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THE IMPACT OF systems ON NAVAL engineering

Naval Engineers Journal 1968年第3期80卷 387-392页

作者： ROOT, L. EUGENE Mr. Root registered professional engineer in California received his B.A. in Engineering and Mathematics in 1932 from the University of the Pacific. He also received a M.S. in both Mechanical and Aeronautical Engineering from the California Institute of Technology in 1933 and 1934 respectively. Mr. Root joined Douglas Aircraft Company in 1934 where he served in such positions as Assistant Chief Aerodynamics Section (1934-39) Chief Aerodynamics Section (1939-46) and from 1946-48 he was assigned to special engineering projects (Project Rand) where he pioneered parametric approach to aircraft design. He joined the Rand Corporation as Chief Aircraft Division in 1948. While on leave from Rand in 1951-52 he acted as Special Assistant to Deputy Chief of Staff/Development Headquarters USAF. He also aided substantially in establishing the Directorate of Development Planning in the Office of Deputy Chief of Staff/Development. In 1953 Mr. Root was offered the position of Director of Development Planning Department with Lockheed Aircraft Corporation where he established a centralized planning effort generally toward a corporate diversification plan and specifically toward the development of missile and space system programs. In 1965 he became Vice President of Lock-heed Aircraft Corporation and General Manager of the Missiles and Space Division. In 1957 Mr. Root was made Group Vice President Missiles and Electronics of Lockheed Missiles and Space Division Lockheed Electronics Company and Grand Central Rocket Company where he served in this capacity until 1961 when he became President of Lockheed Missiles and Space Company in which position he is currently serving. Mr. Root has been very active in the aeronautic field serving on many committees and acting as aircraft design consultant. He holds the patent for central surface shape for aerodynamic balancing and has published many papers within the field. He has also been listed in “Who's Who in America” “Who's Who in the West” “Who's Who in Space” “Men of Space”

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A COMPUTER-MODEL FOR sHIPBOARD ENERGY ANALYsIs

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NAVAL ENGINEERs JOURNAL 1984年第5期96卷 33-45页

作者： DETOLLA, JP FLEMING, JR Joseph DeTolla:is a ship systems engineer in the Ship Systems Engineering Division SEA 56D5 at the Naval Sea Systems Command. His career with the Navy started in 1965 at the Philadelphia Naval Shipyard Design Division. In 1971 he transferred to the Naval Ship Engineering Center. He has held positions as a fluid systems design engineer and auxiliary systems design integration engineer. Mr. DeTolla has worked extensively in the synthesis and analysis of total energy systems notably the design development of the FFG-7 class waste heat recovery system. He is NA VSEA's machinery group computer supported design project coordinator and is managing the development of a machinery systems data base load forecasting algorithms and design analysis computer programs. Mr. DeTolla has a bachelor of science degree in mechanical engineering from Drexel University and a master of engineering administration degree from George Washington University. He is a registered professional engineer in the District of Columbia and has written several technical papers on waste heat recovery and energy conservation. Jeffrey Fleming:is a senior project engineer in the Energy R&D Office at the David Taylor Naval Ship R&D Center. In his current position as group leader for the future fleet energy conservation portion of the Navy's energy R&D program he is responsible for the identification and development of advanced components and subsystems which will lead to reductions in the fossil fuel consumption of future ships. Over the past several years he has also directed the development and application of total energy computer analysis techniques for the assessment of conventional and advanced shipboard machinery concepts. Mr. Fleming is a 1971 graduate electrical engineer of Virginia Polytechnic Institute and received his MS in electrical engineering from Johns Hopkins University in 1975. Mr. Fleming has authored various technical publications and was the recipient of the Severn Technical Society's “Best Technical Paper of the Year” award in 1

In support of the Navy's efforts to improve the energy usage of future ships and thereby to reduce fleet operating costs, a large scale computer model has been developed by the David Taylor Naval ship Research and Development Center (DTNsRDC) to analyze the performance of shipboard energy systems for applications other than nuclear or oil-fired steam propulsion plants. This paper discusses the applications and utility of this computer program as a performance analysis tool for design of ship machinery systems. The program is a simulation model that performs a complete thermodynamic analysis of a user-specified energy system. It offers considerable flexibility in analyzing a variety of propulsion, electrical, and auxiliary plant configurations through a component building block structure. Component subroutines that model the performance of shipboard equipment such as engines, boilers, generators, and compressors are available from the program library. Component subroutines are selected and linked in the program to model the desired machinery plant functional configurations. The operation of the defined shipboard energy system may then be simulated over a user-specified scenario of temperature, time, and load profiles. The program output furnishes information on component operating characteristics and fuel demands, which allows evaluation of the total system performance.

