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时间:2011-03-28 18:24来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

R  |  | Main/Battery Discrete at Main  | 26QJ2  | 
R  |  |  | 27QJ2  | 
R  |  |  |  | 

R -----------------------------------------------------------------------------
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 301-399, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 341
 May 01/04 CES


R (8) INPUT PARAMETERS
R There are three pages of input parameters that supply data.
R They are:
R - (a) INPUT PARAMETERS, Page 1 - FQIS INPUT PARAMETERS
R - (b) INPUT PARAMETERS, Page 2 - FQIS PROBE CAPACITANCES
R - (c) INPUT PARAMETERS, Page 3 - FQIS DISCRETE INPUTS.
R
R The INPUT PARAMETER pages (only) are automatically updated, without
R request from the CFDS, once every 5.5 seconds.

R (a) INPUT PARAMETERS, Page 1 - FQIS INPUT PARAMETERS
R (Ref. Fig. 304A)
R This page shows:
R - the permittivity from the Ultracomp (center and right tanks)
R - the temperature from the Ultracomp (center and right tanks)
R - the velocity from Ultracomp (center and right tanks)
R - the permittivity one from Dualcomp (left tank)
R - the permittivity two from Dualcomp (left tank)
R - the density calculated for each tank
R - the fuel temperature from Probe 2 temperature sensors
R - the effective pitch
R - the effective roll.
R
R The measured values from the Ultracomp of the fuel permittivity
R (K), temperature(T), and velocity (V) are shown on this page.
R These values are used to calculate the density shown which must
R be the density calculated for that tank.
R
R The measured fuel permittivities from the Dualcomp (A) and (B)
R respectively, are shown on this page, as is the measured value of
R fuel temperature from the Probe 2 locations.
R
R The pitch and roll shown is that used by the FQIC for gauging.
R
R There are three methods of obtaining of attitude data, they are:
R - from the longitudinal, lateral, and normal accelerations
R supplied by ADIRS
R - from the capacitive probe data (FQIS)
R - from default data held by the FQIC/OBRM.
R
R The method used is dependant on the availability of valid input
R data.
R The hierarchy/priority of use is as shown in the above list.
R
R The Input Parameter values will be shown as long as they are
R measured, (even if out of valid range). A dash is shown if the
R parameter is not measured (due to a detected circuit failure).
R Out-of-range values exceding the display capacity are shown with
R the display at maximum magnitude and a + or - indicating the
R direction of the excursion, where applicable.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 301-399, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 342
 May 01/04 CES


R  (b) INPUT PARAMETERS, Page 2 - FQIS PROBE CAPACITANCES 
R  (Ref. Fig. 305A) 
R  This page gives the values (in picofarads) for all the 
R  capacitance devices in the tanks. That is for: 
R  - the probes 
R  - the Dualcomps 
R  - the Ultracomps. 

R  From the example of this page, the values can be read across to 
R  the applicable devices cross reference to obtain the tank and 
R  probe/sensor number. 

R  In the example, the left probe No. 10 is 48.0 pF, and the center 
R  tank probe No. 4 is 40.1 pF. 

R  The probe numbers can be related to FINs by reference to Table 
R  301A. 

R  The values will be shown as long as they are measured, (even if 
R  out of valid range). A dash is shown if the parameter is not 
R  measured (due to a detected circuit failure). 
R  Out-of-range values exceding the display capacity are shown with 
R  the display at maximum magnitude and a + or - indicating the 
R  direction of the excursion, where applicable. 

R  If the aircraft does not have an Additional Center Tank (ACT) 
R  installed the related data on the CFDS will not be shown.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 301-399, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 343
 
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