49.040.20 标准查询与下载



共找到 105 条与 相关的标准,共 7

이 규격은 항공기와 항공기 부속품 제조에 사용하는 저합금강으로 제작된 유니파이 볼트 및 스

Aerospace-Heat resistant low alloy bolts

ICS
49.040.20
CCS
V20
发布
2001-11-17
实施
2001-11-17

이 규격은 항공기 기체 및 부속품에 사용하는 저온용(120℃ 이하)의 셀프 로킹 너트(두꺼

Self-locking nuts for aircraft(thick)

ICS
49.040.20
CCS
V20
发布
2001-08-27
实施
2001-08-27

This standard defines self-aligning rod end ball bearing that used in the control system device of aircraft. Note 1. This specification covers rod end roller bearings with application in temperature ranges -55 ~ 149°c and intermittent maximum allowable temperature is 177°C. 2. Unit and dimension in parenthesis in this standard are that use through consultation as things by unit hitherto.

Self-aligning rod end roller bearing for aircraft

ICS
49.040.20
CCS
V42
发布
2000-11-24
实施
2000-11-24

This standard defines double-row rod end ball bearing that used in the control system device of aircraft. Note 1. This specification covers rod end ball bearings with application in temperature ranges -54~121 °C and -54°C to 149°C with 20% reduction of the predicted performance. 2. Unit and dimension in parenthesis in this standard are that use through consultation as things by unit hitherto.

Double-row rod end ball bearing for aircraft

ICS
49.040.20
CCS
V42
发布
2000-11-24
实施
2000-11-24

This specification covers the requirements for solid rivet of aircraft formed by aluminum, aluminum alloys and titanium columbium alloys.

Aircraft solid rivet identification standard

ICS
49.040.20
CCS
V04
发布
1999-12-18
实施
1999-12-18

이 규격은 알루미늄, 알루미늄합금 또는 티타늄ㆍ콜럼븀합금을 재료로 한 100。 접시 머리

100。 Countersunk solid rivet for aircraft

ICS
49.040.20
CCS
V20
发布
1999-12-18
实施
1999-12-18

이 규격은 알루미늄, 알루미늄합금 또는 티타늄-콜럼븀합금을 재료로 한 항공기용 솔리드 리벳

Aircraft solid rivet manufacturing standard

ICS
49.040.20
CCS
V20
发布
1999-12-18
实施
1999-12-18

이 규격은 알루미늄, 알루미늄합금 또는 티타늄ㆍ콜럼븀합금을 재료로 한 냄비 머리 솔리드 리

Universal head solid rivet for aircraft

ICS
49.040.20
CCS
V20
发布
1999-12-18
实施
1999-12-18

이 규격은 점시 머리까지 나사산이 있고 내부 오프셋 십자홈이 있거나 없는 드라이브 형식 금

Aerospace-Screws, pan head, internal offset cruciform ribbed or unribbed drive, threaded to head,MJ threads metallic material, coated or uncoated, strength classes less than or equal to 1100MPa­Dimensions

ICS
49.040.20
CCS
V20
发布
1998-12-19
实施
1998-12-19

이 규격은 보통의 정육각머리 나사의 규격을 몸통의 정밀 공차 또는 큰 공차를 갖는 허용 오

Aerospace-Bolts, normal hexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated strength classes less than or equal to 1100MPa-Dimensions

ICS
49.040.20
CCS
V20
发布
1998-12-19
实施
1998-12-19

This standard specifies the characteristics of screws, 100° countersunk normal head, slotted, threaded to head, in alloy steel, cadmium plated.Classification :900 MPa / 235 ℃ note:1) Minimum tensile strength of the material at ambient temperature2) Maximum temperature thatThe screw can withstand without continuous change in its original characteristics, after return to ambient temperature.The maximum temperature is determined byThe surface treatment

Aerospace series - Screws, 100° countersunk normal head, slotted, threaded to head, in alloy steel, cadmium plated - Classification: 900 MPa (at ambient temperature)/235 °C

ICS
49.040.20
CCS
发布
1997-01-01
实施

This standard specifies the characteristics, qualification and acceptance requirements for self-locking nuts with MJ threads in FE-PA2601.