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FUTURE PROPULsION MACHINERY TECHNOLOGY FOR GAs-TURBINE POWERED FRIGATEs, DEsTROYERs, AND CRUIsERs

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NAVAL ENGINEERs JOURNAL 1984年第2期96卷 34-46页

作者： BAsKERVILLE, JE QUANDT, ER DONOVAN, MR USN The Authors Commander James E. Baskerville USNis presently assigned to Naval Sea Systems Command (NA VSEA) as the Ship Design Manager for the DDG 51 the Navy's next generation surface combatant. A graduate of the U.S. Naval Academy Class of 1969 he is a qualified Surface Warfare Officer and designated Engineering Duty Officer (ED). He received his M.S. degree in Mechanical Engineering and his professional degree of Ocean Engineer from the Massachusetts Institute of Technology (MIT) and holds a patent right on an Electronic Control and Response System. His naval assignments include tours in USSRamsey (FFG-2) Aide and Flag Lieutenant to the Commander Naval Electronic Systems Command and Ship Superintendent Surface Type Desk Officer and Assistant Design Superintendent at NA VSHIPYD Pearl Harbor. He was awarded the Meritorious Service Medal for distinguished performance at Pearl Harbor Naval Shipyard. As an author he has contributed articles to the ASNEJournaland given presentations at local sections on ship design the use of innovative technology in ship repair and maintenance and the costs and risks associated with engineering progress. Commander Baskerville is a registered Professional Engineer in the State of Virginia an adjunct professor teaching marine engineering at Virginia Tech. and in addition to ASNE which he joined in 1975 is a member of SNAME Tau Beta Pi Sigma Xi ASME and the American Society of Heating Refrigeration and Air Conditioning Engineers (ASHRAE). Dr. Earl R. Quandt:received his degree of Chemical Engineer from the University of Cincinnati in 1956 and his Ph.D. degree in Chemical Engineering from the University of Pittsburgh in 1961. He worked in the naval reactors program at the Bettis Atomic Power Laboratory from 1956 to 1963. Since that time he has been with David Taylor Naval Ship Research and Development Center Annapolis Maryland where he is Head of the Power Systems Division. He contributed to this paper while on a one year assignment to the U.S. Naval Academy as V

A turning point occurred in naval engineering in 1972 when the U.s. N avy chose to use marine gas turbines for the propulsion of its new sPRUANCE and PERRY Class ships. This paper reviews the more than twenty years of experience with turbine technology and its design integration into combat ships needed to make that decision. It is concluded that the availability of a good second generation aircraft derivative engine with proven reliability and a strong commercial base, i.e., the LM-2500, was as important to the decision as was the predicted improved ship effectiveness and cost benefits. This paper discusses improvements that can be made to the twin engine, single gear, single propeller shaft system. Focusing only on this mechanical transmission concept, it addresses the impact of possible improvements to the engine, gear, and shafting. In particular, the paper discusses current LM-2500 related R&D efforts to: (a) obtain improved part-power fuel rates, (b) integrate with a reversing reduction gear, and (c) add on a waste heat recovery steam cycle. Looking ahead to the year 2000, this paper suggests that a successor to the ubiquitous LM-2500 will appear in the 15 MW power range to provide the next step in the evolution of the twin engine package. This new naval engine will most likely be based on an aircraft core that exists at present, such that it will have demonstrated its reliability and commercial potential through many hours of testing prior to its mid-1990 marine conversion. This new engine is expected to offer improved air flow, an excellent fuel rate (approaching a flat 0.30 LB/HP-HR), and effective maintenance monitoring, all at some expense in size, weight, and cost. The year 2000 engine will burn a liquid hydrocarbon fuel similar to JP-5 because of its aircraft origins. Combined with advances in gear and shafting technology, the full twin engine propulsion system of the year 2000 should be markedly lighter, smaller, and more efficient than today's units.

