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Design and Analysis of Different Types of Aircraft Radome Special Issue - 2015 International Journal of Engineering Research & Technology (IJERT) ISSN: 2278-0181 NCRAIME-2015 Conference Proceedings Design and Analysis of Different Types of Aircraft Radome Denish Davis#1, Francis Mathew#2, Jamaludheen. K.P#3 ,N. Seenivasaraja*4, Karthikeyan. A$5 #UG Students,*Asst.Proffessor, , $Asso.Professor Department of Aeronautical engineering, Excel engineering college, Komarapalayam, Namakkal, Tamilnadu-637303 Abstract-Radome is an expression built from radar and dome. a wide variety of Radome types, and they can be placed on It is a cover or enclosure in order to protect radar antennas different parts of the aircraft, making its design different from environmental influences. Radome is a protection for the for each case. For example, most common large aircraft antenna against the environment such as dust, rain etc. For radomestypically form the nose or tail cone of the aircraft, different aircraft the size, shape and material of the radome or they can be flush mounted or sited on theleading or will be different. In this paper different aircraft radomes are drawn in CATIA V5 and they have analysed in ANSYS 12 trailing edges of a wing, fuselage or tail fin. This project is with different pressure acting on it and with different about various aircraft radomelocated in front of the aircraft material properties. From the analysis that have been done which houses a radar system. The conception of such a unit can be concluded that, which material can sustain high is subjected to electrical requirements of the radar such as pressure according to its shape high transmission, low reflection, far-field radiation pattern, power transmittance, low absorption and small Key words-cover or enclouser to protect the antenna, different bore sight errors among others. The word radomeis a aircraft size and shape will be different. portmanteau of the words radar and dome. So a radome is a dome which covers the radar to protect the antenna INTRODUCTION assembly from environmental hazards. The cover of a radar A radome is a structural, weatherproof enclosure sensor builds a very important part of the sensor and can that protects a microwave (e.g. radar) antenna. The radome have an important influence on sensitivity, radiated antenna is constructed of material that minimally attenuates the pattern and immunity to vibrations. Radome design means electromagnetic signal transmitted or received by the minimizing microwave reflection at the surface of the antenna. In other words, the radome is transparent to radar cover. Poor radome layout can even cause unwanted or radio waves. Radomes protect the antenna surfaces from sensitivity on the backside of the sensor. The cover weather and conceal antenna electronic equipment from material can act as a lens and focus or disperse the radar public view. They also protect nearby personnel from being waves. This is why it should have a constant thickness accidentally struck by quickly rotating antennas. Radomes within the area used for transmission. In an airborne can be constructed in several shapes (spherical, geodesic, application the aerodynamically designed radome is planar, etc.) depending upon the particular application subject to in-flight damage from bird strikes, erosion, using various construction materials (fiberglass, PTFE- precipitation static, thunderstorm electric fields, lightning coated fabric, etc.). When found on fixed-wing aircraft with strikes, delamination, water ingression, and particle damage forward-looking radar (as are commonly used for object or such as hail or debris on the tarmac. The scope of this weather detection), the nose cones often additionally serve project is to present a complete radome design using catia as radomes. On rotary-wing and fixed-wing aircraft using V5, studying material options, analysing and determining a microwave satellite for beyond-line-of-sight wide range of mechanical loads, using ANSYS to finish communication, radomes often appear as blisters on the with structural verifications, as bird impact numerical fuselage. In addition to protection, radomes also streamline analysis and mechanical material testing. the antenna system, thus reducing drag. A radome is often used to prevent ice and freezing rain from accumulating TYPES / CLASSES / STYLES directly onto the metal surface of antennas. In the case of a Radomes for use on flight vehicles, surface vehicles spinning radar dish antenna, the radome also protects the and fixed ground installations are classified into various antenna from debris and rotational irregularities due to categories according to MIL-R-7705B. Categories are wind. Its shape is easily identified by its hard-shell, which determined by the specific radome use