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時間:2011-03-20 12:25來源:藍天飛行翻譯 作者:admin
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 C.  A DME channel indicator, coarse distance indicator and self-test button are provided on the front of the unit.
 D.  Two cable connectors (Pl and P2) at the rear of the unit provide interconnection for the system and ATE (automatic test equipment). Two coaxial connectors (SUPPR PULSE and ANT) on the front panel connect the suppressor pulses and the antenna to the interrogator. The RCVR OUT coaxial connector is not used.
 5.  Indicators
__________
 A.  The DME indicators are mechanical analog counters, which dispaly nautical miles-to-go on three individual counter dials of hundreds, tens, and units. There are two DME indicators, one for each system, contained within each pilots' radio magnetic indicator (RMI). The left-hand DME indicator in each RMI displays mileage from DME No. 1 and the right-hand indicator displays mileage from DME No. 2.
 B.  Warning flags (shutters) are held out of view by a warning flag voltage and cover the DME indicators when the system is inoperative, in the search mode or in the standby mode (Ref Fig. 1).
 6.  Operation
_________
 A.  Functional Description (See figure 3.)
 (1)  The DME system is used in conjunction with either TACAN, VORTAC, or VOR/DME ground stations. Each station operates on one of 252 alloted frequency channels. The airborne distance measuring equipment interrogates the ground station using one of the 126 frequencies available between 1025 to 1150 MHz (selected at 1-MHz intervals and the ground station replies at a frequency 63 MHz above or below the interrogation frequency depending on the channel being utilized. These channels (designated lX and lY through 126X and 126Y) are associated with 252 VOR/LOC frequency allocations (34-31-00).
 EFFECTIVITY

 SN 301-350  CONFIG 2  01 Page 4  Apr 25/8634-55-00
 (2)  
DME channel selection is accomplished by tuning a VOR/LOC frequency on the VHF NAV control panel which automatically tunes the DME interrogator to the DME frequency asociated with that channel. Tuning is controlled by two resistance bridges (one coarse and one fine), each with half in the control panel and half in the interrogator. Switching to various resistances in the control panel causes bridge imbalance which activates a motor-driven switch, rebalancing the bridge and performing all necessary tuning in the interrogator within 10 seconds.

 (3)  
Current VOR/LOC channel usage covers only 200 channels and, since DME tuning is slaved to VOR/LOC channel selection, DME channel utilization is also limited. VOR/LOC tuning from 108.00 MHz to

 111.95 MHz covers 80 channels where the DME search range is limited to 50 nautical miles (short range search). The remaining 120 channels (VOR/LOC tuning from 112.00 MHz to 117.95 MHz) have a search range of 192 nautical miles.

 (4)  
When the distance from a particular ground station is desired, the frequency selector on the VHF NAV control panel is set to the assigned frequency channel. Operation of the frequency selector activates the AVQ-70 tuning servo circuits which tune frequency synthesizer lAl, frequency multiplier lA2, and RF head lA3 to the proper frequencies. Frequency synthesizer lAl generates a signal which is exactly 1/12 of the required DME transmitting frequency.

 (5)  
The output of frequency synthesizer lAl is coupled to frequency multiplier lA2 where it is quadrupled in frequency, amplified, and passed to rf head lA3. Since the frequency multiplier also receives the modulator pulse output, the resulting output is a pulse-modulated signal at a carrier frequency which is 1/3 of the desired transmitting frequency. The pulsed output from the frequency multiplier is first applied to the RF head tripler cavity where it is tripled in frequency and then fed through the first, second, and final amplifier cavities to the antenna via the duplexer and low-pass filter.

 (6)  
The selected ground-based beacon station receives the interrogation signals and transmits distance reply signals on the associated transmitting channel which is 63 MHz removed from the receiver frequency.

 (7)  
The beacon reply signals picked up by the DME antenna are fed through the low-pass filter and the duplexer to a tuned preselector cavity which allows only the selected receiving frequency to reach the crystal mixer. The crystal mixer also receives a CW local oscillator signal from the rf head tripler cavity. This signal, when heterodyned with the receiving frequency, produces a 63-MHz intermediate frequency output to IF amplifier lA4. The IF amplifier first amplifies and then heterodynes the 63-MHz input signal with a 51.7-MHz local oscillator signal to produce an 11.3-MHz signal which after suitable amplification is fed through a video detector.


 EFFECTIVITY


 
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本文鏈接地址:747飛機維護手冊AMM CHAPTER 34 - NAVIGATION 第34章導航4(90)
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