Quantcast Figure 1-12. AADS Dimensions.

 

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Figure 1-11. AADS Cutaway View showing Static Plumbing.
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TM-9-1270-219-13-P Fire and Flight Air Data Subsystem Helicopter Armament: XM 143 PN 03-004-02 Manual
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AADS FUNCTIONAL DESCRIPTION
TM 9-1270-219-13&P
Figure 1-12. AADS Dimensions.
generate electronic analog angle signals. The main internal
d a t u m s is automatically accomplished by the dowel fitted
volume of the neck is maintained at static pressure by the
on
the
AADS.
The
AADS
is
secured
to
the
sensor
use of sealed bearings at the gimbals.
i n s t a l I a t i o n by three bolts.
d. A A D S
Body. The AADS body consists of three
e. A i r T e m p e r a t u r e S e n s o r ( A T S ) . The ATS, which is
assemblies, the body and the plug assembly, the cover and
attached to the cover and the dowel assembly, draws in
dowel assembly, and the plate and connector assembly.
air through its trailing edge so that the platinum resistance
Two
pressure
connectors
(part
of
the
body
and
plug
sensing
element
is
completely
protected
from
impinging
assembly) and a 22-pin electrical connector (part of the
water droplets, which are separated from the airflow by
plate and connector assembly) interface with the sensor
the inertial effect. Since water is separated out from
i n s t a l l a t i o n . The body has a reference mounting alignment
t h e flow of air over the element no ice formation occurs
pin
against
which
all
AADS
alignment
is
referred.
o n the element. Ice formation on the leading edge of the
Mechanical alignment of the AADS with the helicopter
shroud has an insignificant effect on sensed temperature

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