Fix of LOC/GS scale flickering when LOC/GS capture.
[fg:toms-fgdata.git] / Aircraft / 777 / 777-200LR.xml
1 <!--777-200 LR yasim
2
3 The 777-200LR ("LR" for Longer Range), the C-market model, became the world's longest-range commercial airliner when it entered service in 2006.Boeing named this aircraft the Worldliner, highlighting its ability to connect almost any two airports in the world. It holds the world record for the longest nonstop flight by a commercial airliner, and has a maximum range of 9,380 nautical miles (17,370 km). The ∁E00LR was intended for ultra-long-haul routes such as Los Angeles to Singapore.
4
5 Developed alongside the ∁E00ER, the ∁E00LR features an increased MTOW and three optional auxiliary fuel tanks in the rear cargo hold. Other new features include raked wingtips, redesigned main landing gear, and additional structural strengthening. As with the ∁E00ER and 777F, the ∁E00LR is equipped with wingtip extensions of 12.8 ft (3.90 m). The -200LR is powered by GE90-110B1 or GE90-115B turbofans. The first ∁E00LR was delivered to Pakistan International Airlines on February 26, 2006.As of July 2011, nine different ∁E00LR customers have taken delivery of 52 aircraft, with 3 unfilled orders. Airlines operated 48 of the -200LR variant as of July 2011. The closest competing aircraft from Airbus is the A340-500HGW.
6
7 (Taken from the Wikipedia)
8
9 777-200LR - Range with 301 passengers 17,3957km (9,395nm) - 19hrs.
10
11 Wing span: 64.8m
12 Length: 63.7 m
13 Tail Height: 18.6m
14 Diameter : 6.19 m
15 Max Fuel :53,515 US gal
16 Max TO weight: 766,000 lbs
17 Max Landing weight: 492,000 lbs
18 -->
19
20 <airplane mass="326000">
21
22   <!-- Approach configuration -->
23   <approach speed="132" alt="0.0" aoa="5.0" fuel="0.2" glide-angle="0.0">
24       <control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.25"/>
25       <control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.25"/>
26       <control-setting axis="/controls/flight/flaps" value="1"/>
27       <control-setting axis="/surface-positions/slats" value="1"/>
28       <control-setting axis="/controls/gear/gear-down" value="1"/>
29       <solve-weight idx="0" weight="360"/>
30       <solve-weight idx="1" weight="42072"/>
31   </approach>
32
33   <!-- Cruise configuration -->
34   <cruise speed="512" alt="35000" fuel="0.8" glide-angle="0.0">
35       <control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.95"/>
36       <control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.95"/>
37       <control-setting axis="/controls/flight/flaps" value="0.0"/>
38       <control-setting axis="/controls/gear/gear-down" value="0"/>
39       <solve-weight idx="0" weight="360"/>
40       <solve-weight idx="1" weight="42072"/>
41   </cruise>
42
43   <cockpit x="22.8" y="0.5" z="0.75"/>
44
45   <fuselage ax="25.36" ay="0" az="-0.64" bx="16.231" by="0.00" bz="0.0"
46       width="6.2" taper="0.0" midpoint="1.0"/>
47   <fuselage ax="16.231" ay="0" az="0" bx="-20.0" by="0.00" bz="0.0"
48       width="6.2" taper="1.0" midpoint="0.5"/>
49   <fuselage ax="-20.0" ay="0" az="0" bx="-37.0" by="0.00" bz="1.2"
50       width="6.2" taper="0.0" midpoint="0.0"/>
51   <fuselage ax="4.0" ay="9.8" az="-3" bx="-1.8" by="9.8" bz="-3"
52       width="3.8" taper="1.0"/>
53   <fuselage ax="4.0" ay="-9.8" az="-3" bx="-1.8" by="-9.8" bz="-3"
54       width="3.8" taper="1.0"/>
55
56   <wing x="-0.0" y="3.095" z="-1.66" length="31.6" chord="12.8" sweep="32"
57         taper="0.15" dihedral="7" camber="0.01" incidence="2" twist="-2">
58       <stall aoa="16" width="6" peak="1.5"/>
59       <flap0 start="0" end=".56" lift="1.5" drag="1.7"/>
60       <flap1 start=".64" end=".88" lift="1.5" drag="1.2"/>
61       <slat start="0" end="1" aoa="2" drag="1"/>
62       <spoiler start="0.2" end="0.6" lift="0.2" drag="2.0"/>
63       <control-input axis="/controls/flight/flaps" control="FLAP0"/>
