[PDF] Searches related to qantas a380 model plane filetype:pdf





Previous PDF Next PDF



In-Flight Uncontained Engine Failure Airbus A380-842

https://www.atsb.gov.au/media/4173625/ao-2010-089_final.pdf



Strong pre-order programme drives growth in inflight retail sales for

04.04.2008 direct order from the www.qantas.com website. Purchases of model planes by aviation buffs sustain this category and the new A380 plane ...



EN-Airbus-A380-Facts-and-Figures-Dec-2021

01.12.2021 re-investing millions Euros in their planes to upgrade their cabin for passenger comfort. (todate Singapore Airlines Qantas and Emirates).



Untitled

LIST OF AUTHORISED MEDICAL SUPPORT EQUIPMENT ON QANTAS. A330 A380



2020 Qantas Group Data Book

retirement of its 747-400ERs and moved its A380 fleet to long term storage. Jetstar is the Qantas Group's low-cost airline brand. It is.



Aircraft cabin water leak event involving an Airbus A380 VH-OQD

15.10.2014 On 2 July 2014 a Qantas Airbus A380 aircraft



2011 Annual Review

A380 Aircraft Maintenance Engineer Nelson Lau Qantas A380 fleet until it was fully confident ... aircraft models such as the Airbus A380.



In-flight uncontained engine failure - overhead Batam Island

04.11.2010 of an engine failure on a Qantas Airbus A380 aircraft over Batam ... approximately 20 NM (37 km) racetrack holding pattern at 7400 ft.



Qantas Airways Limited FY12 Results

23.08.2012 9 x B744 aircraft will be reconfigured with A380 product by October 2012. 3. ... Ancillary revenue model working in all markets.





The Upgraded Qantas Airbus A380 Factsheet

QANTAS AIRBUS A380 NEW CABIN FEATURES AIRBUS A380 FAST FACTS No in fleet: 12 First received: 2008 Wingspan: 79 8 metres Cruising speed: Mach 0 85 Engine thrust: 70000 pounds Maximum take-off weight: 560 tonnes Range at full capacity: 13800 kilometres INFLIGHT ENTERTAINMENT Average flights flown annually per aircraft: 400



Qantas Reintroduces 6th Airbus A380 Amid Capacity Boost

The A380 cabin enables airlines to accommodate 232 more seats (+75 ) than747-400 and 199 more seats (+60 ) than 747-8 in a 4 class layout configuration IFE and Connectivity A single simple and intuitive touch screen interface for cabin crew to control all cabinsystems 4th generation In-Flight Entertainment (IFE) experience



A380 MPD & base maintenance analysis - Aircraft Commerce

T he A380-800 began operational service in October 2007 with Singapore Airlines The oldest A380s are now approaching the end of the first cycle of maintenance inputs covering a 12-year (YE) period The A380 was the first Airbus to enter service on a 24-month (MO) base check interval



Seat Map for the A380-800 Aircraft - 14F/64J/35PY/371Y - Qantas

Title: Seat Map for the A380-800 Aircraft - 14F/64J/35PY/371Y Created Date: 12/19/2016 11:20:22 AM



AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING AC

The A380-800 is a subsonic very long range and very high capacity civil transport aircraft The A380-800 offers several payload capabilities ranging from 400 passengers in a very comfortable multi- class configuration up to 853 passengers in an all economy class configuration



Searches related to qantas a380 model plane filetype:pdf

The Airbus A380 is a double deck wide body four-engine jet air liner manufactured by the European corporation Airbus and a subsidiary of EADS It is the world's largest passenger airliner The A380 was initially offered in two models The A380-800 original configuration carried 555 passengers in a three

How many passengers does a Qantas A380 seat?

    Qantas’ Airbus A380s seat a total of 484 or 485 passengers, depending on the layout. The older configuration, which can be found on VH-OQA, features a smaller premium economy class cabin, and a larger economy class cabin.

Where did a Qantas A380 Airbus land?

