Projekt klimatizacijskog sustava za održavanje optimalnih mikroklimatskih uvjeta u putničkom zrakoplovu

master's thesis

• Title (english): Design of an air conditioninig system for maintenance of an optimum environmental conditions in civil transportation aircraft
• Author: Željko Mateković
• Mentor: Marino Grozdek (mentor)
• Granter: University of Zagreb; Faculty of Mechanical Engineering and Naval Architecture; Zagreb
• Defense date and country: 2020-12-04, Croatia
• Scientific / art field, discipline and subdiscipline: TECHNICAL SCIENCES; Aviation, Rocket and Space Technology

Abstract

Kod projektiranja modernih putničkih zrakoplova pored sigurnosti, udobnost je jedan od
važnih kriterija koji je potrebno uzeti u obzir. Faktori koji određuju razinu komfora unutar
kabine pod tlakom su mikroklima i temperatura, a koji zajedno tvore unutarnji toplinski režim
kabine pod tlakom. Izračun toplinskog režima kabine pod tlakom prvi je korak u fazama
projektiranja klimatizacijskih sustava zrakoplova. Dobiveni izračunati parametri na osnovu
toplinskog režima kabine pod tlakom služe kao početni podaci pri odabiru klimatizacijskog
sustava, koji mora osigurati normalne uvjete unutar trupa zrakoplova za život posade i putnika
kako u letu tako i na stajanci.
Kako bi se postigli komforni uvjeti za boravak ljudi u trupu zrakoplova, a zavisno od različitih
atmosferskih uvjeta u kojima se nalazi zrakoplov, u daljnjem tekstu su prikazani su izračuni,
norme i preporuke sustava i uređaja za klimatizaciju zrakoplovnih kabina pod tlakom.

Abstract (english)

During the design of modern passenger aircraft in addition to safety, comfort is one of the most
important criteria to consider. The factors that determine the level of comfort inside the
pressurized cabin are the microclimate and temperature, which together form the internal
thermal regime of the pressurized cabin. Calculating the thermal loads of a pressurized cabin is
the first step in the design phases of air conditioning systems. The obtained calculated
parameters based on the thermal loads of the pressurized cabin serve as initial data when
choosing an air conditioning system, which must ensure normal conditions within the fuselage
for the life of the crew and passengers both in flight and in the parking lot.
In order to achieve comfortable conditions for people to stay in the fuselage, and depending on
the different atmospheric conditions in which the aircraft is located, the following calculations,
standards and recommendations of systems and devices for air conditioning of pressurized
aircraft cabins are presented.

• Keywords: temperatura zraka; tlak zraka; toplinsko opterećenje
• Keywords (english): air temperature; air pressure; heat loads
• Language: croatian
• URN:NBN: urn:nbn:hr:235:674268
• Study programme: Title: Aeronautical Studies; Study programme type: university; Study level: graduate; Academic / professional title: magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva (magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva)
• Type of resource: Text
• File origin: Born digital
• Access conditions: Open access
• Created on: 2020-11-27 06:22:05