• 제목/요약/키워드: Aircraft Carrier

검색결과 93건 처리시간 0.029초

항모쏘티생성시스템(CVSGS) 경계분석에 관한 연구 (The Study of Aircraft Carrier Sortie Generation System(CVSGS) Boundary Analysis)

  • 이승도;박범
    • 시스템엔지니어링학술지
    • /
    • 제11권1호
    • /
    • pp.73-79
    • /
    • 2015
  • This paper describes boundary analysis for modeling Aircraft Carrier Sortie Generation System(CVSGS). An aircraft carrier, as a super system, is a warship going into battle by operating a number of aircraft on deck and it should be lay down a definition about aviation operations interacting between aircraft carrier and carrier air wing in small deck area. For this reason this paper models common aviation support system for generating sortie basic unit of carrier aviation operations unlike to general warship and defines boundaries between this system and aircraft carrier and carrier air wing. This paper analysis activities of aircraft carrier and embarked carrier air wing in carrier aviation operations, and analysis and defines boundaries Aircraft Carrier Sortie Generation System(CVSGS) to perform core functions in interacting between aircraft carrier and embarked carrier air wing.

국가 역량을 고려한 효율성 기반 한국형 항공모함 규모 최적화 연구 (A Study on the Scale Optimization of the Korean-type Aircraft Carrier based on Efficiency Considering National Competency)

  • 정병기;김기태;박성제
    • 산업경영시스템학회지
    • /
    • 제45권3호
    • /
    • pp.49-56
    • /
    • 2022
  • ROK Navy intends to secure the Korean-type aircraft carrier in order to effectively prepare for various future security threats. In general, the Korean national competency is considered to be at the level of having an aircraft carrier, but it is unclear what scale aircraft carrier would be appropriate. In this study, the efficiency was evaluated through the relative comparison between national competency(national power, economic power) and the scale of aircraft carriers, and the optimal scale of the Korean-type aircraft carrier that could be acquired was presented. A DEA(Data Envelopment Analysis) model was applied to aircraft carriers(19 aircraft carriers in 11 countries) currently in operation and scheduled to be possessed in the world. As input variables, CINC(Composite Index of National Capability) and GDP(Gross Domestic Product), which are the most widely used as indicators of national and economic power, and as output variables, the full-load displacement, length, and width of aircraft carriers were selected. ARIMA(short-term within 5 years) and simple regression(long-term over 5 years) were used to estimate the future national competency of each country at the time of aircraft carriers acquisition. The relative efficiency score of the Korean-type aircraft carrier currently being evaluated is 1.062, and it was evaluated as small-scale aircraft carrier compared to the national competency. Based on Korean national competency, the optimal scale of the Korean-type aircraft carrier calculated by aggregating benchmark groups, is 58,308.1 tons of full-load displacement, 279.4m in length, and 68.3m in width.

DoDAF를 이용한 항모 항공지원시스템 아키텍처 개발 (The Development of Carrier Aviation Support System Architecture using DoDAF)

  • 이승도;박범
    • 시스템엔지니어링학술지
    • /
    • 제11권1호
    • /
    • pp.33-39
    • /
    • 2015
  • This paper describes a development of aircraft carrier aviation support system architecture using DoDAF. The aircraft carrier, a warship performing a role of mobile sea air base in offensive and defense mission, is super system that is comprised of carrier itself and carrier-based airwing. Performing critical role in step with aviation operations in carrier-airwing interactions, the aviation support system of aircraft carrier is also system of systems. It requires a complex and integrated approach based on systems engineering in establishing concept of this complex systems. In this view, this study establishes an operational scenario and derives operational requirements by identifying aviation operations environment on deck of aircraft carrier. The study presents the operational architecture of the carrier aviation support system by using DoDAF and CASE tool CORE.

