Engine Holdings of the National Air and Space Museum

Total Page:16

File Type:pdf, Size:1020Kb

Engine Holdings of the National Air and Space Museum Engine Holdings of The National Air and Space Museum (08-12-2002) Air Technical Arsenal TSU-11 (Hitachi Hatsukaze Ha 11 Model 11 Horizontally-Opposed 4, Continental C85-FJ, Pitts S-1C and Jet) Horizontally-Opposed 4, Lycoming O-145-B2 Barrel Diesel 9, SPECO XB-4070-2 Horizontally-Opposed 4, Porsche Type 678/1 Barrell 12, Speco, Michell, Crankless Horizontally-Opposed 4, Voyager-200 Double V, Allison V-3420-23 (V-3420-B10) Horizontally-Opposed 6, Aircooled Motors (Franklin) 0-405-9 Engine, Boeing B-17D Horizontally-Opposed 6, Aircooled Motors (Franklin) O-335-5D Engine, Boeing B-17D Horizontally-Opposed 6, Aircooled Motors (Franklin) XO-425-3 Engine, De Havilland DH-98 B/TT Mk. 35 Mosquito Horizontally-Opposed 6, Continental C-125-2 Engine, De Havilland DH-98 B/TT Mk. 35 Mosquito Horizontally-Opposed 6, Continental O-470-11B Engine, Douglas XB-42A Horizontally-Opposed 6, Lycoming AEIO-540-D4A5 Engine, Douglas XB-42A Horizontally-Opposed 6, Lycoming O-480-1B (GSO-480-B1B6) Engine, Ford 5-AT Tri-motor Horizontally-Opposed 6, Lycoming O-540-A3D5 Engine, General Electric J47, North American F-86A Sabre Horizontally-Opposed 6, Lycoming XO-435-7 Engine, Jumo 004, Messerschmitt Me 262A-1a Schwalbe In-line 1, De Dion-Bouton (Swallow) In-line 16, King-Bugatti Engine, Jumo 004, Messerschmitt Me 262A-1a Schwalbe In-line 3, Elbridge Featherweight (Swallow) In-line 4, Curtiss C-4 or D-4 Engine, Junkers Ju 388L-1 In-line 4, Curtiss E-4 Engine, Junkers Ju 388L-1 In-line 4, Curtiss E-4 Engine, Junkers Jumo 004, Arado Ar 234B-2 Blitz (Lightning) In-line 4, Curtiss Model K Engine, Junkers Jumo 004, Arado Ar 234B-2 Blitz (Lightning) In-line 4, Hall-Scott A-1, 1911-1912 Engine, Lockheed XC-35 Electra In-line 4, Hall-Scott A-7-A Engine, Lockheed XC-35 Electra In-line 4, Hall-Scott A-7-A Engine, Lycoming 0-145-B2, Curtiss-Wright CW-1 Junior In-line 4, Heath-Henderson B-4 Engine, Martin B-26B-25-MA "Flak- Bait" In-line 4, Honda Civic Engine, Martin B-26B-25-MA "Flak- Bait" In-line 4, Kemp (Grey Eagle) I-4 or D-4 Engine, Messerschmitt Me 410A-3/U1 Hornisse (Hornet) In-line 4, Maximotor B-4 Engine, Messerschmitt Me 410A-3/U1 Hornisse (Hornet) In-line 4, Michigan Aero-Engine Corporation Rover L-267 Engine, Nakajima B6N2 Tenzan (Heavenly Mountain) JILL In-line 4, Roberts 4X Engine, Nakajima C6N1-S Saiun (Painted Cloud) Myrt In-line 4, Roberts 4X Engine, Nakajima Ki-115a Tsurugi (Sabre) In-line 4, Roberts 4X Engine, Republic F-105D Thunderchief In-line 4, Wright Vertical 4 Engine, Waterman Whatsit In-line 4, Wright Vertical 4 Engine, Yokosuka P1Y1 Ginga (Milky Way) "Frances" In-line 6 (12) Diesel, Junkers Jumo 207 D-V2 Engine, Yokosuka P1Y1 Ginga (Milky Way) "Frances" In-line 6, Argus As III H-24, Fairchild