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THE FT9 MARINE GAs TURBINE ENGINE DEVELOPMENT program

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Naval Engineers Journal 1975年第6期87卷 79-96页

作者： FAIRBANKs, JOHN W. The author is a graduate of the Maine Maritime Academy Stanford University and the University of Santa Clara. His undergraduate degrees were in Marine and Mechanical Engineering and his Masters Degree Specialization was in Heat-Mass-Momentum Transfer within the Mechanical Engineering Department He has taught Gas Dynamics Thermodynamics and Direct Energy Conversion at Texas A&M and the University of Maryland and has sailed as a licensed Marine Engineer for two and a half years with the American Export Lines currently holding active First Assistant Steam Unlimited and Third Assistant Diesel Unlimited licenses. From 1954 to 1957 he was on active duty in the U.S. Navy serving in the USS Montrose (APA-212) as both Main Propulsion Assistant and Chief Engineer. While employed at Hiller Aircraft Company he was in the Advanced Research Group and worked on the Detached Coanda Effect for VTOL and ground effect machines as well as designing high-speed bearings and high-speed shaft test stands for the SC-142A an experimental tilt wing aircraft program. In 1963 he went to Philco-Ford to design a Brayton Cycle Power System for a solar probe spacecraft and also worked on the Thermal and Power System Design of the IDCSP (DOD's Communication Satellite). At NASA's Goddard Space Center for six years his responsibilities included design fabrication integration test launch and flight operation of solar arrays on two spacecraft and also as Power Systems Engineer for the Orbiting Astronomical Observatory the largest unmanned spacecraft flown. In 1971 he joined NAVSEC where he is currently the Program Engineer on the FT9 Gas Turbine Development Program and Coordinator of the Navy's Materials Programs for advanced gas turbines. Having organized the first two Navy Gas Turbine Materials Conferences he is presently organizing U.S. participation in a joint U.S. Navy Royal Navy Gas Turbine Materials Conference to be held in ‘the United Kingdom in September 1976. Mr. Fairbanks has authored or coauthored 21 technical papers and i

The current Navy philosophy for marine gas turbine engine development is to marinize an existing aircraft turbo jet engine. The FT9 Marine Gas Turbine Engine is a 33,000 horsepower version of the Pratt and Whitney JT9D engine, which powers the 747 aircraft. Marinization of the JT9D basically involves removal of the fan section, addition of a power turbine, structural modification to several components, and material changes to provide corrosion‐resistance in the marine environment. Characteristics and ratings of the individual engine components are discussed as well as the assembled engine. The FT9 design incorporates the modular replacement concept. Modular replacement permits replacement of short‐life components such as the hot‐section without removing the engine from its mounts. The FT9 specification requires development of a condition monitoring system as an integral part of the engine development. Thus, provisions for sensor installations are incorporated in the design. Accelerometers are installed on the internal engine bearing housings to provide improved vibration signals. These accelerometers are mounted on rods such that they are removable without engine disassembly. Extensive borescope provisions are included to provide capability to inspect all hot‐section components without disassembling the engine. The engine life‐limiting component is the hot‐section because of the susceptibility of the blade and vane materials to sulphidation/oxidation at the temperatures encountered with the advanced engines. sophisticated Made and vane cooling is used to allow high turbine inlet temperatures while keeping blade metal temperatures in a region where sulphidation/oxidation is only moderately active. Coatings are added to blades and vanes to extend engine life. Three FT9 engines will be delivered to the Navy. The target date for provisional service Approval of FT9 is mid‐1978. FT9 will provide the U.s. Navy with the most advanced marine gas turbine with the highest powe

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THE MAINTENANCE engineering ANALYsIs, A VITAL LINK BETWEEN THE DEsIGN ENGINEER AND FLEET sUPPORT

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Naval Engineers Journal 1974年第1期86卷 84-94页

