1、MIL-T-5563 66 7797706 OLL15537 7 W - MI L-T-85563 (AS) 2 Septerriber 1982 MILITARY SPECIFICATION FOR TEMPERATURE LIMITER AMPLI FI ER(TLA) -TRIM TEST SET TTK - 383/ E 24M- 30 AND CABLE CASE CNK-320/E24M-30 This specification is approved for use by Naval Air Systems Comnand, Depart- ment of the Navy,
2、and is available for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope - This specification establishes the requirements for the manu- facture andacceptance of the Temperature Limiter Amplifier-Trim Test Set TTK- 383/E24M-30 and the Cab1 e Case CNK-320/E24M-30. 2.
3、APPLICABLE DOCUMENTS 2.1 Government Documents - The following documents of the issue in effect on the date of invitation for bid or request for proposal, form a part of this specification to the extent specified herein: SPECIFICATIONS Mi 1 i tary MIL-Q-9858 - Quality Program Requirements MIL-E-17555
4、 MIL-T-18303 - Electronic and Electrical Equip- ment, Accessories, and Repair Parts: Packaging and Packing of - Test Procedures, Reproduction, Acceptance and Life for Aircraft Electronic Equipment, Format for Benef i ci al comnents (recomendat i ons , addi ti ons , del eti ons ) and any pertinent da
5、ta which may be of use in improving this document should be addressed to: Commanding Officer, Naval Air Engineering Center, Engineering Specifications and Standards Department (ESSD) code 93, Lakehurst, NJ 08733, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426
6、) appearing at the end of this document or by letter. FSC 6685 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-85563( AS) MIL-T-18307 MIL-T-28800 STANDARDS Mi 1 i tary MI L-STD-108 M IL -STD- 1 O9 MIL-STD-129 MIL-STD-454 MIL-STD-461 MIL-STD-462
7、 MI L-STD- 781 - Nomenclature and Identification for Electronic, Aeronautical and Aeronautical Support Equipment including Ground Support Equipment - Test Equipment for use with Electrical and Electronic Equi p- ment, General Specification for ; - Definition of and Basic Requirements for Enclosures
8、for Electric and Electronic Equipment - Quality Assurance Terms and Defi- nitions - Marking for Shipment and Storage - Standard General Requirements - Electromagnetic Interference for Electronic Equipment Characteristics, Requirements for Equipment - Electromagnetic Interference Characteristics, Mea
9、surement of - Reliability Tests: Exponential Distribution MIL-STD-810 - Envi ronmental Test Methods (Copies of specifications, standards, drawings and pub1 ications required by contractors in connection with specific procurement functions should be obtained from the procuring activity or as directed
10、 by the contracting off i cer) HANDBOOKS (C) MIL-HDBK-235-2 -2- - Electromagnetic (Radiated) Envi- ronment Consi derat i ons for Design and Procurement of Elec- trical and Electronics Equipment Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-85
11、563 66 m 9797906 OLLiS54L 7 m a P i O a MIL-T-85563( AS) Handbooks may be obtained from: Comnander Naval Electronic Systems Command Standardization Program Branch Washington, D. C. 20360 DRAW I NGS DL 1083AS100 - Test Set, Temperature Limiter Amp1 i fi er - Trim A/E24M-30 Drawings may be obtained fr
12、om: Cmnandi ng Off i Cer Naval Avionics Center (Code 915.4) 6000 E. 21st Street Indianapolis, Indiana 46218 3. REQUIREMENTS 3.1 Item Definition. The TLA-Trim Test Set TTK-383/E24M-30 and the Cable Case CNK-320/E24M-30, is used to trim and troubleshoot the TF41 engine used in the A-7E aircraft. test
13、set provides on four 3 and 1/2 digit, 7 segment incandescent displays the necessary data for adjusting the engine erformance. high pressure compressor rotor speed (NH B and accel erati on or decel erati on times; low pressure compressor rotor speed (NL); inlet air temperature (Tl); turbine outlet te