한국형 경항공모함 항공관제체계에 대한 연구 (A Study on the air traffic control system of Korea Light Aircraft Carrier)

  • 최연철;정용태;조영진
    • 한국항행학회논문지
    • /
    • 제26권5호
    • /
    • pp.272-280
    • /
    • 2022
  • 항공모함은 해상에서 항공기지 역할을 하는 전투함으로 항공기를 운용하는 군용함정으로 탑재된 항공기를 통하여 전투를 수행한다. 해군은 2033년경 수직이착륙 전투기와 헬기를 탑재할 수 있는 4만 톤급의 경항공모함 운용계획을 제시하였는데 본 연구는 이러한점에 착안하여 해외사례를 기초로 우리나라에서 경항공모함을 운영에서 요구되는 항공지원시스템 가운데 항공관제장비의 운영에 대해 고찰하였다. 필수장비로 공역 관제를 위한 PriFly, TWR의 ILARTS, ILM와 접근관제를 위한 ASR, PAR, LAAS 또는 RNAV, PALS(JPALS) 이 필요하며, 항행안전시설을 위한 URN-25 TACAN, ICLS(El/Az), ACLS OLS, MOVLAS, IFLOLS 등과 함께 통신네트워크를 위한 LINK-16 및 CEC, SATCOM이 요구되며, 적아 식별장비의 구축이 요구된다. 본 연구는 2부로 구성되며 2부에서는 구체적인 항공모함에서의 관제 방법을 기술할 것이다.

미(美) 해군의 해양전략 발전과 우리의 과제 - 항모운용을 중심으로 - (The Development of US Navy's Maritime Strategy and the ROK's Tasks with a Focus on the Roles of Aircraft Carrier)

  • 권영일
    • Strategy21
    • /
    • 통권41호
    • /
    • pp.30-51
    • /
    • 2017
  • Neighboring powers in the Korean Peninsula have started to develop and operate aircraft carriers or equivalent forces to cope with rising North Korean nuclear and missile threats and also to show its national might. For example, the United States has added a aircraft carrier from the 3rd fleet to western pacific theater of operation, while Peoples Republic of China is undergoing operational test of Liaoning as well as preparing for christening of its 2nd aircraft carrier. Japan is flexing its muscle as well by deploying Izumo capable of operating F-35B to Southeast Asia to participate in multilateral exercises starting this year. It is a high time to know more about aircraft carriers or similar types in terms of maritime strategy and history. The U.S. has had by far the vast amount of experiences in utilizing aircraft carrier that it would be beneficial for us to examine U.S. perspectives and its application in the Korean Peninsula. It will provide us with insights to understand and predict what it would be like in times of crisis in the Korean Peninsula in the perspective of aircraft carrier's involvement. This paper intends to show some aspects of future conflicts in the Korean Peninsula and how the ROK Navy can best be ready for such situation. For research purpose, U.S. maritime strategy has been developed in stages ; establishment phase, WWI phase, WWII phase, Cold war phase, post Cold war phase. Each phase includes such factors as threats, strategic concept, applications, and ways to improve maritime strategy. Finally, the role of aircraft carrier based on past history as well as future conflict shines the importance to have power projection capabilities for the ROK Navy. The intrinsic nature of the navy in the world is to project power ashore just as history proved it.

A simulative method for evaluating the resistance of the flight deck's operational capability to the attack of anti-ship weapons

  • Yang, Fangqing;Wang, Chao;Liao, Quanmi;Huang, Sheng
    • International Journal of Naval Architecture and Ocean Engineering
    • /
    • 제8권6호
    • /
    • pp.563-576
    • /
    • 2016
  • The flight deck of an aircraft carrier is relatively vulnerable compared to its hull, as the damage of some subsystems on the flight deck may cause the carrier losing its operational capability. Therefore, this work aims to represent a simulative method for evaluating the resistance of the flight deck's operational capability in the condition that the aircraft carrier is together with its strike group and the enemy uses the anti-ship missiles with the cluster warheads to attack. In the simulations, the susceptibility of the carrier and the vulnerability of the aircraft guarantee resources are gained. Then, with the help of the closed queuing network, the residual sortie generation rate can be solved, which reflects the flight deck's residual operational capability. The results have proven that the flight deck is of strong resistance to these attacks while it is very sensitive to the loss of some key aircraft guarantee resources.

A New Overlap Current Restraining Method for Current-source Rectifier

  • Qin, Haihong;Liu, Qing;Zhang, Ying;Zhang, Xin;Wang, Dan
    • Journal of Power Electronics
    • /
    • 제18권2호
    • /
    • pp.615-626
    • /
    • 2018
  • To ensure a DC current path and avoid large voltage overshoot of the DC-link inductor, alternating PWM pulses in the current-source rectifier should be supplemented by overlap time, which generates an overlap current and causes input current distortion. In this study, the influence of overlap time is illustrated by comparing the AC-side current before and after overlap time is added. The overlap current distribution caused by overlap time is discussed under different modulation carriers, including triangle carrier, positive-going carrier, and negative-going carrier. The quantitative relationship between the extra harmonics of the AC-side current and overlap time is based on the Fourier analysis. Based on the commutation analysis, a new carrier modulation scheme that can restrain overlap current is proposed. A 3 kW prototype is established to verify the effectiveness of the influence of overlap time and the proposed restraining modulation scheme.

