EN 2290-1-1998 pdf download.Aerospace series — Rod bodies, flight control in aluminium alloy, for adjustable end fittings — Part 1: Dimensions and loads.
This EN 2290-1 specifies the rharacierutws of flight control rod bodies for adjustable end fittings. They may be used within the temperature range
of—55CLo+ 120C.
2 Normative references
This F.urniwsn Standnrd incorporates by dated or undated reference. provisions from other publications. These normative references are cited at the appropriate places in the text and the publirat ions nrc listed hereafter. For dated reference.. subsequent amendment.. to or rcvision.i otany of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the lateiit edition of the publication referred to applies.
IS(.) 5855-2. Mros pace ainstructionii — .11.1 Thread — Part 2: Limit dimensions (or nuts and bolts.
EN 2257. Circular structural tubes in aluminium and aluminium alloys — Dimensions — Aems pace series1 .
EN 2289. .4ernspacr series — Rod bodies, flight controls, in aluminium alkw. Technical specification. EN 2290-2. Aerospace series — Rod bodies flight control in alum ins urn alloy for adjustable end fills nga. with .u.uged inserts Dimensions and londs.
EN 2435-01, Aerospace series — Prirnta and rarniahea — (‘orrmenn resistant chrnmated two component cold curing primer— Part 01: Minimum requirrmenla3.
EN 2434. Primer polvu ret hone cold curing typr.
EN 2437. Aerospace series — (‘hromate coswersion coatings yellow for aluminium and aluminium alloy..
EN 2510, Aluminium alloy 024T42 — Drawn tubes for structural applications Aerospace srriesH.
3 Required characteristics
3.1 (‘ontlguration — Dimensions — Tolerances
Sec Figure 1 and Table I and Table 2.
Dimensions and tolernnerm. in millimetres. apply after ebromate treatment but bemore. primer.
3.2 Surface rough ncs
External surfaces: K4 1.6 1am
Internal surfaces: k = 3,2 pm
The values apply before chromate treatment.
3.3 Loads
See Table 3.
3.4 Buckling strength
See Figure 2.
3.5 Masses
The maximum mass, in grammes. is determined by the following formula:
whcrr:
M is (he maximum mass of the rod body, in grammes:
M, as the maiia o(a cylindrical tubc of length L. duimcier I) and thickness a in grammes; see EN 2257:
k is the coeflicwnt of the increase in mass specific to each rod body, in grammes: see Table I.
3.6 Material
En 2510
3.7 Internal and external surface treatment
EN 2437 + EN 2435-01. code A
or
EN 2437+ EN 2436. code H.
No pnmer on threads.EN 2290-1-1998 pdf download.
EN 2290-1-1998 pdf download
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