    AUCKLAND, NEW ZEALAND - OCTOBER 10: A Qantas A380 Airbus lands at Auckland International Airport watched by hundreds of people on October 10, 2008 in Auckland, New Zealand.

When will the Qantas A380 replace the Boeing 747?

    That 'replacement' timeframe is likely to stretch well into the next decade, however – the first Qantas A380 having arrived in 2008, and by comparison the airline has notched up over 15 years flying some Boeing 747s.

MODELING AND ANALYSIS ON WING OF A380 FLIGHT

N.Anjaneyulu1 *, J. Laxmi Lalitha2,

1 Department of Mechanical Engineering, Bapatla Engineering College, Bapatla, Guntur, India

2 Department of Mechanical Engineering, Bapatla Engineering College, Bapatla, Guntur, India,

ABSTRACT

The A380 is currently the largest aircraft in commercial operation and one of the most advance

planes in the world. The Airbus A380 is a double deck, wide body four-engine jet airliner manufactured

by the European corporation airbus, a subsidiary of Eads. This common design approach sacrifices

some Fuel Efficiency (due to a weight penalty) on the A380-800 passenger model, but Airbus estimates

that the size of the aircraft, coupled with the advances in technology described below, will provide lower

operating costs per passenger than the 747-400 and older 747 variants. In recent years we found minor

cracks on wings of A380. Some of them were related to production. The minor cracks - no more than two

centimeters long - were discovered on some of the wing rib brackets and were caused by a manufacturing

issue and not the turbulence. But inspections found that were related to rib feet .originally the cracks are

in brackets in the middle of the giant wings. In this project an attempt is made in to find the reason for

cracks on the wings. Firstly we made modeling of the entire flight. We modeled wing separately. Later we

made steady state thermal analysis and transient thermal analysis on the wing.

1. INTRODUCTION

The Airbus A380 is a double deck, wide

body, four-engine jet air liner manufactured by the

European corporation Airbus and a subsidiary

of EADS. It is the world's largest passenger airliner. The A380 was initially offered in two models. The A380-800 original configuration carried 555 passengers in a three class configuration or 853 passengers (538 on the main deck and 315 on the upper deck) in a single- class economy configuration. In May 2007 Airbus began marketing a configuration with 30 fewer passengers, (525 total in three classes), traded for

370 km (200 nmi) more range, to better reflect

trends in premium class accommodation.

2. Advanced materials:

While most of the fuselage is

aluminum, composite materials comprise more than 20% of the A380's airframe. Carbon-fiber reinforced plastic, glass-fiber reinforced plastic and quartz-fiber reinforced plastic are used extensively in wings, fuselage sections (such as the undercarriage and rear end of fuselage), tail surfaces, and doors. Newer weld able aluminum alloys are also used. This enables the widespread use of laser beam welding manufacturing techniques, eliminating rows of rivets and resulting in a lighter, stronger structure.

International Journal of Engineering Research & Technology (IJERT)Vol. 1 Issue 6, August - 2012ISSN: 2278-01811www.ijert.org

Fig 1. Conceptual design of A380

Fig. 2 Conceptual design of wing

3. PROBLEM DEFINITION:

wings of a380. In this project we made an attempt to find the reason behind the cracks from design prospective. We made all the analysis using

ANSYS WORKBENCH. We applied varying

pressure between 1Mpa and 1.5Mpa with in temperature 22°C to 35°C. We used aluminum alloy as material. Modeling of Flight and wing was done in CATIA V5 R18. Dimensions of the flight

Wing span: 79.75 m

Overall length72.72 m

Height24.09 m

Table 1. Input Values

MATERIAL Aluminum Alloy

VOLUME 793.55 m³

MASS 2.1981e6kg

No. OF NODES 1381

No. OF ELEMENTS 595

DENSITY 2770. kg/m³

SPECIFIC HEAT 875J/Kg °C

4. TOTAL DEFORMATION:

In the fig 3. We fixed one end and we

applied uniform temperature and we have pressure

1Mpa at top and front end of the wing, 1.5Mpa at

bottom of the wing.

