accesss door removed | ±à¼ | ɾ³ý | |
acoustic panel | ÒѼÓÈë | ±à¼ | ɾ³ý |
Blanking of the Hoisting Points | ±à¼ | ɾ³ý | |
deicing fluid | ÒѼÓÈë | ±à¼ | ɾ³ý |
deicing fluids | ±à¼ | ɾ³ý | |
Engine bleed air distribution system | ·¢¶¯»úÒýÆø·ÖÅäϵͳ | ±à¼ | ɾ³ý |
fabric layers | ·Ö¿ª²é | ±à¼ | ɾ³ý |
helitest | ÒѼÓÈë | ±à¼ | ɾ³ý |
hydraulic actuator aft attachment | ±à¼ | ɾ³ý | |
left t/r half | ±à¼ | ɾ³ý | |
main slider | ÒѼÓÈë | ±à¼ | ɾ³ý |
nonlocking | ÒѼÓÈë | ±à¼ | ɾ³ý |
physical description | ÒѼÓÈë | ±à¼ | ɾ³ý |
retainer track | ·Ö¿ª²é | ±à¼ | ɾ³ý |
retract during a stow operation | ±à¼ | ɾ³ý | |
sadwol | ±à¼ | ɾ³ý | |
shows | ±à¼ | ɾ³ý | |
shows the placards | ±à¼ | ɾ³ý | |
stow hydraulic tube | ±à¼ | ɾ³ý | |
The hydraulic actuators move the translating sleeves during T/ | ±à¼ | ɾ³ý |
The T/R auxiliary and main track liners hold the sliders which | ±à¼ | ɾ³ý | |
This document shows the placards | ±à¼ | ɾ³ý | |
track liner | ÒѼÓÈë | ±à¼ | ɾ³ý |
translating sleeve skin | The translating sleeve is a nacelle system that consists of the visible surface of the thrust-reverser, the moveable blocker doors, the acoustical treated inner duct and the mechanical connection that is needed to operate the thrust-reverser doors. FACC develops and manufactures innovative translating sleevesFACC is a partner of Goodrich Aerostructures in the development and fabrication of the translating sleeves for the Boeing 787 and Airbus A350. In the development of the translating sleeves FACC combines proven technologies with completely new design aspects. The carbon fiber component consists of the visible surface of the thrust-reverser, the moveable blocker doors, the acoustical treated inner duct and the mechanical connection that is needed to operate the thrust-reverser doors. A newly developed, double-degree acoustic surface, with the Boeing 787 used for the first time on an airplane, marks an important technology jump. In this process a wider frequency band will be covered by including two noise reduction ranges and the noise will additionally be reduced by two steps. The acoustic surfaces are the result of numerous tiny drillings - 1.8 million per engine - through which the sound waves can penetrate into the sandwich area and be confined, and broken into a number of small sound waves. In the thrust-reverser of the 787 engines, the acoustic surfaces will cover over 80% of the surface. As a comparison, in the present state-of-the-art technology, this percentage is between 60 and 70%. The Boeing 787 will be the first plane with an undulated engine nozzle (chevron). The wave shape at the end of the engine allows the hot air coming from the engine to mix easier with the cold outside air. As a result, the noise level is considerably reduced for the passengers inside the cabin.[attach]3101[/attach] | ±à¼ | ɾ³ý |