Ranger XH-1850-2 In-line 6, Argus As III DZ H-24, Lycoming XH-2470-1 In-line 6, Benz BZ 4S H-24, Lycoming XH-2470-7 In-line 6, BMW Model IIIA H-24, Napier-Halford Dagger Series II In-line 6, Curtiss K-6 Horizontally-Opposed 12, Aircooled Motors (Franklin) O-805-2 In-line 6, Curtiss Model S Horizontally-Opposed 12, Diesel Napier Nomad Model E. 145 In-line 6, Curtiss Ricardo R-6 Horizontally-Opposed 2, A.B.C. Gnat In-line 6, Daimler-Motoren (Mercedes) DIII Avu Horizontally-Opposed 2, Aeronca E-113 In-line 6, De Havilland Gipsy Queen Q70 Mk II Horizontally-Opposed 2, Bates Model 2 B In-line 6, Fiat A-12 Bis Horizontally-Opposed 2, Daimler-Motoren (Mercedes) Type F- In-line 6, Isotta-Fraschini V-6 7502 In-line 6, Kirkham B-6 Horizontally-Opposed 2, Daimler-Motoren (Mercedes) Type F- In-line 6, Maybach 200 shp 7502 In-line 6, Maybach AZ Horizontally-Opposed 2, Detroit In-line 6, Maybach MB IVa Horizontally-Opposed 2, Dutheil-Chalmers In-line 6, Opel (Argus) Type III Horizontally-Opposed 2, Excelsior (Lawrance) A-3 In-line 6, Packard Model 1A-1551 Horizontally-Opposed 2, Kemp G-2 In-line 6, Roberts 6X Horizontally-Opposed 2, Wright Morehouse WM-80 In-line 6, Sturtevant D-6 Horizontally-Opposed 24, Napier Sabre IIA In-line 6, Union Type 1-6 Horizontally-Opposed 4, Aircooled Motors (Franklin) 4AC-171 In-line 6, Union Type 2-6 Horizontally-Opposed 4, Continental A-40 In-line 6, Wright 6-60 Horizontally-Opposed 4, Continental A-50 In-line 6, Wright 6-70 Horizontally-Opposed 4, Continental A-65-8 In-line 6, Wright D-1 Horizontally-Opposed 4, Continental A-65-8S Inverted In-line 4, Erco I-L 116 Horizontally-Opposed 4, Continental C-75 Inverted In-line 4, Hirth 500-B1 Horizontally-Opposed 4, Continental C-75 Inverted In-line 4, Hitachi Hatsukaze 11, Ha 11 Model 11 (Hirth) Inverted In-line 4, Hitachi Hatsukaze 11, Ha 11 Model 11 (Hirth) Radial 14, Mitsubishi Type 1, Ha 31 Model 21 (Ha 102), Kawasaki Inverted In-line 4, Martin 4-333 Ki-45 KAIc Hei ( Inverted In-line 6, Fairchild Ranger L-440-1 (6-440-C2) Radial 14, Nakajima Ha 105 Toku Inverted In-line 6, Fairchild Ranger L-440-3 (6-440-C5) Radial 14, Nakajima Ha 35 Model 21 Inverted In-line 6, Menasco Buccaneer B6S Radial 14, Nakajima Mamoru 11 Inverted Twin V-12 (Coupled), Daimler-Benz DB 610 Radial 14, Nakajima Type 2, Ha 34 Model 11 Inverted V-12, Aichi Atsuta 31, Ha 60 Model 31 Radial 14, Pratt & Whitney Twin Hornet R-2180 E1 Inverted V-12, Aichi Atsuta 32, Ha 60 Model 32 Radial 14, Pratt & Whitney Twin Wasp R-1830-90C (R-1830- Inverted V-12, Aichi Atsuta Model 30 Series S3C4-G) Inverted V-12, Continental Hyper I-1430-11 Radial 14, Pratt & Whitney Twin Wasp R-1830-43 Inverted V-12, Continental Hyper XI-1430-15 Radial 14, Pratt & Whitney Twin Wasp R-1830-92 Inverted V-12, Daimler-Benz DB 601-1E Radial 14, Pratt & Whitney Twin Wasp R-2000 Inverted V-12, Daimler-Benz DB 603 A, Heinkel He 