作者： MARCUCILLI, T.J. HENDRICKsON, M.L. Mr. Theodore J. Marcucilli received his Bachelor's degree in Mechanical Engineering from New York University in 1954. He joined the then Bureau of Ships in the Internal Combustion Engines Branch later to be merged with the Gas Turbine Branch. He progressed through positions of increasing responsibility in the areas of RDT&E Acoustics Shock and Vibration and by June 1962 was in charge of the Machinery Division's efforts in support of Project SEAHAWK an advanced design ASW destroyer. In September 1963 he was designated as Project Manager for the Pressure Fired Boiler Program for seventeen DE's (1040 C1 DEG-1 C1 and AGDE-1). This assignment was the first known application of the Project Management concept in the Bureau of Ships. In June 1966 he was placed in charge of the Plans Policies and Procedures Branch in the Naval Ship Engineering Center and was responsible for the formulation and implementation of Acquisition Management policy and procedures. The following November he was appointed Branch Head for Propulsion Electrical and Auxiliaries Systems in the LHA Project (PMS 377) and has remained with the project from the pre-concept formulation phase through the current building period in the development and production phase. Mr. Marshall L. Hendrickson received his Bachelor's degree in Commerce from the University of Maryland and is presently enrolled in a Master's program in Government Procurement and Contract Administration at George Washington University. He has been involved in Navy Project Management Administration since January of 1963. Prior to that he had extensive Fleet experience as a Field Serivce Engineer for the Philco Corporation. Navy projects he has been associated with include the SPARROW and SIDE-WINDER Missiles the F-4 (Phantom) Series aircraft the Navy Maintenance and Material Management (3-M) System the LHA-1 Class Amphibious Assault Ship and the Ship and Air Systems Integration (SASI) Project. Presently he is the Division Director for Integrated Logistic Support on the SASI Pro

This paper discusses the Maintenance engineering Analyses (MEA) as performed in support of a major ship acquisition process. A major impetus is to demonstrate how the MEA can be utilized better to provide a direct data link between the design agent and the logistic support community to enhance Fleet operational effectiveness. A description of the overall MEA process is provided and several examples are used showing the type of design improvements realizable through an integration of the MEA process into the early stages of ship system design. © 1974 American society of Naval Engineers

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OPPORTUNITIEs FOR PACIFIC FLEET FF-1052 CLAss sHIPs TO sAVE ENERGY

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NAVAL ENGINEERs JOURNAL 1985年第4期97卷 315-321页

作者： PEHLIVAN, H KENYON, CW Hasan Pehlivan:received his BS in marine engineering from the Merchant Marine Academy (Turkey) in 1971 and his MS degree from Old Dominion University (Norfolk) in 1975. He was employed by D.B. Cargo Line (Turkey) as an engineering officer on ocean-going cargo vessels from 1971 to 1973. After receiving his masters degree in power engineering in 1975 he was employed by J.J. Henry Co. Inc. in Washington DC where he was involved in supporting the DTNSRDC Shipboard Energy Conservation Program which included the development of the steam system simulation (STMSYS) heat balance computer program for FF-1052/1078 class frigates. In addition he was cognizant engineer for various fluid systems designs for PCG and CSGN. In 1978 he joined M. Rosenblatt & Sons Inc. where he was cognizant engineer for various fluid systems designs for CVV DDG-51 and ARS-50. He was also leading engineer in support of DTNSRDC for the development of innovative machinery options for the baseline DD-963. In 1980 he joined NKF Engineering Inc. where he directs and performs DTNSRDC ship energy conservation analyses for frigates cruisers destroyers and aircraft carriers. He has been assisting the NAVSEA energy office in directing and performing Ship Energy Conservation Assist Team (SECAT) surveys aboard Navy ships since 1982. Mr. Pehlivan is currently manager of ship auxiliary systems in charge of the design and development of fluid systems pollution abatement distilling plants etc. He is a member of ASNE. Clarence W. Kenyon:graduated from the State University of New York Maritime College in 1960 and sailed on a third assistant engineer's license with Isbrandtsen Steamship Company before accepting an engineering position with the Long Beach Naval Shipyard in 1961 where he worked in the Steam Propulsion and Auxiliaries Section and the Mechanical and Hydraulic Section. He also taught a course in engineering fundamentals to engineering technicians in the evenings. In 1963 he accepted a position with the Space Division of North American Avia