동역학 시뮬레이션을 이용한 함재기 견인차량의 주행특성 분석 기법에 관한 연구 (A Study on Analytical Method of Driving Characteristics of Carrier Aircraft Towing Vehicles Using Dynamic Simulation)

  • 오재원;홍사영;홍섭
    • 대한조선학회논문집
    • /
    • 제60권4호
    • /
    • pp.288-295
    • /
    • 2023
  • This paper deals with the dynamic simulation method for analysis of driving characteristics of aircraft and towing vehicles (TUG) on carrier vessel in wave motions. For prompt deployment in a short period of time, optimization of the movement of carrier aircraft becomes a major issue. In this regards, strategy studies using real-time simulation technology and optimal decision-making technologies are being conducted. In the present work, the dynamic characteristics of carrier aircraft and TUG connected by towbar or towbarless mechanism were investigated by means of multi-body dynamics model. Meanwhile, for real-time simulation, Dugoff's model of tire loads calculation was adopted. Through comparative analysis it was confirmed that the similarity of results between the multi-body contact model and the tire load calculation model can be achieved by coefficients tuning.

경항공모함 이·착함 성능평가 및 안전임무 수행범주 일관 해석 연구 (A Study on Short-Take-Off and Vertical Landing (STOVL) Performance Evaluation of a Light Aircraft Carrier and a Consistent Analysis of Safe Operating Envelope (SOE))

  • 홍사영;박동민;정재환;서민국;조석규
    • 대한조선학회논문집
    • /
    • 제61권2호
    • /
    • pp.125-134
    • /
    • 2024
  • The Safe Operating Envelope (SOE) combined with Short-Take-Off and Vertical Landing (STOVL) performance is an essential consideration of a light aircraft carrier for design of hull shape with excellent seakeeping performance in terms of naval air operations as well as traditional naval ship missions such as Transit and Patrol (TAP), and Replenishment at Sea (RAS) and so on. A variety of procedures are systematically combined to determine SOE considering rather complicated missions associated with operation of aircraft onboard. The evaluation of take-off and landing safety missions onboard should consider wind effect on deck and severer seakeeping indices and standards compared with conventional naval ships. In order to support take-off and landing missions, various support activities of the crews are required. So, additional evaluation is needed for indicators such as MSI(Motion sickness Index) and MII(Motion Induced Interruptions), which are quantitative indicators of work ability that appear as a result of motion response. In this study, a standard procedure is developed including the seaworthiness performance indicators, standards, and evaluation procedures that should be considered during design of STOVL aircraft carrier. Analysis results are discussed in terns of air-wake on deck as well as seakeeping indices associated with design parameter changes in view of conceptual design of a light aircraft carrier.

Analysis of the Flow Field of Carrier-Based Aircraft Exhaust Jets Impact on the Flight Deck

  • Yue, Kuizhi;Sun, Yicheng;Liu, Hu;Guo, Weigang
    • International Journal of Aeronautical and Space Sciences
    • /
    • 제16권1호
    • /
    • pp.1-7
    • /
    • 2015
  • In order to provide some references for suitability of carrier-based aircrafts, this paper studies the flow field of exhaust jets and its impact on the flight deck. The geometrical models of aircraft carrier and carrier-based aircrafts are firstly built, on which unstructured tetrahedral meshes are generated for numerical analysis. Then, this paper simulates the flow field of exhaust jets to evaluate its impact on the Jet Blast Deflector (JBD) and the flight deck, when four carrier-based aircrafts are ready to start off in the bow. The standard k-${\varepsilon}$ equations, three-dimension N-S equations and the Computational Fluid Dynamics (CFD) theory are used in the analysis process. To solve the equations, the thermal coupling of the wind and the jet flow are also considered. The velocity and temperature distributions are provided with the simulation of the CFD software, FLUENT. The results indicate that: (1) this analytical method can be used to simulate aerodynamic problems with complex geometrical models, and the results are of high reliability; (2) the safety working area, the installation scheme of the JBD and the arrangement of the take-off position can be optimized through analysis.