AECMA PREN 4673-001-2009 Aerospace series Inserts UNJ threads self-locking with self-broaching keys Part 001 Installation and removal procedure Edition P 1《航空航天系列.带自拉孔键的自锁UNJ螺纹插件.第.pdf

《AECMA PREN 4673-001-2009 Aerospace series Inserts UNJ threads self-locking with self-broaching keys Part 001 Installation and removal procedure Edition P 1《航空航天系列.带自拉孔键的自锁UNJ螺纹插件.第.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 4673-001-2009 Aerospace series Inserts UNJ threads self-locking with self-broaching keys Part 001 Installation and removal procedure Edition P 1《航空航天系列.带自拉孔键的自锁UNJ螺纹插件.第.pdf（11页珍藏版）》请在麦多课文档分享上搜索。

1、ASD STANDARD NORME ASD ASD NORM prEN 4673-001 Edition P 1 December 2009 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONAvenue de Tervuren, 270 - B-1150 Brussels - Tel. 32 2 775 8126 - Fax. 32 2 775 8131 - www.asd-stan.orgICS: Descriptors: ENGLISH VERSION Aer

2、ospace series Inserts, UNJ threads, self-locking, with self-broaching keys Part 001: Installation and removal procedure Srie arospatiale Douilles filetes, filetage UNJ, freinage interne, clavettes autobrochantes Partie 001 : Procdure dinstallation et dextraction Luft- und Raumfahrt Gewindeeinstze, U

3、NJ-Gewinden, selbstsichernd, mit selbstrumenden Stiften Teil 001: Ein- und Ausbauverfahren This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the E

4、uropean Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, w

5、ithout re-identification of the standard. After examination and review by users and formal agreement of ASD-STAN, it will be submitted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN nation

6、al members have then to implement the EN at national level by giving the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. Edition approved for publication 15 December 2009 Comments should be sent within six months after the date of publication t

7、o ASD-STAN Mechanical Domain Copyright 2009 by ASD-STAN Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-001:2009 (E) 2 Contents Page Foreword2 1 Scope 3 2 Normative references 3 3 Insert informat

8、ion 3 4 Inspection requirements before installation.5 5 Installation tools 5 6 Checks of insert position and keys broaching.8 7 Inspection of minimum self-locking torque 9 8 Insert replacement.9 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Mechanical Domain. A

9、fter inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without li

10、cense from IHS-,-,-prEN 4673-001:2009 (E) 3 1 Scope This standard specifies the installation and removal procedure (hole profile, tools) of self-locking, self-broaching key, UNJ thread inserts defined by EN standards, for aerospace applications. 2 Normative references The following referenced docume

11、nts are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 4673-002, Aerospace series Inserts, UNJ threads, self-locking, with self-broa

12、ching keys Part 002: Design standard 1)EN 4673-004, Aerospace series Inserts, UNJ threads, self-locking, with self-broaching keys Part 004: In heat resisting nickel base alloy Ni-P100HT (Inconel 718), silver plating 1)EN 4673-005, Aerospace series Inserts, UNJ threads, self-locking, with self-broach

13、ing keys Part 005: in heat resisting nickel base alloy Ni-P101HT (WASPALOY), silver plating1)EN 4673-006, Aerospace series Inserts, UNJ threads, self-locking, with self-broaching keys Part 006: in heat resisting steel FE-PA2601 (A286), MoS2coated1)ISO 3161, Aerospace series UNJ threads General requi

14、rements and limit dimensions 3 Insert information Tables 1 to 3 provide the cross reference between the insert codification, the related bolt thread and the tapped hole diameter. 1) Published as ASD-STAN Prestandard at the date of publication of this standard. Copyright ASD-STAN Provided by IHS unde

15、r license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-001:2009 (E) 4 Table 1 Normal size insert Insert reference Bolt thread diametera Tapped hole diametera Tapped hole referencea EN 4673-004-3-0 EN 4673-005-3-0 EN 4673-006-3-0 .190 0-32UNJ

