DataSheet26.com

NAS1101 PDF даташит

Спецификация NAS1101 изготовлена ​​​​«AIA» и имеет функцию, называемую «Screw / FLAT FILLISTER HEAD».

Детали детали

Номер произв NAS1101
Описание Screw / FLAT FILLISTER HEAD
Производители AIA
логотип AIA логотип 

4 Pages
scroll

No Preview Available !

NAS1101 Даташит, Описание, Даташиты
*k*
Reproduced By IHS
With The Permission Of AWNAS
Under Royalty Agreement
NATIONAL AEROSPACE STAN DARD
e) COPYRIGHT 2013 AEROSPACE INDUSTRIES ASSOCIATION OF AMERIC& INC. ALL RIGHTS RESERVED
OFFSE:T CRUCIFORM RECESS
PER NASM14191 OR NASM337B1
(sEE CODE)
U
=4
eU
BREAK EDGE
,O10 MAX.
E
z
tsar
H9
q:N
uiz
>d!>vt;
fa,Y=p<
1,IIEAD MARKING 117/
@ COMPLETELY REVISED
35"*5" 2 PL
@K
2 HOLES
u<
SH
utF:FO
Eo
oE
>?
=Sx:
60
ad<z<I
Zgpiii
9q
4x.zo
t!s!tsr
=<iHr
:<UU
!oE
ap
96
=<
=<x;il6ot9as9>E29
Ed
DRTLLED HEAD (CODE H)
cRoss-DRTLLED HEAD (CODE D)
PART
NUMBER
NAS1101-00
NAS1101-01
NAS1101-02
NAS1101-04
NAS1101-06
NAS1101-08
NAS1101-3
NAS1101-4
NAS1101-5
NAS1101-6
THR[:AD QA @B
IL2U
MIN
.0600-80
UNJF:-3A
.096
.092
,082
.073U64
UN]C!3A
.118
.LL4
.104
.0860-s6
UNJC!34
.140
.136
.L26
.11 20-40
UNJC!3A
.183
.178
.168
.1380-3?
UNJC!34
.226
.22L
.2tr
.L64U32
UNJC!34
.270
.265
.255
,1900-32
UNJF:-3A
.JI.J
.306
.296
,2s00-28
UNJF'-34
.375
.?67
.357
.3L2!;24
UNJF'-34
.438
.429
.413
.375Ct-24
UNJF-3A
.563
.552
.536
(c)
.034
.044
.049
.056
.075
.094
.113
@D
MAX
.060
.073
.086
,It2
,138
.764
.190
.250
.3t2
.375
TABLE I _ DIMENSIONS
E H QK R T
RAD MAX
,03s
.030
.045
,03s
,050
,040
.060
.050
.080
.070
.090
.080
.100
.090
.037
.029
.045
.037
.053
.044
.069
,059
,086
.074
.r02
.OBB
.118
,103
.150
,133
.183
.162
.2t5
.191
lrsl
.042
.034
.042
.o34
.042
.034
,068
,060
.068
.060
.068
.060
,010
,00s
,010
,005
,010
,00s
,010
.00s
.010
.005
.020
.010
.020
,010
.020
,010
.020
.010
.02s
.015
,033
.039
,046
.059
.072
.0Bs
.098
.t2B
.134
.161
(u)
.010
.010
.010
.013
.016
.016
,016
.018
.02L
.021
@w
MAX
.087
.r04
.722
.L57
.193
.228
.263
.345
.382
.457
RECESS GAGE
PENETMTION /3/
MAX
MIN
.0250 .0170
.0300 .0215
.0350 .0260
.0450 .0350
.0555 .0450
,0660 .0545
.0760 .063s
.0990 .0850
,0985 .0825
.1 180 .1000
TENSILE
STRENGTH
MIN LBF /16/
2BB
420
591
966
1,450
2,240
3,180
5,820
9,200
14,000
PROCUREMENT
SPECIFICATION
NOTED
CUSTODIAN
NATIONAL AEROSPACE STANDARDS COMMITTEE
TITLE
scREw, MACHINE, FLAT FILLISTER HEAD,
FULL THREAD, OFFSET CRUCTFORM
@
REVISION
L2
CLASSIFICATION
PART STANDARD
NAS1101
5ntrtrt r uF a
USE OF OR RELIAI{CE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUAUFY SUPPUERS OR CERTIFY
CONFORMANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. AiA MAKES NO REPRESENTATiON OR CLAIM RESPECTING (1) THE SUITABiUTY OF
ITEMS FOR ANY P,qRTICULAR APPLICATION OR (2) THE EXISTENCE OF OR APPLICABiLITY THERETO OF PATENT OR TMDEMARKS RIGHTS.
m
N
j
t
z
uFl
6
zo.
th
U
d.
ho
uz:)
uF
o
U
ttt









