Browse > Article
http://dx.doi.org/10.12673/jant.2014.18.5.445

Considering the Multi-Purpose Display Designed for Aircraft Lightning Protection  

Cheon, Young-Ho (Avionics R&D Lab LIGNex1 Co., Ltd.)
Lee, Seoung-Pil (Avionics R&D Lab LIGNex1 Co., Ltd.)
Park, Jun-Hyeon (Avionics R&D Lab LIGNex1 Co., Ltd.)
Publication Information
Journal of Advanced Navigation Technology / v.18, no.5, 2014 , pp. 445-454 More about this Journal
Abstract
In this paper, we introduce measures designed content for RTCA DO-160 F, Section 22 tests performed to verify the effects of indirect lightning and testing process of the test was carried out in the multi-purpose display certification process. This is referred to as indirect effects of lightning capability of an aircraft having electrical electronic equipment failure or damage to bring lightning induced voltages. In order to protect the avionics from lightning indirect effects of these aircraft are analyzing the effects of lightning strikes on aircraft and aircraft systems and interior design needs protection against the threat on their part. In this paper, we introduce RTCA DO-160 F, component selection process according to Section 22 category selection method and the selected level for determining the level of such measures for protection against lightning of multipurpose display for this aircraft. It also introduces the actual test process to confirm that the designed effectiveness of the selected part. We expect a good example of the lightning planned for future development of measures designed avionics through each step of the process introduced this.
Keywords
Indirect lightning Test; RTCA DO-160 F Section22; Lightning protection; Pin injection test; Cable induction test;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
1 Radio Technical Commission for Aeronautics Inc : RTCA/DO-160F, Environmental Conditions and Test Procedures for Airborne Equipment, Section22 Lightning Induced Transient Susceptibility, RTCA, Inc : 1828 L Street, NW Suite 805 Washington, DC 20036, pp. 22_21-22_38 , Dec. 2007.
2 Federal Aviation Administration, Protection of aircraft electrical/electronic systems against the indirect effects of lightning, Technical Report AC 20-136A, pp. 4-14, Mar. 1990.
3 C. Bosco, Certification issues for electrical and/or electronicengine controls, Society of Automotive Engineers, Warrendale: PA, Technical Paper 871844, 1987.
4 F. A. Fisher and J. A. Plumer, Aircraft Lightning protection Handbook, Pittsfield, MA: Lightning Technologies Incorporated, Sept 1989.
5 M. A. Uman and V. A. Rakov, "The interaction of lightning with airborne vehicles," Progress in Aerospace Sciences, Vol. 39, Issue 1, pp. 3-22, Jan. 2003.
6 M. A. Uman and V. A. Rakov, "Natural and artificially Initiated Lighting," Sciences, Vol. 246, No. 4929, pp. 457-464, Oct. 1989.   DOI
7 Society of Automotive Engineers : SAE Aerospace Standard 8034A, Minimum Performance Standard for Airborne Multipurpose Electronic Displays, pp. 28, Jul. 2005.
8 S. H. Han, "Avionics and authentication techniques for the indirect effects of lightning system," The Magazine of the Institute of Electronics Engineers of Korea , Vol. 31, No. 12, pp. 96-106, Dec. 2004.
9 S. H. Han, J. H. Lee, "Effects of lightning strikes on aircraft airworthiness certification," Journal of The Korean Society for Aeronautical & Space Sciences, Vol. 31, No. 9, pp. 110-120, Nov. 2003.
10 On Semiconductor Components Industries, LLC. Transient Overvoltage Protection [Internet].Available: http://www.onsemi.com/PowerSolutions/search.do?queryTND335-D¶m1=type¶m1_val=document¶m2=doc_type¶m2_val=White Papers