Aerospace series - Nuts, self-locking, MJ threads, in heat resisting steel FE-PA2601 (A286) - Classification: 1100 MPa (at ambient temperature)/650 °C - Technical specification

ICS
49.040.20
CCS
发布
1997-01-01
实施

This standard specifies the dimensions andaluminium alloys, diameter 6 mm‘D‘applic鱿ions.tolerances100 mm,of circularthicknesstubes for1 mm

Aerospace series - Circular tubes for structures in aluminium and aluminium alloys - Diameter 6 mm <= D <= 100 mm - Thickness 1 mm <= a <= 6 mm - Dimensions

ICS
49.040.20
CCS
发布
1997-01-01
实施

This standard specifies the characteristics, qualification and acceptance requirements for bolts withMJ threads in NI-PH2601.

Aerospace series - Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) - Classification: 1275 MPa (at ambient temperature)/650 °C - Technical specification

ICS
49.040.20
CCS
发布
1997-01-01
实施

Diese Norm legt die Eigenschaften von 100° Senkschrauben mit Schlitz, Gewinde ann?hernd bis Kopf, aus korrosionsbest?ndigem Stahl, passiviert, fest. Klasse : 600 MPa 1> / 425 °C 2?

Aerospace series-Screws ,100 degree countersunk moumal head,slotted,threaded to head,in corrosion resisting steel,passivated-Classification-600MPa (at ambient temperature)/425 degree

ICS
49.040.20
CCS
发布
1996-10-01
实施
1996-10-01

Diese Norm legt die Eigenschaften von Flachkopf-Pa?schrauben mit Flügelkreuzschlitz und kurzem Gewinde, aus legiertem Stahl, verkadmet, fest. Klasse : 900 MPa 1> / 235 °C 2>

Aerospace series-Screws,pan head,offset cruciform recess,close tolerance normal shank,short thread,in alloy steel,cadmium plated-Classification-900MPa (at ambient temperature)/235 degree

ICS
49.040.20
CCS
发布
1996-10-01
实施
1996-10-01

Diese Norm legt die Eigenschaften von Flachkopf-Pa?schrauben mit Flügelkreuzschlitz und kurzem Gewinde, aus legiertem Stahl, verkadmet, fest. Klasse : 1 100 MPa 1? / 235 °C 2?

Aerospace series-Screws,pan head,offset cruciform recess,close tolerance normal shank,short thread,in alloy steel,cadmium plated-Classification-1100MPa (at ambient temperature)/235 degree

ICS
49.040.20
CCS
发布
1996-10-01
实施
1996-10-01

Diese Norm legt die Einbaubedingungen (Werkzeuge, Einnietung und Prüfung) für selbstsichernde, verzahnte Einnietmuttern nach EN-Normen fest. Sie ist anzuwenden, wenn auf sie Bezug genommen wird.

Aerospace series-Shank nuts,self-locking,serrated-Installation procedure

ICS
49.040.20
CCS
发布
1996-10-01
实施
1996-10-01

Diese Norm legt die Eigenschaften von Flachkopfschrauben mit Schlitz, Gewinde ann?hernd bis Kopf, aus korrosionsbest?ndigem Stahl, passiviert, fest. Klasse : 600 MPa U / 425 °C 2?

Aerospace series-Screws ,pan head,slotted,threaded to head,in corrosion resisting steel,passivated-Classification-600MPa (at ambient temperature)/425 degree

ICS
49.040.20
CCS
发布
1996-10-01
实施
1996-10-01

Diese Norm legt die Ma?e der Einbaul?cher für Einnietmuttern mit 60°-Aufweitung nach EN-Normen und die entsprechenden Funktionsma?e des Bauteilflansches zur Verwendung in der Luft- und Raumfahrt fest.

Aerospace series-Shank nuts-Installation holes,60 degree swage,flanges-Design standard

ICS
49.040.20
CCS
发布
1996-10-01
实施
1996-10-01



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