16、F .312 5-18UNJC-3B EN 4673-002-3-0 EN 4673-004-4-0 EN 4673-005-4-0 EN 4673-006-4-0 .250 0-28UNJF.375 0-16UNJFC-3B EN 4673-002-4-0 EN 4673-004-5-0 EN 4673-005-5-0 EN 4673-006-5-0 .312 5-24UNJF .437 5-16UNJ-3B EN 4673-002-5-0 EN 4673-004-6-0 EN 4673-005-6-0 EN 4673-006-6-0 .375 0-24UNJF .500 0-16UNJ-3

17、B EN 4673-002-6-0 EN 4673-004-7-0 EN 4673-005-7-0 EN 4673-006-7-0 .437 5-20UNJF .562 5-16UNJ-3B EN 4673-002-7-0 EN 4673-004-8-0 EN 4673-005-8-0 EN 4673-006-8-0 .500 0-20UNJF .625 0-16UNJ-3B EN 4673-002-8-0 aAccording to ISO 3161. Table 2 First repair size insert Insert reference Bolt thread diameter

18、a Tapped hole diametera Tapped hole referencea EN 4673-004-3-1 EN 4673-005-3-1 EN 4673-006-3-1 .190 0-32UNJF .375 0-16UNJC-3B EN 4673-002-3-1 EN 4673-004-4-1 EN 4673-005-4-1 EN 4673-006-4-1 .250 0-28UNJF.437 5-16UNJ-3B EN 4673-002-4-1 EN 4673-004-5-1 EN 4673-005-5-1 EN 4673-006-5-1 .312 5-24UNJF .50

19、0 0-16UNJ-3B EN 4673-002-5-1 EN 4673-004-6-1 EN 4673-005-6-1 EN 4673-006-6-1 .375 0-24UNJF .562 5-16UNJ-3B EN 4673-002-6-1 EN 4673-004-7-1 EN 4673-005-7-1 EN 4673-006-7-1 .437 5-20UNJF .625 0-16UNJ-3B EN 4673-002-7-1 EN 4673-004-8-1 EN 4673-005-8-1 EN 4673-006-8-1 .500 0-20UNJF .687 5-16UNJ-3B EN 46

20、73-002-8-1 aAccording to ISO 3161. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-001:2009 (E) 5 Table 3 Second repair size insert Insert reference Bolt thread diametera Tapped hole diametera Ta

21、pped hole referencea EN 4673-004-3-2 EN 4673-005-3-2 EN 4673-006-3-2 .190 0-32UNJF .437 5-16UNJ-3B EN 4673-002-3-2 EN 4673-004-4-2 EN 4673-005-4-2 EN 4673-006-4-2 .250 0-28UNJF.500 0-16UNJ-3B EN 4673-002-4-2 EN 4673-004-5-2 EN 4673-005-5-2 EN 4673-006-5-2 .312 5-24UNJF .562 5-16UNJ-3B EN 4673-002-5-

22、2 EN 4673-004-6-2 EN 4673-005-6-2 EN 4673-006-6-2 .375 0-24UNJF .625 0-16UNJ-3B EN 4673-002-6-2 EN 4673-004-7-2 EN 4673-005-7-2 EN 4673-006-7-2 .437 5-20UNJF .687 5-16UNJ-3B EN 4673-002-7-2 EN 4673-004-8-2 EN 4673-005-8-2 EN 4673-006-8-2 .500 0-20UNJF .750 0-16UNJF-3B EN 4673-002-8-2 aAccording to I

23、SO 3161. 4 Inspection requirements before installation Prior to installation check the installation hole to receive the insert are free from burrs and any foreign objects, grease, oil, etc. Inspect insert to be installed and ensure that it is clean and free from protective grease, etc. 5 Installatio

24、n tools 5.1 General In order to facilitate the correct assembly of the inserts use the appropriate tools. It is necessary to use one tool by insert reference. The tools and their methods of application described in this standard are not mandatory and show only the basic principles to be observed to