No Preview Available !

NAS1101 Даташит, Описание, Даташиты
Js.e{
ttltlf* tt x tis P.'tc t:. tN tl ttNr
NATI.NAL AERosPAcE
'TANDARDo copyRIGHT 20t3 AERospAcE INDUSTRIEs AssocIATIoN oF AMERIca, rNc, ALL RIGHTs RESERVED
z-
d
du
E
6z
tr
U
q
llt _
EQ-zo>:<ii
H6<
*3H
9f<,=dp<p a
MATERIAL:
ALLOY STEEL: 4140 (UNS c41400) PER M+tii€€e6 AMS63B2, 4340 (UNS G43406) PER M+t #000
AMS6415 OR AMS64B4, OR 8740 (UNS G87400) PER +.4{]-s€e49 AMS6322,
CRES: A286 (UNS 566286) CONFORMING TO THE CHEMISTRY 0F AMS5731, AMS5732, AMS5737 OR
AM55853,
TITANIUM ALLOY: 6Al-4V (UNS R56400) PER AMS492B OR AMS4967,
HEAT TREATMENT:
DEVELOP BASIC MATERIAL PROPERTiES AS FOLLOWS, WITH CONTROLS PER AM5-F€875 AMS2759
FOR ALLOY STEEL AND CRES AND AMS-H-B12OO OR AMS2BOl FOR TITANIUM:
ALLOY STEEL: 160-180 KSI FTU.
CRES: 160-190 KSI FTU, /16/
TITANIUM (6Al-4V): 160 KSI FTU MIN,
FINISH:
IiLLOY STEEL: CADMIUM PLATE PER AMS-QQ-P-416, TYPE II, CLASS 2 (NO CODE) OR CADMIUM PLATE
pER AMS-QQ-p-416, TypE Ir, CLASS 2 WrTH DULL BLACK CHROMATE TREATMENT (B CODE),
CRES: CLEAN AND PASSIVATE IN ACCORDANCE WITH AMS2700, METHOD 1, TYPE 2 OR WPE 8,
CLASS 1 (NO CODE) OR CADMIUM PLATE PER AMS-QQ-P-416, TYPE II, CLASS 2 (P CODE),
'IITANIUM ALLOY: NONE (NO CODE) OR ALUMINUM COAT PER NAS4006 (A CODE) OR ALUMINUM
I€€D+ WcoAT PER MIL-DTL-B34BB, TYPE II, CLASS 3 (C CODE)
U<tn
*H:J
uF
FE
o:PL
>z
=$oad<xoz<-=
Zgiltr
:z'g6
g9
t2<u[Htr
<oEu
HH
;;@ui
aE<2t<zo^<
#9a
CODE:
"
F:IRST DASH NUMBER DESIGNATES DIAMETER AND THREAD.
s;EcoND DASH NUMBER TNDTCATES LENGTI-| IN .062s INCREMENTS (AS CONVERTED TO THREE
DECIMAL PLACES PER ASME Y14,5).
INTERMEDIATE OR LONGER LENGTHS MAY I3E SPECIFIED BY USE OF WHOLE DASH NUMBERS ONLY.
IJSE OF ,25 INCH INCREMENTS IS RECOMMENDED FOR SCREWS OVER 3 INCHES LONG,
'A" FOLLOWING LAST DASH NUMBER DESIGNATES ALUMiNUM COAT PER NAS4OO6.
''B" FOLLOWING LAST DASH NUMBER DESIGNATES CADMIUM PTATE WITH DULL BLACK CHROMATE
TREATMENT.
"C" FOLLOWING LAST DASH NUMBER DESIGNATES ALUMINUM COAT PER MIL'DTL-B34BB, TYPE II,
CLASS 3,
"D" IN LIEU OF SECOND DASH DESIGNATES CROSS-DRILLED HEAD.
"E" IN LIEU OF FIRST DASH DESIGNATES CRES.
"H" IN LIEU OF SECOND DASH DESIGNATES DRILLED HEAD.
*P" FOLLOWiNG LAST DASH NUMBER DESIGNATES CADMIUM PLATE PER
*V"
IN
AMS-QQ-P-416, TYPE II, CLASS 2,
LIEU OF FIRST DASH DESIGNATES TITAN]UM
ALLOY,
!'W" FELtEWING ' \ST DASH NUI4BET+DEsI€NATES TYPE I N' \T{N6. /14/
: @ corvnr-rrElY REVISED
d
REVISION
12
NASl101
USE OF OR RELIAN(:E UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUALIFY SUPPLIERS OR CERTIFY
CONFORMANCE OF ITEI,IS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATION OR CLAIN1 RESPE TING (1) THE SUITABILITY OF









