LHD 8: a Step Toward the All Electric Warship
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Orientation Sheet for Horizon Updated: 2017-Apr-21
Orientation Sheet for Horizon Updated: 2017-Apr-21 General • All voyages should be documented in the ship’s log book. Report any damage or deficiencies to [email protected] and to boat manager [email protected] / 410-203-2673 Specifications Registration #: MD 5596 AC Hull#: XLY 595267 Make: Islander 36 Year: 1977 Engine: Perkins 4.108; 4-cyl Diesel 48-HP Displacement: 13,450 lbs Draft: 5’ 02” Mast Height Fuel Capacity: 30 gal. Holding tank: 18 gal. (from waterline): 52’ 06” Water Capacity: 54 gal. 2 tanks, below Salon Settees LOA: 36’ 08" Batteries: House battery 1 and 2 (Starboard lazaret) LWL: 28’ 25” Starting Battery (under companionway steps) Beam: 11’ 17” Sails: Main, Genoa on furler, staysail with boom Safety Equipment First Aid Kit: Drawer port side Rescue Sling: Stern Rail PFDs: V-berth Fire Extinguishers: (2) – Starboard side cabin, Port quater berth Day/Night Flares: Aerial & Hand-held – Drawer port side above seats in salon Sounds (Horn, Bell & Whistle): Drawer port side above seats in salon Auto-Switched Bilge Pump: Wired directly to House Battery (must be switched to Auto when leaving boat). The switch is located on the starboard side inside the cabin above the galley sink Old Bilge Pump: Wired to Electric Panel on the engine compartment wall (manual mode only). Do not use this pump unless the other one is not working. Manual Bilge Pump: Cockpit Port side (handle located in drawer port side above seats) Anchors: Danforth (35 lbs) bow; Rode: 15’ of chain & 150’ of line (marked every 30’) Thru-hulls/Sea-cocks: Engine -
Forces on Large Steam Turbine Blades RWE Npower Mechanical and Electrical Engineering Power Industry
Forces on Large Steam Turbine Blades RWE npower Mechanical and Electrical Engineering Power Industry INTRODUCTION RWE npower is a leading integrated UK energy company and is part of the RWE Group, one of Europe's leading utilities. We own and operate a diverse portfolio of power plant, including gas- fired combined cycle gas turbine, oil, and coal fired power stations, along with Combined Heat and Power plants on industrial site that supply both electrical power and heat. RWE npower also has a strong in-house operations and engineering capability that supports our existing assets and develops new power plant. Our retail business, npower, is one of the UK's largest suppliers of electricity and gas. In the UK RWE is also at the forefront of producing energy through renewable resources. npower renewables leads the UK wind power market and is a leader in hydroelectric generation. It developed the UK's first major off- shore wind farm, North Hoyle, off the North Wales Figure 1: Detailed view of turbine blades coast, which began operation in 2003. With blades (see Figure 1) rotating at such Through the RWE Power International brand, speeds, it is important that the fleet of steam RWE npower sells specialist services that cover turbines is managed to ensure safety and every aspect of owning and operating a power continued operation. If a blade were to fail in- plant, from construction, commissioning, service, this could result in safety risks and can operations and maintenance to eventual cost £millions to repair and, whilst the machine is decommissioning. not generating electricity, it can cost £hundreds of SCENARIO thousands per day in lost revenue. -
Use of Cogeneration in Large Industrial Projects
COGENERATION USE OF COGENERATION IN LARGE INDUSTRIAL PROJECTS (RECENT ADVANCES IN COGENERATION?) PRESENTER: JIM LONEY, PE [email protected] 281-295-7606 COGENERATION • WHAT IS COGENERATION? • Simultaneous generation of electricity and useful thermal energy (steam in most cases) • WHY COGENERATION? • Cogeneration is more efficient • Rankine Cycle – about 40% efficiency • Combined Cycle – about 60% efficiency • Cogeneration – about 87% efficiency • Why doesn’t everyone use only cogeneration? COGENERATION By Heinrich-Böll-Stiftung - https://www.flickr.com/photos/boellstiftung/38359636032, CC BY-SA 2.0, https://commons.wikimedia.org/w/index.php?curid=79343425 COGENERATION GENERATION SYSTEM LOSSES • Rankine Cycle – about 40% efficiency • Steam turbine cycle using fossil fuel • Most of the heat loss is from the STG exhaust • Some heat losses via boiler flue gas • Simple Cycle Gas