• Title/Summary/Keyword: compound drone

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Flying-wing Type Compound Drone Design and Mission Accuracy Analysis (전익기형 복합드론의 설계 및 임무 정확도 연구)

  • Sung, Dong-gyu;Koh, Eun-hak;Kim, Ju-chan;Nam, Yong-hyeon;Lee, Jeong-ho;Lee, Jae-seung;Lee, Chan-bin;Jeon, Yeong-bae;Choi, Cheol-kyun;Lee, Jae woo
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.26 no.4
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    • pp.122-128
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    • 2018
  • A compound drone that combines a fixed wing and a rotary wing is an aircraft that can take off and landing vertically, and can increase flight time and fly faster with fixed wings. The compound drones are divided into many types depending on the method of adding the thrust vectoring or the lift fan and the position of the rotor. In this study, we designed and fabricated a composite drone with four V-TOL motors in a fixed-wing, and assigned missions to the aviation body, hence judged mission accuracy using the actual flight test. The design process and the mission evaluation process employed in this study can be utilized on the development of various unmanned aerial vehicle.

Analysis of Nutritional Compounds and Antioxidant Effect of Freeze-Dried powder of the Honey Bee (Apis mellifera L.) Drone (Pupal stage) (서양종 꿀벌(Apis mellifera L.) 수벌번데기 동결건조 분말의 영양학적 성분 및 항산화 효과)

  • Kim, Jung-Eun;Kim, Do-Ik;Koo, Hui-Yeon;Kim, Hyeon-Jin;Kim, Seong-Yeon;Lee, Yoo-Beom;Kim, Ji-Soo;Kim, Ho-Hyuk;Moon, Jae-Hak;Choi, Yong-Soo
    • Korean journal of applied entomology
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    • v.59 no.3
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    • pp.265-275
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    • 2020
  • In this study, we analyzed the nutritional ingredients of drone pupae (16th to 20th instar old) to evaluate the value of bee products and provide basic data for product diversification, and the extracts prepared using these pupae were tested for physiological activity. According to the analysis of the general ingredients of the freeze-dried powder of these bee pupae, the moisture, crude protein, crude fat, and crude ash was 1.69 ± 0.07%, 48.52 ± 0.20%, 23.41 ± 0.14%, and 4.05 ± 0.02%, respectively. Vitamin C and vitamin E were 14.92 ± 0.52 mg/100 g and 6.06 ± 0.11 mg α-TE/100 g, respectively. Regarding minerals, the highest content of K (1349.13 ± 34.57 mg/100 g) and P (1323.55 ± 43.85 mg/100 g) was observed and Ca and Fe were 55.43 ± 1.51 mg/100 g and 5.49 ± 0.19 mg/100 g, respectively. The fatty acids of the water extracted freeze-dried pupae powder accounted for approximately 59.62 of saturated fatty acids and 40.38 of unsaturated fatty acids, and high-quality fatty acids such as palmitic acid (C16:0) was 35.49 ± 0.08 and oleic acid (C18:1, n-9) was 35.91 ± 0.22 (g/100 g total fatty acids). The total amino acid content was 38.99 ± 2.63 g/100 g and the free amino acid was a total of 5129.04 mg/100 g, of which 1257.68 mg/100 g was proline and 759.12 mg/100 g glutamic acid. The DPPH (1,1-diphenyl-2-picrylhydrazyl) radical scavenging activity of the drone pupae extract showed values of 0.8 for distilled water extract, 3.2 for 50% EtOH extract, 6.4 for 70% EtOH extract, and approximately 90% for 32 ㎍/mL for 100% EtOH extract. These results suggest that the main compound contributing to the antioxidant activity is a polar compound, and it is highly likely to be a low-molecular protein or a free amino acid. In conclusion, the honey bee drone pupa is excellent as a food resource and can be utilized as a new functional material for food and functional food.

Aerodynamic Analysis, Required Power and Weight Estimation of a Compound (Tilt rotor + Lift + Cruise) Type eVTOL for Urban Air Mobility using Reverse Engineering Techniques (역설계 기법을 사용한 도심항공 모빌리티용 복합형(틸트로터 + 양력 + 순항) eVTOL의 공력 해석, 요구 동력 및 중량 예측)

  • Kim, Dong-Hee;Lee, Joon-Hee;Hwang, Ho-Yon
    • Journal of Advanced Navigation Technology
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    • v.25 no.1
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    • pp.17-28
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    • 2021
  • Recently, eVTOL, the next-generation of eco-friendly transportation, has been in the spotlight due to global warming along with traffic jams in large cities of many countries. This study benchmark the external features of Hyundai Motors S-A1, a compound eVTOL combined fixed and tilt rotors among many types of eVTOLs, to create the basic configuration using reverse design techniques. Basic configurations were created using CATIA and aerodynamic analyses were performed using the aircraft design and aerodynamic analysis programs, OpenVSP, XFLR5, and the aircraft wetted area, drag, and lift were calculated after selecting the airfoil, incidence angle, and dihedral and anhedral angles through trade study. Also, required powers were estimated for completing the given mission profile and components weight and the total weight were predicted using the estimation formula and data survey.