter factors and an appendix that is associated with this topic, and deleting the original Appendix A.
The references in the document have been updated.
Editorial changes have been made to improve the readability of the document.
|Aerospace Standard||Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For|
|Aerospace Standard||Hydraulic System Components, Aircraft and Missiles, General Specification For|
Data Sets - Support Documents
|Unnamed Dataset 1|
|TABLE A1||DETERMINATION OF FATIGUE TEST CYCLES TYPICAL AILERON ACTUATOR, 62 000 FLIGHTS - 1 LIFE|
|TABLE A2||AIRCRAFT MANUFACTURERS DATA FOR THE EXAMPLE CHOSEN|
|TABLE A3||G-A-G CYCLE FOR THE EXAMPLE CHOSEN|
|TABLE A4||STRESS/PRESSURE RATIO FOR THE EXAMPLE CHOSEN|
|TABLE A7||n/N, Σ n/N FOR EXAMPLE CHOSEN|
|TABLE B1||VARIATION OF SCATTER FACTOR WITH NUMBER OF COMPONENTS TESTED|
A-6 Aerospace Actuation, Control and Fluid Power Systems
The committee A-6 is a service organization to promote the advancement of actuation, control and fluid power in sciences, technologies, engineering practices, and standards associated with the design, manufacture, operation, and support of aerospace vehicles. The Committee A-6 is comprised of a parent committee, subcommittees, panels, and a Steering Council. The Steering Council may from time to time create or dissolve subcommittees and panels and amend their responsibilities. The current panels include A-6A1, A-6A2, A-6A3, A-6B1, A-6B2, A-6B3, A-6C1, A-6C2, A-6C3, A-6C4 and A-6C5. The Committee A-6 is the approval body for all documents developed by its subcommittees and panels.