Fig 3. Total deformation

International Journal of Engineering Research & Technology (IJERT)Vol. 1 Issue 6, August - 2012ISSN: 2278-01812www.ijert.org

5. EQUIVALENT STRESS:

In the fig 4. We fixed one end and we

applied uniform temperature and we have pressure

1Mpa at top and front end of the wing, 1.5Mpa at

bottom of the wing.

Fig 4. Equivalent Stress

6. MAXIMUM PRINCIPAL STRESS:

In the fig 5. We fixed one end and we

applied uniform temperature and we have pressure

1Mpa at top and front end of the wing, 1.5Mpa at

bottom of the wing.

Fig 5. Max. Principal Stress

7. MINIMUM PRINCIPAL STRESS:

In the fig 6. We fixed one end and we

applied uniform temperature and we have pressure

1Mpa at top and front end of the wing, 1.5Mpa at

bottom of the wing.

Fig 6 Min. Principal Stress

8. DIRECTIONAL HEAT FLUX:

In the fig 7. We fixed one end and we

applied uniform temperature and we have pressure

1Mpa at top and front end of the wing, 1.5Mpa at

bottom of the wing.

Fig 7 Directional Heat Flux

International Journal of Engineering Research & Technology (IJERT)Vol. 1 Issue 6, August - 2012ISSN: 2278-01813www.ijert.org

9. TRANSIENT THERMAL

ANALYSIS:

Table 2. Input Values

MATERIAL Aluminum Alloy

VOLUME 793.55 m³

MASS 2.1981e6kg

No. OF NODES 1381

No. OF ELEMENTS 595

DENSITY 2770. kg/m³

SPECIFIC HEAT 875J/Kg °C

TEMPERATURE

BETWEEN

22 TO 35°C

10. TOTAL HEAT FLUX:

In the Fig 8. We have given varying

temperature between 35°C to 28°C. with pressure

1Mpa at the front end of the wing.

Fig 8 Total Heat Flux

11. DIRECTIONAL HEAT FLUX:

In the Fig 9. We have given varying

temperature between 35°C to 28°C. with pressure

1Mpa at the front end of the wing

Fig 9 Directional Heat Flux

Structural

Young's Modulus 7.1e+010 Pa

Poisson's Ratio 0.33

Density 2770. kg/m³

Thermal Expansion 2.3e-005 1/°C

Thermal

Specific Heat 875. J/kg·°C

Fig. 10 Aluminum Alloy > Thermal Conductivity

International Journal of Engineering Research & Technology (IJERT)Vol. 1 Issue 6, August - 2012ISSN: 2278-01814www.ijert.org

Fig. 11 Temperature - Global Minimum

Fig. 12 Directional Heat Flux

11. CONCLUSION:

Under the above conditions we got stress

and strain values with in the limiting range. The maximum stresses that wing of a flight can with stand are 700pa. but we got stress 400pa So the wing we have designed is safe.

12. References:

http://en.wikipedia.org/wiki/Airbus_A380 and other websites of a380 and database of other fight designs.

International Journal of Engineering Research & Technology (IJERT)Vol. 1 Issue 6, August - 2012ISSN: 2278-01815www.ijert.org

quotesdbs_dbs22.pdfusesText_28
[PDF] qantas airbus a330 300 seat map

[PDF] qantas flight 32 air crash investigation

[PDF] qatar 2022

[PDF] qatar address format

[PDF] qatar airways annual report 2017

[PDF] qatar airways annual report 2019

[PDF] qatar airways coronavirus

[PDF] qatar airways fleet

[PDF] qatar airways pdf

[PDF] qatar airways strategy

[PDF] qatar civil code english pdf

[PDF] qatar refund policy

[PDF] qbasic 1.1 dosbox download

[PDF] qbasic book pdf download

[PDF] qbasic book pdf free download