The shipboard energy conservation assist team (sECAT) program was introduced to the Us Pacific surface Fleet (sURFPAC) in 1983 following one year testing in the Us Atlantic surface Fleet (sURFLANT). Experiences aboard sURFLANT ships had provided the basis for improvements which could also be applied to sURFPAC ships. Chief among these improvements were simple fuel measurement, fuel curve development methods, an energy survey checklist, and an equipment status board which identifies economic machinery alignments. The first sURFPAC ship to receive a sECAT visit was a FF-1052 class ship. Fuel consumption was significantly higher on this ship than the six FF-1052/1078 class sURFLANT ships previously visited. sECAT immediately looked for reasons for this increase in fuel consumption. Three significant changes received by this ship and not received by the six sURFLANT ships were identified. They were a new design economizer, Navjet vice Wallsend burners, and removal of overload control valves on the forced draft blowers. Another sURFPAC frigate with the same three changes was visited to validate the results obtained from the first ship. This paper discusses recent improvements to the sECAT program. It also examines the differences in fuel consumption observed between sURFLANT and sURFPAC FF-1052/1078 class ships. The economics of potential solutions to the higher fuel consumption problem aboard sURFPAC ships is analyzed with special emphasis on alternative burner designs and forced draft blower changes. Recommendations are made to reduce fuel consumption both by equipment changes and expanded energy initiatives.

关键词： NAVAL VEssELs

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The U.s. Navy Diving program

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Naval Engineers Journal 1974年第4期86卷 17-28页

作者： COLEMAN, JAMEs J. USN The author is a graduate of the U.S. Navy Academy Class of 1957. Prior to pursuing an advanced degree at Webb Institute of Naval Architecture he spent two years in destroyers and four years in submarines. Designated an Engineering Duty Officer (EDO) in 1966 he attended the Deep Sea Diving School and proceeded to Hunters Point Division of the San Francisco Naval Shipyard. Here he was responsible for the production efforts in the Deep Dive System MK 2 and the SEALAB III Program. While at Hunters Point he was also the 12th Naval District Salvage Officer and the Salvage Master during the raising of the nuclear submarine USS Guitarro which sank at Mare Island Naval Shipyard in May 1969. Following a tour on the Staff Commander Service Force U.S. Atlantic Fleet as the Fleet Salvage Officer he assumed command of the Experimental Diving Unit Washington D.C. in 1971 with additional duty at the Naval Ship Systems Command as the Supervisor of Diving. During this tour the Experimental Diving Unit conducted a world record 1600 foot wet hyperbaric dive. Relieved of this command on 1 October 1973 he presently remains as the Supervisor of Diving.

The office of the supervisor of Diving, Naval ship systems Command, is responsible for the development and testing of swimmer and diver equipment. The goal of the Navy Diving program is to enable the diver to work safely, efficiently, and in comfort at 1,000 feet today;1,500 feet in the near future;and 2,500 feet in the far term. This program is divided into three areas of concern: a) surface supported Diving;b) Integrated Diving system;and c) Man‐in‐the‐sea Deep Ocean. The paper focuses on the aforementioned areas by relating to existing equipments, their problems, and what programs are currently being proved to resolve these problems. © 1974 American society of Naval Engineers

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Developing a prototype concurrent design tool for composite topside structures

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NAVAL ENGINEERs JOURNAL 1997年第3期109卷 279-290页

作者： Dirlik, s Hambric, s Azarm, s Marquardt, M Hellman, A Bartlett, s Castelli, V Steve Dirlik:began his career at the Naval Surface Warfare Center Carderock Division in 1981 as an aerospace engineer co-op student. He completed his bachelor of science degree in aeropace and ocean engineering from Virginia Polytechnic Institute and State University in 1985 and his master of science degree in aerospace engineering from the University of Maryland in 1990. Mr. Dirlik recently completed a master of science program in applied physics at The Johns Hopins University and currently works in the Radar Cross Section and Target Physics Branch of the Signatures Directorate at the Naval Surface Warfare Center Corderoke Division. He has worked on Navy low observable programs since 1990. Stephen Hambric:is a research associate at the Applied Research Laboratory at The Pennsylvania State University. He received his B. S. and M.S. degree in mechanical engineering from Virginia Polytechnic Institute and State University and his D. Sc. in mechnical engineering from the George Washington University. He has worked on several computer aided multidiscikplinary design and optimization projects over the years including an automated propeller design system and a structural acoustic optimization capability. Dr. Shpour Azarm:is currently working as an associate professor with the Design and Manufacturing Group of the Department of Mechanical Engineering at the University of maryland at College Park. Dr Azarm's expertise is in the areas of optimization-based designed and concurrent design and optimization of multidisciplinary systems. He was a consultant at Black & Decker Corporation (summer 1996) and worked as a Navy senior summer faculty fellow (summer 1995) and a NASA summer faculty fellow (summer 1994). He was a visiting scientist at NASA Langley Research Center for Multidisciplinary Analysis and Applied Structural Optimzatiom at the University of Siegen in Germany (spring 1992) and the Design Institute of the Technical University of Denmark (summer 1990). Dr Azarm was an associate technical editor of the ASME Jour

