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CONES, FRONT, PROPELLER HUB
- Aerospace Standard
- AS92B
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Rationale
THIS DOCUMENT HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE 5-YEAR REVIEW POLICY.
THE BEARING CONTACTS ON THE TAPER CONE SEAT SHALL BE EVENLY. DISTRIBUTED AND SHALL COVER NOT LESS THAN 75 PER CENT OF THE BEARING AREA WHEN CHECKED TO AN APPROVED GAGE BY MINUTE BLUING PRIOR TO SPLITTING CONE.
INSPECT DIMENSIONALLY PRIOR TO SPLITTING.
MAXIMUM TAPER ON "A" DIMENSION NOT TO EXCEED .0005 PER INCH OF LENGTH.
MATING HALVES OF EACH CONE TO BE PACKED IN A SEALED CONTAINER AND OPENED ONLY WHEN READY FOR USE.
BREAK SHARP EDGES .016 ± .010.
MATERIAL: AMS 6415 OR AMS 6448.
FINISH: CADMIUM PLATE AMS 2400-1 OR CHROME PLATE .0003-.0005 THICK AFTER SPLITTING.
HEAT TREATMENT: ROCKWELL C48-52.
CHROMIUM PLATED CONES TO BE DESIGNATED BY THE PREFIX "A" PLACED BEFORE THE DASH NUMBER. EXAMPLES OF PART NUMBERS:
Data Sets - Support Documents
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Unnamed Dataset 1 |
Issuing Committee
E-25 General Standards for Aerospace and Propulsion Systems
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.
Reference
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