A typical helicopter cabin heat load estimation methodology and analysis of aircraft cabin pressure control system (Record no. 237172)

MARC details
000 -LEADER
fixed length control field 01397nam a2200121Ia 4500
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 231221s9999 xx 000 0 und d
041 ## - LANGUAGE CODE
Language code of text/sound track or separate title English
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name Dinakar Aradhya, R.
245 #2 - TITLE STATEMENT
Title A typical helicopter cabin heat load estimation methodology and analysis of aircraft cabin pressure control system
Remainder of title Krishna, V.
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Date of publication, distribution, etc. Jan - May 2019
Name of publisher, distributor, etc. PES University
Place of publication, distribution, etc. Bengaluru
510 ## - CITATION/REFERENCES NOTE
Name of source Helicopters are an essential part of both civil and military activities. In the future, it is expected that a significant increase in the use of this mode of transportation widely. There is a need to maintain the cabin in a good and safe condition so that the passengers and the crew inside the cabin feel comfortable. For a cabin to be maintained in comfort conditions, an efficient environmental control system is to be adapted and in case of an aircraft, cabin pressure control system (CPCS) is needed to depressurize the cabin and maintain constant cabin pressure. Helicopter heat loads are challenging because of their design i.e., more transparent surfaces, heat from the engine (generally mounted on the ceiling) and infiltration effect. Heat load on the cabin must be mitigated through an efficient air cycle system. In this project, helicopter cabin heat load values and mass flow of air required at different altitudes are determined and a heat exchanger for an environmental con
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26/01/2024   CD7286 26/01/2024 Compact Disks       Central Library Central Library   ME/PG RS 1  

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