14、mperature (TOT or T5.1); inlet guide vane (IGV) angle; tem- perature limiter amplifier output current (mAdc) and voltage (Vdc). set can simulate the low pressure compressor tachometer signal (NL SIM) and turbine outlet (T5.1 SIM) or inlet air (T1 SIM) thermocouple signals. The cables provide the nec
15、essary engine interface and the The test set measures The test 3.1.1 Major Components List. The major components are: Component Part Number Quantity Manufacturer TTK-383/E24M-30 1083AS200-1 1 IAW Drawing CNK-320/E24M-30 1083AS700-1 1 IAW Drawing 3.2 Characteristics. 3.2.1 Test Conditions and Standar
16、d Operating Conditions. The General Requirements (Section 3) of MIL-STD-810 apply to the test conditions and stand- ard operating conditions for the TLA-Trim Test Set and Cable Case. 3.2.2 Perfomance. The performance characteristics for the TLA-Trim Test Set and Cable Case, are described below for t
17、he operating temperature range of -40C to +55OC. The cables must be connected to the test set to obtain the performance characteristics. locates the controls, switches, digital displays, etc. , identified in para- graphs 3.2.2.1 through 3.2.2.14 below). (Figure 1, TLA-Trim Test Set front panel, -3-
18、Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-P MIL-T-5563 bb W 777770b 03455412 7 MIL-T-85563( AS) 3.2,2.1 FUNCTION Display. The FUNCTION Display on the test set shall indicate voltage, current, or inlet guide vane (IGV) angle probe position as se
19、lected by the FUNCTION rotary switch, shown below, the positive Direct Current (DC) voltage applied to pin 12 (e) and pin 14 (-) of the W6 cable connector labled Temperature Limiter Amplifier Connector 1 (TLA CONN 1) . 3.2.2.1.1 VOLTAGEI The FUNCTION display shall indicate within the limits Range 0.
20、0 50.0 VdC Resol ut i on OS Vdc Accuracy 4 0.5 Vdc Transient Response time (t) (10% (SV)50 Hz 1/(5 X input freq.) fr input freq. 50.0) Accel Timer Start display , the resistance between the pins in 3,2.2,6 and 3-2.2.7 shall measure greater than 1 megohm. -8- Provided by IHSNot for ResaleNo reproduct
21、ion or networking permitted without license from IHS-,-,-MIL-T-5563 bb 77999Ob 0145547 MI L-T-85563 (AS ) 3.2.2.9 NL SIM Adjust(AD3). When the ENG SPEED rotary switch is set to NL SIM, the NL SIM-ADJ shall vary the frequency of the waveform at pin 5 1-1 ) and pin 4 (common) of W6 cable connector lab
22、eled To TLA CONN 4. limits of the NL SIM waveform are listed below. The Frequency Range Less than 252 Hz to 462 Hz Frequency -Range Adjustment f 20 Hz min. using R6 on Printed Ci rcui t Board Assembly Reference Desi gnator 1AlA2A9. Amplitude (LOAD = 1,000 ohm) Greater than 20 Volts peak to peak Wave
23、form Si ne wave Di stort i on Less than 10% - (VP-P) 3.2.2.10 Temperature Simulation. The test set provides an adjustable millivolt source for simulatPng thermocouple outputs from -75C to 900OC. The output is selected by the SIM switch and adjusted by the SIM ADJ potentiometer. 3.2c2-.J0.1 SIM Inlet
24、 Air Temperature (Tl). When the SIM switch is set to T1, the millivolt source is connected to pin A (t) and pinJ-(-) of W3 cable connector labeled To TLA CONN B. set to T5.1, the millivolt source is connected to pin E (+) and pin F (-) of W3 cable connector labeled To TLA CONN B. 3.2.2.10.2 SIM Turb
25、ine Outlet Temperature (T5.1), When the SIM switch is 3.2.2.10.3 Temperature Simulation Limits. The limits of the millivolt source are listed below. Range (min.) -3.0 mV to t38.0 mV Adj ustment Source Impedence (max. ) Continuous (i0 turn .potentiometer) 6 ohm 3.2.2.11 LOAD-OFF-PULLDOWN Switch. In t
