NAVY MIL-I-22027-1959 IGNITER JET ENGINE MK 243 MOD 2《MK 243 MOD 2型喷气发动机点火器》.pdf
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1、MIL-1-22027 13 W 7977906 0301901 3 W Y, - / 7 ML 1-22 027 (Nord) MILITARY SPEGIFIGATION IGNITER, JET ENGINE, MK 243 MOD 2 1. SCOPE 1,l This specification governs the manufacture, assembly and preparation for delivery of the Igniter9 Jet Ehgine Mk 243 Mod 2 and methods of inspection and tests upon wh
2、ich product acceptance I will be based, 2, APPLICABLE DOCUMENTS 2.1 The following documents of the issue in effect on date of invitation for bids, form a part of this specification: SPECIFICATIONS Federal PPP-T-60 Tape, Pressure Sensitive Adhesive, Waterproof for Packaging and. Sealing PPP-B-566 Box
3、es, Folding, Paperboard PPP-B- 62 1 Boxea; W00d, Nailed and Lockcorner PPP-B- 636 Boxes; Fiber PPP-B-67 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-1-22027 13 7777706 0301702 5 Military MIL-P-116 MIL-Bol31 STANDARDS Military MIL-STD-105 MIL
4、-STD-129 MIL-STDo356 MIL-STD-351 i MIL-STD-352 MIL- STD- 354 DRAWINGS Bureau of OrdLnaiio.e LD 282366 Preservation, Methode of Barrier Material; Waiter Vaporproof, Flexible Sampling Proeedurea and Tables for Marking f0.r Shipment and Storage Jolt Test for u8e in Production of Jumble Test for ube in
5、Production Forty (40) Foot Drop Teat for use Teqer-eituize md Humidity Test for Iniupsstloar .by Attributes Fuzes of Fuzes in Produstiow of Fuses We in Prod.uction of Fuzee and all drawingsi, s-andarcis ad specifica$iswa listed on the above LD, (Copies of specifications, fn 4,3 o 1 Coqsaaents The Go
6、vemnt iiiqectcar shall acertain that prior t assembly all oonents of the igniter procured under separate specfieations car drawings have been inspected, tested and accepted in accordance with their respective speci- fications 0% drawings, 4,4 Acceptance testso Unless otherwise specified a11 inspee-
7、tion and tests shall be at the place of manufacture, 4,4,1 JmbBs test.:, Four igniters shall be rmdomly selected from each seventy-five (75) prsductisn samples or multiples thereof selected in accordance with 4,4020 shall be subjected to the jumble. test of Standard MZL-STD-351, These igniters Provi
8、ded by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-1-22027 13 77999Ob 030190b 2 4.401,1 Acceptance criteria (1) No explosive or pyrotechnie element shall be initiated, (2) The igniter shall show no signs of breakdown or loosen- ing which will make the as
9、sembly unsafe to handle or dangerous to use, The failure of one or more igniters to meet the above requirements shall be cause for rejection of the lot, subjected t0 the functional test of 4,4,2, more igniters to meet the requirement8 of 30202 ahall be cause for rejection of the lot represented, The
10、se samples shall be Failure of one or 4.4,2 Functional test, The igniter shall be mounted, axis vertically with the primer end up, in a suitable safety chamber which simulates the emergency igniter combustion chamber of Aircraft Jet Engine 5-48“ Head spaceD firing pin protrusion, firing pin tension,
11、 firing pin contour, and seating flange dia- meter shall conform tO applicable combustion chamber drawings. The igniter shall be fired by actuating the firing pin, shall be conducted in accordance with Standard MIL-STD-105, Inspection Level I, AQL 0,6% percent defective, combustion chamber informati
12、on, Sampling See 602 for 4.49201 Aeeeptmee, Conformance with requirements of 3.2,2 shall determine acceptability, 4.5 Preproduction lot tests, These tests shall be conducted on the prepmduetion lot and on such production material as specifically designated by the Government, lot must prove acceptabl
13、e prior to any further production under the contract The preproduction 4.5, Jumble test, Twenty-four igniters shdh be subjected to the jumble test of 40401, 4,5,1,1 Acceptance criteria (i) No explosive OF pyrotechnie element shall be initiated, (2) The igniter shall show no signs of breakdm or loose
14、ning which will make the assembly unsafe to handle or dangerous to use, 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-1-22027 13 M 7977706 0303707 4 i *-; MIL-1-22027(NO1?d) Failure of one or more igniters to meet the above requirements shall
15、 be cause for rejection of the lot represented, 4.5 1 1 1 The twenty-four igniters, accepted ia accordance with 4050101, shall be subjected to the functional test of 4,4,2, Failure of two or more igniters to meet requirements of 3.2.2 shall be cause for rejection of the lot represented, 4,5, Tempera
16、ture and humidity test, Fifty igniters shall be subjected to the temperature and humidity test of Standard MIL-STD-354, 4050201 Acceptance criteria, Follcwng this teat the igniters shall be subjected to the functional test of 4.4,2, Failure of four or more igniters to meet the requirements of 3.2.2
17、shall be cause for rejection of the lot represented, 4,5,3 Forty Foot Drop test, Ten igniters shall be subjected to the forty foot drsp test as prescribed in Standard MIL-STD- 352, Two igniters shall be subjected to a guided drop; one to strike flange dom, and one fonge up, The remaining igniters sh
18、all be dropped for random impact, 4,5 3 u 1 Acceptance criteria (1) The igniter shall be safe to handle and dispose of (2) N0 explosive OP pyrotechnic element shall be initiated, Failure of one or more igniters t0 meet the above requirements shall be cause for rejection of the lot represented, 4,5.4
19、 Jolt test, Ten igniters shall be subjected to the jolt test of Standard MIL-STD-350, mounted in a fixture which rigidly sinppsrts the igniter by the flanged end and shall be jolted in each of the following positions: Each igniter shall be (i) Axis vertical; flanged end up (2) Axis vertical; flanged
20、 end dm (3) Axis horisontal 7 Q .i* Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NIL-1-22027 13 M 997990b 0301908 b MIL- 1-22027 (01-d 4,5,4,1 Aeeeptanee criteria (1) No explosive or pyrotechnic element shall be initiated, (2) The igniter shall be
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