25、achieve the satisfactory installation and subsequent broaching and the satisfactory removal of the inserts. The maximum dimensional requirements provided shall be achieved and on no account shall the design of the tools or their methods of application be such that damage may occur to the threads or

26、the locking zone of the insert or the component into which it is being installed. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-001:2009 (E) 6 5.2 Hand installation 5.2.1 Installation tool Figu

27、re 1 illustrates a combined tool used for hand screwing and hand broaching and its overall dimensions. Figure 1 a) and Table 4 give the overall dimensions. Key 1 Screwing nose Key 1 Broaching nose for keys setting a) b) c) Figure 1 Table 4 Dimensions in millimetres Insert external thread H L .312 5-

28、18UNJC-3B 12,7 .375 0-16UNJC-3B 14,3 .437 5-16UNJ-3B 15,9 .500 0-16UNJ-3B 17,5 .562 5-16UNJ-3B 19,0 .625 0-16UNJ-3B 20,6 .687 5-16UNJ-3B 22,2 .750 0-16UNJF-3B 71 25,4 Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license fro

29、m IHS-,-,-prEN 4673-001:2009 (E) 7 5.2.2 Procedure a) Lubricate the outer thread of the insert with the lubricant referenced on the assembly drawing. Inserts installed in aluminium or magnesium alloy components shall be lightly smeared externally with a suitable compound to prevent galvanic corrosio

30、n if required on the assembly drawing. b) Fit into place and screw the insert by two turns into the component. c) Fit into place the screwing nose of the tool onto the keys, then screw the assembly into the threaded hole until the screwing nose mates the component surface as shown in Figure 1 a). d)

31、 Adjust the insert position within the X limits given in Figure 3. e) Turn the tool on the broaching nose side as showed in Figure 1 b). f) Apply a sufficient load in the direction indicated Figure 1c to broach the keys by stamping or by pressing on the tool. The keys are fitted in the proper positi

32、on corresponding to Y dimension given in Figure 3. g) Remove the tool from the insert. h) Remove excess sealing compound or lubricant if any. 5.3 Air pressure installation 5.3.1 Installation tool Figure 2 illustrates a tool for screwing, broaching and unscrewing assembled on an air pressure gun. The

33、 overall dimensions are given in Figure 2. Dimensions in millimetres 24360 2954 7613Key 1 Threaded mandrel 2 Interchangeable installation nose corresponding to the insert reference 3 Gun 4 600 kPa (6 bars) air pressure inlet Figure 2 Copyright ASD-STAN Provided by IHS under license with AECMA Not fo

34、r ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-001:2009 (E) 8 5.3.2 Procedure The air pressure gun shall be previously adjusted in order to obtain the satisfactory installation of insert and of the keys as given in Figure 3. a) Lubricate the outer thread of th

35、e insert with the lubricant referenced on the assembly drawing. Inserts installed in aluminium or magnesium alloy components shall be lightly smeared externally with a suitable compound to prevent galvanic corrosion if required on the assembly drawing. b) Screw the insert on to the threaded mandrel

36、until it is fully seated on the installation nose. c) Using the tool, screw the insert into the tapped hole until positioned: The screwing/broaching tool comes into contact with the surface of the component, when operating the air gun. The insert comes in position as shown in Figure 3 below the surf

37、ace of the casing. d) Use the air gun in the percussion mode to broach the keys. e) Unscrewing is automatic to extract the tool from the crimped insert. f) Remove excess sealing compound or lubricant if any. 6 Checks of insert position and keys broaching These checks shall be carried out with an ins

38、pection gauge common to all insert dimensions. Check dimensions X and Y which shall be in accordance with Figure 3. After broaching of keys, the component surface shall not show any distortion or cracks. Dimensions in millimetres 12X =0,130,75Y =0,250,75Key 1 Installation depth of the keys 2 Install

39、ation depth of the insert Figure 3 Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-001:2009 (E) 9 7 Inspection of minimum self-locking torque The minimum self-locking torque for the installed ins