A prototype concurrent engineering tool has been developed for the preliminary design of composite topside structures for modern navy warships. This tool, named GELs for the Concurrent engineering of Layered structures, provides designers with an immediate assessment of the impacts of their decisions on several disciplines which are important to the performance of a modern naval topside structure, including electromagnetic interference effects (EMI), radar cross section (RCs), structural integrity, cost, and weight. Preliminary analysis modules in each of these disciplines are integrated to operate from a common set of design variables and a common materials database. Performance in each discipline and an overall fitness function for the concept are then evaluated. A graphical user interface (GUI) is used to define requirements and to display the results from the technical analysis modules. Optimization techniques, including feasible sequential quadratic programming (FsQP) and exhaustive search are used to modify the design variables to satisfy all requirements simultaneously. The development of this tool, the technical modules, and their integration are discussed noting the decisions and compromises required to develop and integrate the modules into a prototype conceptual design tool.

关键词： Warships

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Comparative Heave Dynamics Of Two Unusual ship Configurations For Recovery Of submersibles

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Naval Engineers Journal 1971年第5期83卷 30-36页

作者： MOTHERWAY, D.L. HELLER, s.R. D. L. Motherway received his Bachelor of Science Degree in Mechanical Engineering from the University of Rhode Island in June 1961. He was subsequently employed at General Dynamics/Electric Boat Division Groton Connecticut where he held positions in their Planning Department as a planning engineer for FBM Submarine Construction and in the Mechanical Division as a design engineer. Motherway went to the Naval Ship Engineering Center Washington D. C. in March of 1966 with the Submarine Hydraulics Section of the Hull Design Branch where he participated in the design of submarine hydraulic systems. He later transferred to the Ocean Engineering Section of the Deck Systems Branch where he participated in design related to deep submergence vehicles and ocean salvage and retrieval systems. During this period at NavSEC he received his Master Science Degree in Mechanical Engineering from the Catholic University of America Washington D. C. From April 1970 to May 1971 he was with the Undersea Long-Range Missile System (ULMS) Submarine Design Development Office in the capacity of Assistant Subsystem Design Director. Currently he is the Senior Project Engineer for the ULMS program at the office of the Supervisor of Shipbuilding Conversion and Repair Groton Connecticut. He is a member of ASNE and ASE. S. R. Heller Jr. a retired Engineering Duty Officer of the United States Navy received his undergraduate education at the University of Michigan in Naval Architecture and Marine Engineering and in Mathematics. Following typical shipyard duty during World War II he received postgraduate instruction at the Massachusetts Institute of Technology leading to the degrees of Naval Engineer and Doctor of Science in Naval Architecture. Since then he has had design responsibilities in the Bureau of Ships had a maintenance assignment with the Fleet directed structural research at the David Taylor Model Basin engaged in submarine design and construction at Portsmouth Naval Shipyard and was the last Head of Hull Design in the

The comparative heaving characteristics of two unusual ship configurations, a spar‐type ship similar to FLIP and a catamaran which employs a submerged cradle suspended by sophisticated motion attenuation devices, for recovery of small submersibles are presented. The two ships are described and their heaving characteristics are determined analytically using classical vibration theory. © 1971 American society of Naval Engineers

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InCosmiCon: A New Italian-Peruvian project about sETI and Big History 70

InCosmiCon: A New Italian-Peruvian project about SETI and Bi...