Turbine– about 40% efficiency • The heat loss is from the gas turbine exhaust • Combined Cycle – about 60% efficiency • Recover the heat from the gas turbine exhaust and run a Rankine cycle • Cogeneration – about 87% efficiency COGENERATION • What is the problem with cogeneration? • Reality Strikes • In order to get to 87% efficiency, the heating load has to closely match the thermal energy left over from the generation of electricity. • Utility electricity demand typically follows a nocturnal/diurnal sine pattern • Steam heating loads follow a summer/winter cycle • With industrial users, electrical and heating loads are typically more stable COGENERATION • What factors determine if cogeneration makes sense? • ECONOMICS! • Not just the economics of the cogeneration unit, but the impact on the entire facility. • Fuel cost • Electricity cost, including stand-by charges • Operational flexibility including turndown ability • Reliability impacts • Possibly the largest influence • If the cogeneration unit has an outage then this may (will?) bring the entire facility down. -
Gannet Electronics
Gannet Electronics A Summary of the Electronic Equipment Fitted to early Model R.A.N Gannet A.S.1 Aircraft Prepared by David Mowat Ex-L.R.E.M.(A) 21st. August 2003 Page 1 Page 2 GANNET ELECTRONIC EQUIPMENT Introduction The ‘Heart’ of the Gannet as a Weapons System was its Electronic Equipment. It contained a comprehensive range of electronic equipment to enable it to perform the various roles for which it was designed. Its Primary Role was to detect, locate, and destroy enemy submarines. For this Role, the Aircraft was fitted with a Search Radar and Sonobuoy Systems. Other electronic systems were also installed for Communications, both internal and external, and Navigation. The various equipments were allocated an ‘Aircraft Radio Installation’ (ARI) number, which specified the actual equipment used in each installation. These may vary between aircraft depending on the role that the particular aircraft was to perform. A cross- reference List of ARI’s is shown at Appendix ‘A’. The various equipments can be grouped into four major categories as follows: a.! Communications b.! Navigation c.! Warfare Systems d.! Stores Communications Equipment The Communications Equipment was used to enable the crew to talk to each other (internal communications) and other aircraft, ships or bases (external communications). They are as follows: a.! Audio Amplifier Type A1961 The Type A1921 was used to amplify the Microphone outputs from the three crew members and feed it back into the earphones. It was located on the port side of the rear cockpit at about seat height just forward of the Radio Operator. -
19750827-0 DC-3 5Y-AAF.Pdf
1 CAV/ACC/24/75 ACCIDENT IUVESTIGATION BRANCH CIVIL AIRCRAFT ACCIDEiiT Report on the Accident to Douglas DC-3 Aircraft Registration number 5Y-AAF which occurred on the 27th August,1975 At 0922 hours, at Mtwara Airport, Tanzania. E A S T A F R I CAN C 0 M M U NIT Y AOCIDEwr REPORT AOCIDE:~T INVESTIGATIOn BRAl'WH 'CIVIL ACCIDENT REPORT CAV/ACC/24/75 AIRCRAFT TYPE 8; HEGISTRATION: Douglas DC-::- 5Y-l~ ENGINE: Pratt & \filii tney R1830-90D REGISTERED OWlIJ]~R & OPERATOR: East African Airways Corporation, P.O. Box 19002, NAIROBI, Kenya. CREVf: CAPTAIN Gabriel Sebastian Turuka ) ) Uninjured FIJ:1ST OFFICER Steven Robert Wegoye ) PASSENGER: Sixteen - Uninjured. PLACE OF ACCIDEHT: ~,1twara Airport, Tanzania. DATE AND T1MB: 27th August, 1975, 0922 hours. ALL rrU'lES IN THIS REPORT ARE G.1VI. T. SUMMARY The aircraft was operating East African Airways Service flight number EC037 from Dar es Salaam to Nachingmea with an unscheduled refuelling stop at I1twara with 3 crew and 16 passengers on board. The flight from Dar es Salaam was uneventful and an approach and landing was made onto runway 19. After touch down the aircraft swung to the left and then to the right, after which it left the runway where both main landing gear assys collapsed causing substantial daLage to the centre section and nacelle structure. The report concludes that the most probable cause of the accident was the failure of the pilot to initiate corrective action to prevent the aircraft from turning off the runway. 1.1 HISTORY OF THE FLIGHT: The aircraft departed Dar es Salaam with three crew and 16 passengers. -
Y ...Signature Redacted