õºì | ÒѼÓÈë | ±à¼ | ɾ³ý |
30QJ1 | ±à¼ | ɾ³ý | |
accumlate | ±à¼ | ɾ³ý | |
bullnose seal | ±à¼ | ɾ³ý | |
configurations | ±à¼ | ɾ³ý | |
CONTR. | ±à¼ | ɾ³ý | |
CONTR.COMP. | ±à¼ | ɾ³ý | |
flap configuration | ÒѼÓÈë | ±à¼ | ɾ³ý |
flap configurations | ±à¼ | ɾ³ý | |
grid pattern | ÒѼÓÈë | ±à¼ | ɾ³ý |
HIGH LVL | ±à¼ | ɾ³ý | |
hinge beam | ±à¼ | ɾ³ý | |
identified | ±à¼ | ɾ³ý | |
inner wall | ÒѼÓÈë | ±à¼ | ɾ³ý |
innerwall | ±à¼ | ɾ³ý | |
latch beam | ±à¼ | ɾ³ý | |
QJ | ±à¼ | ɾ³ý | |
randrom | ±à¼ | ɾ³ý | |
rejiect | ±à¼ | ɾ³ý | |
right T/R sleeve | ±à¼ | ɾ³ý | |
rubstrip | ±à¼ | ɾ³ý |
stow position | ÒѼÓÈë | ±à¼ | ɾ³ý |
tension latches | ±à¼ | ɾ³ý | |
translate sleeve | translating sleeveÒѼÓÈë | ±à¼ | ɾ³ý |
ttzl | ±à¼ | ɾ³ý | |
¹«Îï²Õ | ±à¼ | ɾ³ý |
[size=-1]chuapter | ±à¼ | ɾ³ý | |
engine strut | ÒѼÓÈë | ±à¼ | ɾ³ý |
FLIGHT CREW LIGHTS | ±à¼ | ɾ³ý | |
fuel-fed | ±à¼ | ɾ³ý | |
lamp p-6 PNL DOME LZGHT | ±à¼ | ɾ³ý | |
undercowl | ±à¼ | ɾ³ý | |
È¥ÃÀ¹úµÄº½°à¼´½«Æð·É | ±à¼ | ɾ³ý |
Barcol | ÒѼÓÈë | ±à¼ | ɾ³ý |
compresses | ±à¼ | ɾ³ý | |
concerns | ±à¼ | ɾ³ý | |
consulation | ÒѼÓÈë | ±à¼ | ɾ³ý |
EFFECT FROM TO | ±à¼ | ɾ³ý | |
engineers | ±à¼ | ɾ³ý | |
in force | ÒѼÓÈë | ±à¼ | ɾ³ý |
insept | ±à¼ | ɾ³ý | |
installaton | ±à¼ | ɾ³ý | |
maintenance log | ÒѼÓÈë | ±à¼ | ɾ³ý |
maintence | ±à¼ | ɾ³ý | |
mfgr | ±à¼ | ɾ³ý | |
norn | ±à¼ | ɾ³ý | |
rejected take-off test | ±à¼ | ɾ³ý | |
system synoptics | ÒѼÓÈë | ±à¼ | ɾ³ý |
undercowl | ±à¼ | ɾ³ý | |
Variations in temperature cause differences of air density and therefore differences in weight and pressure of the air. | ±à¼ | ɾ³ý | |
ÓÐЧºÅ | ÓÐЧ£«ºÅ | ±à¼ | ɾ³ý |
accesss door removed | ±à¼ | ɾ³ý | |
ato-restow | ÊÇauto-restow£¬ÒѼÓÈë | ±à¼ | ɾ³ý |
control the thrust reverser auto-restow operatio | ±à¼ | ɾ³ý | |
flanges | ±à¼ | ɾ³ý | |
inner wall | ÒѼÓÈë | ±à¼ | ɾ³ý |
P5 | ±à¼ | ɾ³ý | |
restow | ÒѼÓÈë | ±à¼ | ɾ³ý |
REVERSER Lights | ±à¼ | ɾ³ý | |
screws. | ±à¼ | ɾ³ý | |
the engine accessory unit has these functions | ±à¼ | ɾ³ý | |
TROUBIE | ±à¼ | ɾ³ý | |
TROUBIE-shooting | ±à¼ | ɾ³ý | |
v-blade | ±à¼ | ɾ³ý | |
weld-machining-tool | ±à¼ | ɾ³ý |
dents | ±à¼ | ɾ³ý | |
EE COMPARTMENT | ±à¼ | ɾ³ý | |
furrle | ±à¼ | ɾ³ý | |
hydraulic link | ÒѼÓÈë | ±à¼ | ɾ³ý |
inner liner | ÒѼÓÈë | ±à¼ | ɾ³ý |
LOOKING AFT | ±à¼ | ɾ³ý | |
sliders | ±à¼ | ɾ³ý | |
SPARKS, | ±à¼ | ɾ³ý |
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