No Preview Available !

NAS1101 Даташит, Описание, Даташиты
ffiocoPYRIGHT2o,,I:l,i:H,:*:T:::^*::,:J*}:R'T:*,"n,,REsERVED
ffifr
N,Aliorl/r[ ntfi oSracf iln.MD^!i5
z
-
:dg
6z
tr
ooao
UA
g:R
l>d1>=6f9;_z
a_z
aYa
u<6
oU<EUF
FFEO
=SooHx
ad<z<x
gZiltr
lc
zAtr6qz
<ir
]<U'Lu
OE
oU-i
d-
;;oui
x<<F9?ZE9
,^ o g.l
#9P,
F4g
EXAMPLE OF PAFIT NUMBER:
=NASl101-3-8 .1900-32 SCREW, ,500 LENGTH, ALLOY STEEL, NASM337B1 RECESS, TypE II
PLATING,
=NAS1101-5-108 ,3125-24 SCREW, ,625 LENGTH, ALLOY STEEL, CADMIUM pLATING WITH DULL
BLACK CHROMATE TREATMENT, NASM33781 RECESS,
NAS11O1E5-1OP
==NASl101V5-10
=NAS1101V5HR10
,3125-24 SCREW, ,625 LENGTH, CRES, NASM337B1 RECEsS, TYPE II PLAT]NG.
,3L25-24 SCREW/ ,625 LENGTH/ TITANIUM ALLOY, NASM337B1 RECESS,
,3L25-24 SCREW, ,625 LENGTH, TITANIUM ALLOY, DRILLED HEAD, NASM1419i
RECESS.
NOTES:
(1)
DIAMETER OF UNTHREADED PORTION OF SCREWS SHALL NOT BE LESS THAN MINIMUM PITCH
DIAMETER NOR MORE THAN MMIMUM MAJOR DIAMETER OF THREAD,
. (2) FOR SCREWS 2 INCHES LONG OR SHORTER, COMPLETE THREADS SHALL EXTEND TO W]TH]N 2
THREADS OF THE BEARING SURFACE OF THE HEAD. SCREWS OF LONGER LENGTH SHALL HAVE A
MINiMUM COMPLETE THREAD LENGTH OF i.750 INCHES,
l3l
(4)
(5)
(6)
(7)
RECESS GAGING iN AccoRDANCE wITH NASM33781 oR NASM1419i AS AppLrcABLE,
REMOVE ALL BURRS AND SHARP EDGES,
OFFSET CRUCIFORM SCREWS TO BE INSTALLED AND REMOVED WITH DRIVERS PER NASM33781 OR
NASM14191 AS APPLICABLE,
BEARING SURFACE SQUARENESS: WITHIN ,OO3 FIM oF SHANK DIA,
FOR CRES, MAGNETIC PERMEABILITY SHAI-L BE LESS THAN 2.0 (AIR = 1,0) FOR A FIELD STRENGTH
H = 200 OERSTEDS USING A MAGNETIC PERMEABILITY INDICAToR pER AbTM A342lA34zM.TEST
METHOD 3,
(B)
'
TENSiLE STRESS AREAS USED FOR CALCULATION OF ULTIMATE TENSILE STRENGTH VALUES ARE