64       <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
65       <control-input axis="/surface-positions/flap-pos-norm" control="SLAT"
66                      src0="0" dst0="0" src1="0.1428" dst1="1.0"/>
67       <control-output control="SLAT" prop="/surface-positions/slats"/>
68       <control-speed control="FLAP0" transition-time="78"/>
69       <control-input axis="/controls/flight/speedbrake" control="SPOILER"/>
70       <control-output control="SPOILER" prop="/surface-positions/speedbrake-norm"/>
71       <control-speed control="SPOILER" transition-time="2"/>
72       <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
73       <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
74       <control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-pos-norm"/>
75       <control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-pos-norm"/>
76   </wing>
77
78   <hstab x="-31.0" y="1.5" z="1.0" chord="6.0" length="10.84" taper=".20"
79          sweep="28" dihedral="7" camber="0.0">
80     <stall aoa="18" width="5" peak="1.5"/>
81     <flap0 start="0" end="1" lift="1.4" drag="1.2"/>
82     <control-input axis="/controls/flight/elevator" control="FLAP0"/>
83     <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
84     <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
85   </hstab>
86
87   <vstab x="-30.0" y="0.00" z="2.7" chord="8.0" length="12.2" taper="0.3"
88          sweep="33">
89     <stall aoa="14" width="5" peak="1.5"/>
90     <flap0 start="0" end="1" lift="1.4" drag="1.2"/>
91     <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
92     <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
93     <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
94                     min="1" max="-1"/>
95   </vstab>
96
97 <!-- General Electric GE90-115B
98
99
100 General characteristics
101
102     Type: axial flow, twin-shaft, bypass turbofan engine
103     Length: 287 in (7,290 mm)[14]
104     Diameter: overall: 135 in (3.429 m);[14] fan: 128 in (3.251 m)
105     Dry weight: 18,260 lb (8,283 kg)[14]
106
107 Components
108
109     Compressors: axial: 1 wide chord swept fan, 4 low pressure stages, 9 high pressure stages
110     Turbines: axial: 6 low pressure stages, 2 high pressure stages
111
112 Performance
113
114     Maximum thrust: max at sea level: 115,540 lbf (514 kN) ; world record set at 127,900 lbf (568,9 kN) 827 feet above sea level
115     Overall pressure ratio: 42:1
116     Thrust-to-weight ratio: approx. 6.3:1
117
118
119 -->
120
121   <jet x="1.16" y="9.89"  z="-2.995" mass="18260" thrust="115540" spool-time="3"
122        egt="840" tsfc="0.23 " epr="40" n1-idle="18.5" n1-max="110.5" n2-idle="70" n2-max="107">
123     <control-input axis="/controls/engines/engine[0]/throttle-lever" control="THROTTLE"/>
124     <control-input axis="/controls/engines/engine[0]/reverser" control="REVERSE_THRUST"/>
125     <control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[0]"/>
126     <control-speed control="REVERSE_THRUST" transition-time="4"/>
127     <actionpt x="-2.7" y="9.89" z="-2.995"/>
128   </jet>
129
130   <jet x="1.16" y="-9.89"  z="-2.995" mass="18260" thrust="115540"  spool-time="3"
131        egt="840" tsfc="0.23" epr="40" n1-idle="18.5" n1-max="110.5" n2-idle="70" n2-max="107">
132     <control-input axis="/controls/engines/engine[1]/throttle-lever" control="THROTTLE"/>
133     <control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST"/>
134     <control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[1]"/>
135     <control-speed control="REVERSE_THRUST" transition-time="4"/>
136     <actionpt x="-2.7" y="-9.89" z="-2.995"/>
137   </jet>
138
139   <!-- nose -->
140   <gear x="19.28"  y="0.00" z="-5.55"
141         compression="0.7" spring="1.2" damp="1" sfric="1.5" dfric="1.0">
142     <!-- up to 70 degrees max steering angle with tiller, input is limited to 7 degrees with rudder (see Nasal/ground_steering.nas) -->