Modeling Brake Specific Fuel Consumption to Support Exploration of Doubly Fed Electric Machines in Naval Engineering Applications by Michael R. Rowles, Jr. B.E., Electrical Engineering, Naval Architecture, State University of New York, Maritime College, 2006 Submitted to the Department of Mechanical Engineering in Partial Fulfillment of the Requirements for the Degrees of Naval Engineer and Master of Science in Naval Architecture and Marine Engineering at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY June 2016. 2016 Michael R. Rowles, Jr. All rights reserved. The author hereby grants to MIT permission to reproduce and to distribute publicly paper and electronic copies of this thesis document in whole or in part in any medium now known or hereafter c: A uth or ........................................... Signature redacted Department of Mechanical Engineering A may 22,k 2016 C ertified by ............................ Signature redacted .... Weston L. Gray, CDR, USN Associate Professor of the Practice, Naval Construction and Engineering redacted ..Thesis Reader Certified by .......... Signature Ll James L. Kirtley Professor of Electrical Engineering redacted Isis Supervisor Accepted by ............ SSignatu gnatu re ...................... Rohan Abeyaratne MASSACHUSETTS INSTITUTE Chairman, Committee on Graduate Students OF TECHNOLOGY Quentin Berg Professor of Mechanics Department of Mechanical Engineering JUN 02 2016 LIBRARIES ARCHIVES Modeling Brake Specific Fuel Consumption to Support Exploration of Doubly Fed Electric Machines in Naval Engineering Applications by Michael R. Rowles, Jr. Submitted to the Department of Mechanical Engineering on May 12, 2016 in Partial Fulfillment of the Requirements for Degrees of Naval Engineer and Master of Science in Mechanical Engineering Abstract The dynamic operational nature of naval power and propulsion requires Ship Design and Program Managers to design and select prime movers using a much more complex speed profile rather than typical of commercial vessels. -
Drivetrain 17 36 30 30 31 32 32 33 35 37 38 39 39 40 40 41 41 41 41 41 40 36-40
B Drivetrain ............................... 18 to 41 Drivetrain Struts Main .............................................................................18-19 Self-aligning gland type (with space) ................................. 30 Intermediate ...................................................................... 18 Heavy duty ..................................................................... 30 Sailboat ............................................................................. 19 Studs .................................................................................. 31 Port and starboard ............................................................ 20 Tournament (with space) ................................................ 32 Vee .................................................................................... 21 Self-aligning gland type (without space) ............................ 32 Universal ........................................................................... 21 Spud type Adjustable ....................................................................22-23 Tournament water cooled ............................................... 33 Cut off type ..................................................................... 22 Right hand thread ........................................................... 35 Swivel type ..................................................................... 23 Shaft logs..........................................................................36-40 Strut bolts ............................................................................. -
Bureau of Air Safety Investigation Report Basi
BUREAU OF AIR SAFETY INVESTIGATION REPORT BASI Report B/916/1017 Bell 214ST Helicopter VH-HOQ Timor Sea Latitude 12° 30' south Longitude 124° 25' east 22 November 1991 Bureau of Air Safety Investigation /i.:V Transport and Healonaf Development Department of Transport and Communications Bureau of Air Safety Investigation ACCIDENT INVESTIGATION REPORT B/916/1017 Bell 214ST Helicopter VH-HOQ Timor Sea Latitude 12° 30' south Longitude 124° 25' east 22 November 1991 Released by the Director of the Bureau of Air Safety Investigation under the provisions of Air Navigation Regulation 283 Bureau of Air Safety Investigation When the Bureau makes recommendations as a result of its investigations or research, safety, (in