40、ert shall conform to Table 5 and shall be checked using a low third pitch diameter passivated stainless steel test bolt (see Table 5). Bolts shall not be lubricated. The test bolts shall be periodically checked for wear and damage, any bolt falling outside the tolerances in Table 5 shall not be used

41、 for this check. The sample size/frequency for this check shall be at the responsibility of the installer. Table 5 Part number Test bolt pitch diameter Self-locking torque Normal First repair Second repair max. min. min. Associated bolt thread size insert size insert size insert mm mm Nm .190 0-32UN

42、JF EN 4673-004-3-0 EN 4673-005-3-0 EN 4673-006-3-0 EN 4673-004-3-1EN 4673-005-3-1EN 4673-006-3-1 EN 4673-004-3-2EN 4673-005-3-2EN 4673-006-3-2 0,168 0,1674 0,46 .250 0-28UNJF EN 4673-004-4-0 EN 4673-005-4-0 EN 4673-006-4-0 EN 4673-004-4-1EN 4673-005-4-1EN 4673-006-4-1 EN 4673-004-4-2EN 4673-005-4-2E

43、N 4673-006-4-2 0,225 0,2243 0,80 .312 5-24UNJF EN 4673-004-5-0 EN 4673-005-5-0 EN 4673-006-5-0 EN 4673-004-5-1EN 4673-005-5-1EN 4673-006-5-1 EN 4673-004-5-2EN 4673-005-5-2EN 4673-006-5-2 0,284 0,2827 1,46 .375 0-24UNJF EN 4673-004-6-0 EN 4673-005-6-0 EN 4673-006-6-0 EN 4673-004-6-1EN 4673-005-6-1EN

44、4673-006-6-1 EN 4673-004-6-2EN 4673-005-6-2EN 4673-006-6-2 0,346 0,3450 2,14 .437 5-20UNJF EN 4673-004-7-0 EN 4673-005-7-0 EN 4673-006-7-0 EN 4673-004-7-1EN 4673-005-7-1EN 4673-006-7-1 EN 4673-004-7-2EN 4673-005-7-2EN 4673-006-7-2 0,403 0,4019 3,16 .500 0-20UNJF EN 4673-004-8-0 EN 4673-005-8-0 EN 46

45、73-006-8-0 EN 4673-004-8-1EN 4673-005-8-1EN 4673-006-8-1 EN 4673-004-8-2EN 4673-005-8-2EN 4673-006-8-2 0,465 0,4643 4,06 8 Insert replacement 8.1 Insert removal When repairing, the self-broaching key inserts can be removed as follows: Copyright ASD-STAN Provided by IHS under license with AECMA Not f

46、or ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-001:2009 (E) 10 a) Drill using a diameter A drill to depth B as shown in Figure 4 and Table 6 or pilot spot facing cutter. Material may also be ground or milled away locally in the key area as shown in Figure 4,

47、so that keys can be removed. OR Key 1 Drill 2 Mill or grinder Figure 4 b) Deflect the keys inward to clear the tapped hole as shown in Figure 5. Figure 5 c) Unscrew the insert with the extraction tool as shown in Figure 6. Figure 6 d) After machining, remove the part fragments of the insert using th

48、e appropriate tool. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-001:2009 (E) 11 Table 6 Dimensions in millimetres Tapped hole A B reference diameter max. max. EN 4673-002-3-0 .312 5-18UNJC-3B 6,3 3,0 EN 4673-002-3-1 EN 4673-002-4-0 .375 0-16UNJC-3B 7,7 3,1 EN 4673-002-3-2 EN 4673-002-4-1 EN 4673-002-5-0 .437 5-16UNJ-3B 9,3 3,4 EN 4673-002-4-2 EN 4673-002-5-1 EN 4673-002-6-0 .500 0-16UNJ-3B 10,9 3,6 EN 4673-002-5-2 EN 4673-002-6-1 EN 4673-00