D. Pylon Section
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 003)
**ON A/C 301-399,
(Ref. Fig. 003A)
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
(Ref. Fig. 007)
R **ON A/C 151-199, 401-499,
(Ref. Fig. 007A)
**ON A/C ALL
-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA
| | | | DOOR | REF. _______________________________________________________________________________ 1HF1 ELEMENT-OVERHEAT SENSING, LH 410 414FR 36-22-00 1HF2 ELEMENT-OVERHEAT SENSING, RH 420 423FL 36-22-00 2HF1 CABLE-CONNECTING, LH 410 414FR 36-22-00 2HF2 CABLE-CONNECTING, RH 420 423FL 36-22-00 3HF1 CABLE-CONNECTING, LH 410 414FR 36-22-00 3HF2 CABLE-CONNECTING, RH 420 423FL 36-22-00
3. System Description
__________________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 001)
Component Location - Pylon
Figure 007
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 36-22-00Page 22 1301-399, 1May 01/05 1 1 1CES 1
Component Location - Pylon
Figure 007A
R 1EFF : 151-199, 401-499, 1 36-22-00Page 23 1 1 Aug 01/05 1 1 1CES 1 **ON A/C 301-399,
(Ref. Fig. 001A)
**ON A/C ALL
The aircraft leak detection system is divided into LH and RH zones by the crossfeed valve in the crossfeed duct at STA1537 (FR35). Each leak detection system operates independently. Both wing/fuselage leak detection systems are made up of twin loops (A and B) of overheat sensing elements. This eliminates the possibility of incorrect warnings, due to an AND logic. The overheat sensing elements are installed in each wing along the forward face of the front spar. Clamps and rubber grommets attach the overheat sensing elements at regular intervals along the whole length. In the fuselage, the elements are installed at STA1537 (FR35) and close to the crossover bleed-air duct. They continue (LH side elements only) up to the APU check valve on the pressurized fuselage between STA2189 and STA2243. A single loop system is installed along the bleed air duct between the APU check valve and the APU bleed valve. In each of the pylons, there is a single loop. Each loop is located near the pylon ventilation duct.
4.
Component Description
_____________________ (Ref. Fig. 002) The overheat sensing elements have a solid nickel center conductor set in a ceramic insulation of porous aluminum oxide. An inconel tube contains these components and is sealed at both ends. Eutectic salt fills the space between the tubing, the ceramic insulation and the center conductor. This mixture is compounded to give a signal at alarm temperature. For the wing and fuselage, the alarm temperature is 124 plus or minus 7 deg.C. The pylon alarm temperature quantity is 204 plus or minus 12 deg.C. The impedance between the conductor and the outer tubing decreases suddenly when the alarm temperature is reached. At this temperature, the center conductor grounds and gives an alarm signal.
5.
Operation
_________
R **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
(Ref. Fig. 007)R **ON A/C 151-199, 401-499,
(Ref. Fig. 007A)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 008)
**ON A/C 301-399,
(Ref. Fig. 008A)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 009)
**ON A/C 301-399,
(Ref. Fig. 009A)
**ON A/C ALL
(Ref. Fig. 010, 011) The overheat sensing elements continuously monitor the surrounding areas for overheat conditions. They are connected in series and detect overheat conditions at any point along the length of the elements. When only a few inches of the elements are heated to the pre-determined temperature, an alarm is caused. When this occurs, the bleed air supply is shut off automatically. If one loop is inoperative (loop A or B), the remaining loop takes over. If hot air escapes from the bleed air duct and heats an element of the operative loop, a signal is given. The signal causes:
-
the amber FAULT light on the AIR COND overhead panel to come on,
-
the activation of the ECAM system.
When the ECAM system is activated:
-
the MASTER CAUT lights on the panels 131VU and 130VU come on amber
-a single chime sounds
-
the message on the upper ECAM display unit comes on
-
the BLEED page on the lower ECAM display unit comes on.
R The FAULT light stays on as long as the overheat condition exists. The
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM PNEUMATIC 气源 2(111)