143     <control-input control="STEER" axis="/controls/gear/nosegear-steering-cmd-norm" src0="-1.0" dst0="-1.2217304764" src1="1.0" dst1="1.2217304764" />
144     <control-output control="STEER" prop="/controls/gear/nosegear-steering-angle-rad" />
145     <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
146     <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
147     <control-speed control="EXTEND" transition-time="19"/>
148   </gear>
149
150   <gear x="-6.39" y="5.6" z="-5.7" compression="0.8" spring="1.0" sfric="1" dfric="0.9">
151     <control-input axis="/autopilot/autobrake/left-brake-output" control="BRAKE"/>
152     <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
153     <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
154     <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
155     <control-speed control="EXTEND" transition-time="20"/>
156   </gear>
157
158   <gear x="-6.39" y="-5.6" z="-5.7" compression="0.8" spring="1.0" sfric="1" dfric="0.9">
159     <control-input axis="/autopilot/autobrake/right-brake-output" control="BRAKE"/>
160     <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
161     <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
162     <control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
163     <control-speed control="EXTEND" transition-time="20"/>
164   </gear>
165
166   <!-- aft axle on left main gear -->
167   <gear x="-7.8" y="5.6" z="-6.22" compression="3.0" spring="1.2" >
168     <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
169     <control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/>
170     <control-speed control="EXTEND" transition-time="20"/>
171     <!-- 8 degrees main gear steering when nose gear steering above 13 degrees commanded (see Nasal/ground_steering.nas) -->
172     <control-input control="STEER" axis="/controls/gear/maingear-steering-cmd-norm" src0="-1.0" dst0="-0.1396263402" src1="1.0" dst1="0.1396263402" />
173     <control-output control="STEER" prop="/controls/gear/maingear-l-steering-angle-rad" />
174   </gear>
175
176   <!-- aft axle on right main gear -->
177   <gear x="-7.8" y="-5.6" z="-6.22" compression="3.0" spring="1.2">
178     <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
179     <control-output control="EXTEND" prop="/gear/gear[4]/position-norm"/>
180     <control-speed control="EXTEND" transition-time="20"/>
181     <!-- 8 degrees main gear steering when nose gear steering above 13 degrees commanded (see Nasal/ground_steering.nas) -->
182     <control-input control="STEER" axis="/controls/gear/maingear-steering-cmd-norm" src0="-1.0" dst0="-0.1396263402" src1="1.0" dst1="0.1396263402" />
183     <control-output control="STEER" prop="/controls/gear/maingear-r-steering-angle-rad" />
184   </gear>
185
186 <!--Fuel 
187
188 Maximum Fuel Capacity   Basic - 47,890 U.S. gallons
189 (181,280 L)
190 With three optional fuel tanks -
191 53,515 U.S. gallons (202,570 L) 
192
193 Source: http://www.boeing.com/commercial/777family/pf/pf_lrproduct.html
194
195 -->
196
197   
198   <tank x="-4.3" y="5" z="-1.5" jet="true" capacity="70475"/>
199   <tank x="-4.3" y="0" z="-2.5" jet="true" capacity="180870"/>
200   <tank x="-4.3" y="-5" z="-1.5" jet="true" capacity="70475"/>
201
202   <tank x="-4.3" y="1" z="-8" jet="true" capacity="12600"/>
203   <tank x="-4.3" y="0" z="-9.5" jet="true" capacity="12600"/>
204   <tank x="-4.3" y="-1" z="-8" jet="true" capacity="12600"/>
205
206
207
208   <weight x="22.0" y="0" z="0" mass-prop="/sim/weight[0]/weight-lb"/>
209   <weight x="-4.3" y="0" z="0" mass-prop="/sim/weight[1]/weight-lb"/>
210
211   <ballast x="-30" y="0" z="4" mass="-40000"/>
212
213   <thruster x="19.28"  y="0.00" z="-5.55" vx="1" vy="0" vz="0" thrust="20000">
214     <control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE"
215                    src0="-1" src1="1" dst0="-1" dst1="1"/>
216   </thruster>
217
218 </airplane>