BASED ON FED.STD-H28.
(9) FOR DESCRTPTION OF STATUS NOTES, SEE NAS3BO,
(10) DiMENSIONS IN INCHES AND APPLY AFTER FINISH UNLESS OTHERWISE SPEC]FIED.
(11) SURFACE ROUGHNESS ',@D,,UNDERSIDE OF HEAD AND SIDES AND ROOT OF THREADS, 32
MICROINCHES RA; ALL OTHER SURFACES, 125 MICROINCHES Ra PER ASME 846,1,
It2l THREADS rN ACCORDANCE W]TH AS8879,
(13) NASM14191 RECESS iS APPLICABLE TO SIZES 06 THRU 5 INCLUSIVE; NASM337B1 RECESS iS
APPLICABLE TO ALL SIZES.
/I4I TYPE I PLATING (''W" CODE) IS INACTIVE FOR NEW DESIGN.
/15/ FOR THE-DRILLED HEAD
"0K" IS .022 TO ,030,
(H
CODE),
"OK"
IS
,034
TO
,042.
FOR
THE
CROSS-DRILLED
HEAD
(D
CODE),
REVISION
@Ed coveLrrElY REVTsED
L2
NASl101
3
uCITsOEENMF0SOFRF0MORARNRACNEEYLIAOPIIIIT;CRIETTEICUMUPSOLANPRRTOAHDPIUSPCLDEICODACTUUIMNOEDNNETRORNOTAR,T)AIOTNHNYFANLFAAYTETIOSRNToFsAPNLA.FACEENRFOSSnTPAnANCADEpApRSI DTTS.AA.NBDAIIAIAIRTDYMAITSKHEEFNsQTNIfRofnERLYnEFPVRDOEALSTUFENNNITTTAARTYIo.NTAoo^IAnnEDcMOuIE^TSDNrNcnOTbTsIp.Q-UeU-TcAncLi.JIFGY
SUPPLIERS OR CERTIFY
(1) THE SUITABILIry oF
^o










Скачать PDF:

[ NAS1101.PDF Даташит ]

Номер в каталогеОписаниеПроизводители
NAS1101Screw / FLAT FILLISTER HEADAIA
AIA
NAS1102ScrewCoast Fabrication
Coast Fabrication
NAS1102-02ScrewCoast Fabrication
Coast Fabrication
NAS1102-04ScrewCoast Fabrication
Coast Fabrication

Номер в каталоге Описание Производители
TL431

100 мА, регулируемый прецизионный шунтирующий регулятор

Unisonic Technologies
Unisonic Technologies
IRF840

8 А, 500 В, N-канальный МОП-транзистор

Vishay
Vishay
LM317

Линейный стабилизатор напряжения, 1,5 А

STMicroelectronics
STMicroelectronics

DataSheet26.com    |    2020    |

  Контакты    |    Поиск