26、he LOAD position, this switch con- nects simulated thermocouple 1 oads across the temperature simulation outputs. A 2.8 IC 0.3 ohm load and a 1.3 I 0.3 ohm load are connected across pins E and F and pins A and J, respectively, of the W3 cable connector labeled To TLA CONN B. In the PULLDOWN position
27、, the resistance between pin 2 and pin 10 of - NL switch function is enabled. means of checking the circuitry within the test set. TEST function are listed below. cable conKZ5FTabeled To TLA CONN 1 is less than 1 ohm and the +LO% 3.2.2.12 SELF-TEST Rotary Switch. The SELF TEST rotary switch provides
28、 a The limits of the SELF -9- Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-_- -tlIL-T-55b3 bb 777770b 0/1i554 T a MI L-T-85563 (AS ) SELF TEST Position Indi cat or I ndi cat i on - LAMP - TIME Display -188.8 ENG SPEED Display -188.8 - TEMP Display
29、 -1 888 FUNCTION Di spl ay -188.8 - t10v FUNCTION Di spl ay 10.0 f 0.2 - T1 - TEMP Display -0 1 2 - T5.1 - TEMP Display 733 4 2 - NL ENG SPEED Display 100,o f 0.1 - NH ENG SPEED Display 100.0 i: 0.1 3.2.2.13 Intensity (INTEN) Switch, The INTEN switch controls the brightness of the illuminated front
30、panel and-displays. In the OFF position, the front panel is not illuminated and the displays are dir In the Low (LO1 position, the front panel is dimly illuminated and the displays are bright, In the Hi h HI position, the front panel is brightly illuminated and the displays + are im. 32.2.14 POWER S
31、witch and Indicator. When 400 Hz 115 Volts alternating current (Vac) power is connected to the test set, the POWER switch shall turn the test set ON and and the indicator shall glow green in the position, When 60 Hz 11rVac power is connected to the test set, the POWER switch shall not energize the t
32、est set but the indicator lamp shall glow green when the - POWER switch is &l. performance requi rements of 3.2.2 when exposed to the fol 1 owing envi ronmental condi ti ons , 3,2.3 Environmental. The TLA-Trim Test Set and Cable Case shall meet the 3.2.3.1 Temperature and Altitude. a, Operating temp
33、erature range shall be -4OOC to + 55OC. b. Operating ATtitude shall be 10,000 feet maximum, c. Non-operating temperature range shall be -55OC to +7OoC, d. Non-operating altitude-shall be 50,000 feet maximum. 3.2.3.2 Vibration. Requirements of MIL-T-28800 for Class 6 equipment apply. -1 o- . I Provid
34、ed by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-85563 (AS ) 3.2.3.3 Shock, Mechanical Pulse. Requirements of MIL-T-28800 apply. 3.2.3.4 Spl ashproof. Requirements of MIL-T-28800 for Sty1 e A apply. 3.2.3.5 Humidity. As required by the test procedure
35、of 4.2.7. 3.2.3.6 Salt Atmosphere. Requirements of MIL-T-28800 for Style A, 3.2.3.7 Explosive Atmosphere. Requirements of MIL-T-28800 apply. 3.2.3.8 Sand. and Dust. Requi rements of MIL-T-28800 apply. exposure , encl osure apply. 3.2.3.9 Fungus. The TLA-Trim Test Set shall be inherently fungus-inert
36、. A certification of non-nutrient fungus-inert materials duly witnessed and certified shall be submitted to the procuring activity for approval. 3.2.3.10 Electromagnetic Interference (Contractor). Requirements of MIL-T-28800 for C1 ass 2 equi pment applies , with the additional requirements of Condu
37、cted Emissions CEO1, CE02, CE04, and Radiated Suscepti bl ity RSOl RS02. 3.2.3.11 Electromagnetic Vulnerability (Government). The TLA-Trim Test Set shall not be vulnerable to the electromagnetic environment of an aircraft carrier flight deck when tested in accordance with 4.2.1.12. 3.2.4 Reliabilit
