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ITS » Non Degree » Teknik Mesin - D3
Posted by fandikaaqsa@its.ac.id at 28/04/2016 10:34:27  •  1163 Views


PERHITUNGAN BEBAN PENDINGIN PADA KABIN PESAWAT AIRBUS 330-300

THE CALCULATION OF COOLING LOAD ON CABIN AIRBUS 330-300

Author :
HERVIANDO ARYO K.W ( 2111030001 )




ABSTRAK

Definisi pengkondisian udara yang nyaman comfort air conditioning adalah proses perlakuan terhadap udara untuk mengatur suhu kelembaban kebersihan dan pedistribusiannya secara serentak guna mencapai kondisi nyaman yang di butuhkan oleh penghuni yang berada di dalamnya oleh karena itu pesawat terbang memerlukan system pengkondisian udara karena ketika semakin tinggi kita terbang temperature dan tekanan udara sekitar akan semakin rendah. Suatu pesawat yang sedang terbang dengan ketinggian sekitar 8000 sampai 10000 m tekanan temperatur dan kelembaban adalah sangat jauh berbeda dengan keadaan jika kita di darat. Tujuan yang ingin dicapai dalam tugas akhir ini adalah untuk mencapai tingkat kenyamanan penumpang pesawat yang telah ditentukan oleh Federal Aviation Regulation FAR dengan menghitung beban total pendinginan yang ada pada pesawat Airbus 330 300 pada 2 keadaan yang berbeda yaitu Ground idle dan maximum cruise. Pada tugas akhir ini didapatkan perhitungan grand total heat berdasarkan penjumlahan cooling load Q dari atap dinding kaca lantai radiasi sinar matahari yang melalui kaca jumlah lampu jumlah penumpang dan peralatan elektronik yang menghasilkan panas. Serta adapun factor lain yang berpengaruh pada perhitungan ini adalah dimensi pesawat jam keberangkatan bulan keberangkatan dan tujuan keberangkatan.


ABSTRACT

Definition of comfortable air conditioning is the process of air treatment to control temperature humidity cleanliness and the distribution is simultaneously in order to achieve comfortable conditions that needed by residents inside therefore an aircraft requires air conditioning system because when the higher we fly the temperature and pressure of the surrounding air would be lower. An aircraft in flight with elevation about 8000 to 10000 m pressure temperature and humidity is very different from the situation on the ground. Objectives to be achieved in this final project is to achieve the level of comfort of airline passengers that have been determined by the Federal Aviation Regulations FAR by calculate the total cooling load on the Airbus 330-300 on two different conditions that is ground idle and maximum cruise In this final project grand total calculation of heat obtained by the summary of cooling load Q of the roof walls glass floors solar radiation through glass number of lights number of passengers and electronic equipment that generates heat.



KeywordsBeban pendingin; ground idle; maximum cruise; grand total heat
 
Subject:  Mesin pendingin
Contributor
  1. Ir. Denny M.E. Soedjono, MT
Date Create: 28/04/2016
Type: Text
Format: PDF
Language: Indonesian
Identifier: ITS-NonDegree-21002160001395
Collection ID: 21002160001395
Call Number: RSM 621.564 Her p


Source
Non Degree of Machine Engineering, RSM 621.564 Her p, 2014

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Copyright @2016 by ITS Library. This publication is protected by copyright and per obtained from the ITS Library prior to any prohibited reproduction, storage in a re transmission in any form or by any means, electronic, mechanical, photocopying, reco For information regarding permission(s), write to ITS Library




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  1.  ITS-NonDegree-41390-2111030001-abstract_en.pdf - 298 KB
  2.  ITS-NonDegree-41390-2111030001-conclusion.pdf - 375 KB




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