accordance with our charter), is our primary consideration. However, the Bureau fully recognises that the implementation of recommendations arising from its investigations will in some cases incur a cost to the industry. Consequently, the Bureau always attempts to ensure that common sense applies whenever recommendations are formulated. BASI does not have the resources to carry out a full cost- benefit analysis of every recommendation. The cost of any recommendation must always be balanced against its benefits to safety, and aviation safety involves the whole community. Such analysis is a matter for the CAA and the industry. ISBN 0642 193959 June 1993 This report was produced by the Bureau of Air Safety Investigation (BASI), PO Box 967, Civic Square ACT 2608. The Director of the Bureau authorised the investigation and the publication of this report pursuant to his delegated powers conferred by Air Navigation Regulations 278 and 283 respectively. -
Comparison of ORC Turbine and Stirling Engine to Produce Electricity from Gasified Poultry Waste
Sustainability 2014, 6, 5714-5729; doi:10.3390/su6095714 OPEN ACCESS sustainability ISSN 2071-1050 www.mdpi.com/journal/sustainability Article Comparison of ORC Turbine and Stirling Engine to Produce Electricity from Gasified Poultry Waste Franco Cotana 1,†, Antonio Messineo 2,†, Alessandro Petrozzi 1,†,*, Valentina Coccia 1, Gianluca Cavalaglio 1 and Andrea Aquino 1 1 CRB, Centro di Ricerca sulle Biomasse, Via Duranti sn, 06125 Perugia, Italy; E-Mails: [email protected] (F.C.); [email protected] (V.C.); [email protected] (G.C.); [email protected] (A.A.) 2 Università degli Studi di Enna “Kore” Cittadella Universitaria, 94100 Enna, Italy; E-Mail: [email protected] † These authors contributed equally to this work. * Author to whom correspondence should be addressed; E-Mail: [email protected]; Tel.: +39-075-585-3806; Fax: +39-075-515-3321. Received: 25 June 2014; in revised form: 5 August 2014 / Accepted: 12 August 2014 / Published: 28 August 2014 Abstract: The Biomass Research Centre, section of CIRIAF, has recently developed a biomass boiler (300 kW thermal powered), fed by the poultry manure collected in a nearby livestock. All the thermal requirements of the livestock will be covered by the heat produced by gas combustion in the gasifier boiler. Within the activities carried out by the research project ENERPOLL (Energy Valorization of Poultry Manure in a Thermal Power Plant), funded by the Italian Ministry of Agriculture and Forestry, this paper aims at studying an upgrade version of the existing thermal plant, investigating and analyzing the possible applications for electricity production recovering the exceeding thermal energy. A comparison of Organic Rankine Cycle turbines and Stirling engines, to produce electricity from gasified poultry waste, is proposed, evaluating technical and economic parameters, considering actual incentives on renewable produced electricity. -
WO 2015/012935 A2 29 January 2015 (29.01.2015) P O P C T
(12) INTERNATIONAL APPLICATION PUBLISHED UNDER THE PATENT COOPERATION TREATY (PCT) (19) World Intellectual Property Organization International Bureau (10) International Publication Number (43) International Publication Date WO 2015/012935 A2 29 January 2015 (29.01.2015) P O P C T (51) International Patent Classification: Bart Dean [US/US]; 2691 Daunet Ave., Simi Valley, Cali B64C 27/26 (2006.01) B64C 27/54 (2006.01) fornia 93065 (US). PARKS, William Martin [US/US]; B64C 5/02 (2006.01) B64C 39/02 (2006.01) 2805 North Woodrow Ave., Simi Valley, California 93065 B64C 9/00 (2006.01) G05D 1/08 (2006.01) (US). GANZER, David Wayne [US/US]; 4607 Kleberg B64C 25/00 (2006.01) B64C 29/00 (2006.01) St., Simi Valley, California 93063 (US). FISHER, Chris¬ topher Eugene [US/US]; 4 1 Los Vientos Dr., Thousand (21) International Application Number: Oaks, California 91320 (US). MUKHERJEE, Jason Sid- PCT/US20 14/036863 harthadev [US/US]; 605 Muirfield Ave., Simi Valley, (22) International Filing Date: California 93065 (US). KING, Joseph Frederick 5 May 2014 (05.05.2014) [US/US]; 10540 Gaviota Ave., Granada Hills, California 91344 (US). (25) Filing Language: English (74) Agent: DAWSON, James K.; 1445 E. Los Angeles Ave., English (26) Publication Language: Suite 108, Simi Valley, California 93065-2827 (US). (30) Priority Data: (81) Designated States (unless otherwise indicated, for every 3 May 2013 (03.05.2013) 61/819,487 US kind of national protection available): AE, AG, AL, AM, (71) Applicant: AEROVIRONMENT, INC. [US/US]; 181 W . AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, Huntington Drive, Suite 202, Monrovia, California 91016 BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DK, DM, (US). -