and wall has strong properties against being damaged. The basic construction. Customer satisfaction is met by the following, function of a radome is to form a protective cover between Type’s definitions an antenna and the environment with minimal impact to the Type I: low frequency radomes at or below 2 electrical performance of the antenna. This improves GHz. system availability since the antenna is not affected by Type II: Directional guidance radomes having winds, rain or ice. It also provides a stable environment for specified directional accuracy and requirements. service personnel from harsh weather conditions. There are Volume 3, Issue 26 Published by, www.ijert.org 1 Special Issue - 2015 International Journal of Engineering Research & Technology (IJERT) ISSN: 2278-0181 NCRAIME-2015 Conference Proceedings Bore sight error (BSE), bore sight error slope B. Beam Deflection (BSES), antenna pattern distortion and antenna Beam deflection, also known as bore sight error, is side lobe degradation. the shift of the main-lobe electrical axis due to the presence Type III: narrowband radomes with an operational of the radome. bandwidth less than 10%. Type IV: multiple frequency band radomes used at C. Pattern Distortion two or more narrow frequency bands. Pattern distortion due to the presence of an Type V: broadband radomes generally providing incorrectlyrepaired radome can cause changes in the main- an operational bandwidth between 0.100GHz and lobe beam widths, null depths and the structure of the side 0.667GHz. lobes. Type VI: very broadband radomes that provide and operational bandwidth greater than 0.667GHz. D. Reflected Power Reflected power can cause degradation of the pattern Style definitions and raise side lobe levels. It can also cause frequency Radome styles are defined according to the dielectric pulling of a magnetron. wall construction. There are 5 basic styles. • Style A: Half wave wall solid (monolithic). Mechanical Characteristics • Style B: Thin wall monolithic with a wall thickness equal The basic purpose of using a radome is to protect to or less than 0.1 wavelengths at the highest operating an antenna from its environment. It is required to frequency. withstand the various environmental effects like wind, • Style C: A-Sandwich multi-layered wall. Consisting of hail , snow , ice , sand , lightning ,and in the case of three layers two high density skins and a low density core. high speed airborne applications ,thermal erosion and The dielectric constant of the skins is greater than the aerodynamic effects. In fact, these environmental dielectric constant of the core material. 0.25 wavelengths. factors determine the mechanical design requirements • Style D: Multi layered wall having 5 or more dielectric of radome. In meeting these requirements there is no layers. Odd number of high density layers and an even option but to compromise the desire for ideal electro number of low density core layers. As the number of layers magnet transparency of the radome , because the is increased, the broadband frequency performance is mechanical and electrical requirements are often in improved. conflict. As leader man points out , when the • Style E: Other radome wall constructions not fitting into mechanical specifications are severe (like in high- the above style definitions. Including the B-Sandwich speed airborne radars) , it is difficult to find a design consisting of two low density skins and a high density core. that meets satisfactorily both mechanical and electrical Dielectric constant of the skins is less than the dielectric requirements. Unless such circumstances , it may be constant of the core. necessary to relax the electrical specifications to some extent. The five important mechanical requirements of RADOME CHARACTERISTICS radome are as follows: Strength: To sustain the aerodynamic and It has been well-known for some time that the handling loads presence of a radome can affect gain, beam width, side lobe Stiffness: To provide elastic stability. level, and the direction of the bore sight, or pointing Temperature resistance: To tolerate extreme direction of a radar antenna. The radome characteristics are conditions in flight and on ground. classified in to, Resistance to moisture absorption: To keep the Electrical Characteristics material property constant. Mechanical Characteristics Abrasion and Erosion resistance: To reduce the effects of rain , hailstorm, dust , stone etc. Electrical Characteristics The electrical-performance characteristicsare RADOME MATERIALS quantified in terms of transmission loss, beam deflection, pattern distortion and reflected power. Materials used in the construction of radomes include fiberglass, quartz, graphite and Kevlar. A. Transmission Loss Resins include polyester, vinyl ester, cyanate
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