38、. The TLA-Trim Test Set shall have a Mean-Time-Between Failure (MTdhours demonstrated at the 98% Re1 iabil i?y Level when tested in accordance with 4.2.1.13. 3.3 Design and Construction. 3.3.1 Workmanship. Requirements of MIL-T-28800 apply. 3.3.2 Production Drawings. The TLA-Trim Test Set and Cable
39、Case shall be fabricated in accordance w-ith the drawings listed in DL1083ASI00 and subsi- diary specifications listed in the data list defined bv this sPecification. except insofar as ments of this spec condition of final .cab1 e requi rements may be applicable. 3.3.3 Interch rrors on the drawings
40、may be incomp&ible with the require- fication and related specifications. In any case, it is a acceptance that the units manufactured meet all the app1.i- of this specification and such acceptance test documents as ngeabi 1 i ty. The requi rements of MIL-T-28800 apply. 4. QUALITY ASSURANCE PROVISION
41、S 4.1 Responsibility for Inspection. Unless otherwise specified in the contract or purchase order, the supplier is responsible for the performance of al 1 inspect i on requi rements speci fi ed herei n. Except as otherwi se speci $i ed in the contract or purchase order, the supplier may use his own
42、or any other facilities suitable for the inspections required herein. The procurring acti- vity reserves the right to perform any of the inspections specified herein -1 1- Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-M I L- T-85 56 3 (AS ) where s
43、uch inspections are deemed necessary to assure that the product con- forms to the specified requirements. 4.1.1 Quality Assurance Terms and Definitions. The quality assurance terms used herein are defined in MIL-STD-109. 4.1.2 gual ity Assurance Program. The requirements of MIL-Q-9858 apply as speci
44、fied in the contract. 4.2 Classification of Inspections. The inspection requirements are classified as (a) Qualification or First Article and (b) Quality Conformance. . 4.2.1 Qualification or First Article Inspection. Tests and examinations for Qualification or First Article Inspection are listed be
45、low: a. Preoperational Inspection b. Temperature and Al ti tude c. Vibration d. Shock, Mechanical Pulse e. Spl ashproof f. Humidity g. Salt Atmosphere h. Explosive Atmosphere i. Sand and Dust j. Electromagnetic Interference k. 1. Reliability El ectromagnet i c Vu1 nerabi 1 i ty 4.2.1.1 Test Plans an
46、d Test Reports. Unless otherwise specified in the contract or purchase order, test plans and test reports shall be submitted to the procuring activity for approval . 4.2.1.1.1. Test Plans. Test plans shall detail the test procedures and reference the test method to the requirements specified herein.
47、 The test plans shall provide for the recording of actual readings rather than check marks to indicate conformance to the requirements. Limits for acceptance shall be included. 4.2.1.1.2 Test Reports. Test reports shall detail the execution of the test lans and present the required data with the lim
48、its for acceptance. be included where the recorded data does not meet the limits for acceptance. Detai P s of corrective action required to meet the limits for acceptance shall -12- I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-85563 bb m 7
49、777906 OL4555L T = MI L-T-85563( AS ) 4.L1.1.3 Commencement of Testing. The procuring activity shall be notified, at least three weeks in advance, of the scheduled date for the start of Qualification or First Article inspection to permit timely witnessing of the inspection by technical personnel from the procuring activity. 4.2.1.1.-4 Failure Criteria. Failure to meet the requirements of any tests or exami