Steam Turbine Corrosion and Deposits Problems and Solutions
STEAM TURBINE CORROSION AND DEPOSITS PROBLEMS AND SOLUTIONS by Otakar Jonas Consultant and Lee Machemer Senior Engineer Jonas, Inc. Wilmington, Delaware longer blades) resulted in increased stresses and vibration Otakar Jonas is a Consultant with Jonas, Inc., in Wilmington, problems and in the use of higher strength materials (Scegljajev, Delaware. He works in the field of industrial and utility steam cycle 1983; McCloskey, 2002; Sanders, 2001). Unacceptable failure corrosion, water and steam chemistry, reliability, and failure analysis. rates of mostly blades and discs resulted in initiation of numerous After periods of R&D at Lehigh University and engineering projects to investigate the root causes of the problems (McCloskey, practice at Westinghouse Steam Turbine Division, Dr. Jonas started 2002; Sanders, 2001; Cotton, 1993; Jonas, 1977, 1985a, 1985c, his company in 1983. The company is involved in troubleshooting, 1987; EPRI, 1981, 1983, 1995, 1997d, 1998a, 2000a, 2000b, 2001, R&D (EPRI, GE, Alstom), failure analysis, and in the production 2002b, 2002c; Jonas and Dooley, 1996, 1997; ASME, 1982, 1989; of special instruments and sampling systems. Speidel and Atrens, 1984; Atrens, et al., 1984). Some of these Dr. Jonas has a Ph.D. degree (Power Engineering) from the problems persist today. Cost of corrosion studies (EPRI, 2001a, Czech Technical University. He is a registered Professional Syrett, et al., 2002; Syrett and Gorman, 2003) and statistics (EPRI, Engineer in the States of Delaware and California. 1985b, 1997d; NERC, 2002) determined that amelioration of turbine corrosion is urgently needed. Same problems exist in smaller industrial turbines and the same solutions apply Lee Machemer is a Senior Engineer at Jonas, Inc., in Wilmington, (Scegljajev, 1983; McCloskey, 2002; Sanders, 2001; Cotton, 1993; Delaware. -
PATROL COMBATANT MISSILE HYDROFOIL- DESIGN DEVELOPMENT and PRODUCTION- a BRIEF HISTORY by David S
PATROL COMBATANT MISSILE HYDROFOIL- DESIGN DEVELOPMENT AND PRODUCTION- A BRIEF HISTORY by David S. Oiling and Richard G. Merritt Boeing Marine Systems Published as Boeing Document 0312-80948-1, December 1980, and in the January-February issue of IIHigh-Speed Surface Craft," London ABOUT THE AUTHORS DAVID S. OLLING - Mechanical Specialist Engineer, PHM Variants Preliminary Design BS, Mechanical Engineering, University of Washington, 1967 With Boeing 21 years o 17 years in Advanced Marine Systems design, preliminary design, engineering liaison and testing organizations RICHARD G. MERRITT - Manager of PHM Variants Preliminary Design BS, Civil Engineering, Yale University, 1950 MS, Civil Engineering, California Institute of Technology, 1951 Degree of Civil Engineer, California Institute of Technology, 1953 Executive Program in Business Administration, Columbia University, 1967 With Boeing 17 years o 1 year as engineer with U.S. Naval Ordnance Test Station, Pasadena, before joining Boeing. o 6 years on airplane and missile system structural research. o 21 years in advanced marine system technology management, including supervision of hydrofoil technology staff, project design, and preliminary design groups. o Member of American Institute of Aeronautics and Astronautics, serving on AIAA technical committee on marine systems and technology. o Author of 12 articles in scientific and professional journals. PATROL COMBATANT MISSILE (HYDROFOIL) Design, Development and Production - A Brief History by David S. OUing and Richard G. Merritt, Boeing Marine Systems INTRODUCTION 1974. Its completion (PHM 2) was later incorporated into the production program, In 1972 three NATO navies formally agreed reference 3. to proceed with the joint development of a warship pro ject. The United States took the Major Events leadership before the "Memorandum of Understanding" was signed by the Federal Developing a new, sophisticated naval ship Republic of Germany and Italy and awarded system requires a considerable investment a letter contract to The Boeing Company of time, talent and money.