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70th International Astronautical Congress, IAC 2019

作者： Musso, Paolo Antonietti, Nicolò Asla, Mariano Atachahua, Wilmer Azcona, Guisella Capatinta, María Ceroni, Mauro Crippa, Roberto Gómez, Ángel Jordan, Alejandra Lagos, David López, Didier Maccone, Claudio Montebugnoli, stelio Navarro, Janina Oliva, Jorge Pereyra, Carlota savio, Giuseppe Valdivia-silva, Julio Vargas, Teófilo Cervantes, Víctor Daniel Vera Viaña, Carlos Vinces, Patricia Vilcapuma Zapata, Remigio Zumaeta, Esaú Department of Human Sciences Innovation and Territory University of Insubria Via Sant'Abbondio 12 Como22100 Italy Department of Electronic Engineering Polytechnic of Torino Torino Italy Instituto de Filosofía Universidad Austral Calle Mariano Acosta Buenos Aires1611 Argentina Facultad de Ciencias de la Educación y Humanidades Universidad Católica Sedes Sapientiae Av. Gonzales Prada s.n. Urb. Villa Los Ángeles Los Olivos Peru Departamento de Humanidades Universidad Tecnológica del Perú Av. Arequipa 265 Lima Peru Facultad de Letras y Ciencias Humanas Universidad Nacional Mayor de San Marcos Calle German Amézaga 375 Lima Peru Department of Sciences of the Nervous System and Behavior University of Pavia Italy Scientific Board of the Museum "Volandia" Somma Lombardo Italy Departamento de Filosofía y Teología Universidad Femenina del Sagrado Corazón Av. Los Frutales La Molina Lima15023 Peru Departamento de Arquitectura UPC Prolongación Primavera 2390 Santiago de Surco Lima15023 Peru Facultad de Educación Básica Bilingüe Intercultural Universidad Católica Sedes Sapientiae Filial de Nopoki Carretera Atalaya-Aerija km 15 Atalaya Ucayali Peru IAA SETI Committee Via Martorelli 43 Torino10155 Italy INAF Senior Engineer and SETI Advisor Viale del Parco Mellini Roma Italy Departamento de Filosofía Facultad de Teología Pontificia y Civil de Lima Calle Carlos Bondy 700 Pueblo Libre Lima15086 Peru Program "Ecovida y Universo" of the "Asociación Qespichyq" Av. Jorge Basadre 607 oficina 422 Lima San Isidro15073 Peru CEO of H4 Research Via Ostiense 177/C Roma00154 Italy Facultad de Bioingeniería UTEC Jr. Silva 165 Barranco Lima15063 Peru Facultad de Ciencias Físicas Grupo de Astronomía SPACE-FCF-UNMSM Universidad Nacional Mayor de San Marcos Calle German Amézaga 375 Lima Peru

InCosmiCon (Intelligence in the Cosmic Context) is a project about sETI and Big History which arises on one side from the experience of the Italian sETI program, and on the other side from the project La vida en el universo: su origen, su naturaleza, su sentido (Life in the universe: its origin, its nature, its meaning), which has been developed in Peru as one of the six Oxford Templeton Visiting Fellowships to Latin America offered by the Ian Ramsey Centre for science and Religion at the Oxford University and the John Templeton Foundation in 2017. From that project, originally proposed by two Universities of Lima, the UCss (Universidad Católica sedes sapientiae) and the UNIFÉ (Universidad Femenina del sagrado Corazón), many new relationships and projects have arisen, so that finally we had the idea of creating a stable international interdisciplinary research group, based at the University of Insubria (Italy) and open to scholars from any countries all over the world, but, first of all, from Italy and Peru. The name InCosmiCon means that we want to investigate, through both theoretical reflections and field researches, the topic of intelligent life in the universe, first of all from the point of view of classic sETI, but also into the more general framework of the so-called Big History, as strongly suggested by the present Chairman of the IAA sETI Committee, Dr. Claudio Maccone. A special role will be played, as already in the project La vida en el universo, by the UCss Amazonian seat of Atalaya (called UCss Nopoki), one of the very few cases in the world (maybe the unique fully successful) of a positive interaction between cultures with a very different technological level, as on one side our Western civilizations and on the other side the 14 native Amazonian peoples having their sons studying in Nopoki, which could be also a model for a positive interaction with a hypothetical extraterrestrial civilization. In the present paper some of the founders of the InCosmi

关键词： Cosmology

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