219A-2 Uhu Radial 14, Pratt & Whitney Twin Wasp R-2000 (2SD13-G) (Eagle Owl) Radial 14, Sleeve Valve Continental XR-1740-2 Inverted V-12, Daimler-Benz DB 603 A, Heinkel He 219A-2 Uhu Radial 14, Wright Cyclone GR-2600-A2A (Eagle Owl) Radial 14, Wright Cyclone R-2600-13 (GR-2600-B655) Inverted V-12, Daimler-Benz DB 603 A-2 Radial 14, Wright Cyclone R-2600-13 (GR-2600-B655) Inverted V-12, Daimler-Benz DB 605 Radial 14, Wright Cyclone R-2600-8 Inverted V-12, Deschamps Diesel Radial 18, Mitsubishi Ha 42 Model 41 Ru (Ha 214 Ru) Inverted V-12, Fairchild Ranger V-770-15 (SGV-770C-1C) Radial 18, Mitsubishi Ha 43 Model 11 (Ha 211 Ru) Inverted V-12, Fairchild Ranger V-770-8 (SGV-770C-2) Radial 18, Mitsubishi Ha 43 Model 11 Ru (Ha 211 Ru) Inverted V-12, Junkers Jumo 210 D Radial 18, Mitsubishi Ha 43 Model 11 Ru (Ha 211 Ru) Inverted V-12, Junkers Jumo 211 Radial 18, Nakajima Ha 44 Model 12 Ru (Ha 219 Ru) Inverted V-12, Junkers Jumo 211-9 Radial 18, Nakajima Homare 12, Ha 45 Model 12 Inverted V-12, Junkers Jumo 211-9 Radial 18, Nakajima Homare 12, Ha 45 Model 12 Inverted V-12, Junkers Jumo 213 Radial 18, Nakajima Homare 12, Ha 45 Model 12 Inverted V-12, Junkers Jumo 213A-1 Radial 18, Nakajima Homare 21 Ru, Ha 45 Model 21 Ru Inverted V-12, Naval Aircraft Factory XV-715-2 Radial 18, Nakajima Homare 21, Ha 45 Model 21 Inverted V-12, Packard 2A-1500 Radial 18, Pratt & Whitney Double Wasp R-2800 CB16 Inverted V-12, Shoda-Hikoki Shoda-Ken No. 1 Radial 18, Pratt & Whitney Twin Wasp R-2800-43 Inverted V-16, Chrysler XI-2220-11 Radial 18, Pratt and Whitney Double Wasp R-2800-52W Inverted V-8, Argus As 10 R Radial 18, Pratt and Whitney Double Wasp R-2800-52W Mock-up (wood), Engine, Turbojet, Air Technical Arsenal TR-30 Radial 18, Pratt and Whitney Double Wasp R-2800-52W Propeller, Horizontally-Opposed 2, Bates Model 2 B Radial 18, Pratt and Whitney Double Wasp R-2800-52W Propeller, Turboprop Radial 18, Pratt and Whitney Double Wasp R-2800-52W Pulse Reactor, Hiller "Six Pack" Radial 18, Salmson Type Z18 Pulsejet, Marquardt (General Tire and Rubber Company) 12 Inch Radial 18, Wright Cyclone GR-3350 Diameter Radial 18, Wright Cyclone R-3350-14 Pulsejet, Marquardt (General Tire and Rubber) 8 Inch Diameter Radial 18, Wright Cyclone R-3350-23 (670C18BA3) Pulsejet, McDonnell XPJ40-MD-2 Radial 18, Wright Cyclone R-3350-57 Pulsejet, SNECMA Escopette Radial 18, Wright Cyclone R-3350-57AM Radial 9, Diesel Guiberson XR-918-2 Radial 18, Wright Cyclone R-3350-65 (787C18BC5) Radial 10, Anzani-Brownback 10 (105 x 140) Radial 18, Wright Cyclone R-3350-91TC Radial 12, Curtiss Chieftain H-1640 Radial 18, Wright Turbo-Cyclone 18R-3350-TC (972TC18DA2) Radial 12, Wright CH-2120 Radial 28, Pratt & Whitney Wasp Major XR-4360-4 Radial 12, Wright XR-2120 Radial 28, Pratt & Whitney Wasp Major XR-4360-43 Radial 14, BMW 801 Radial 28, Pratt and Whitney Wasp Major R-4360, Cutaway Radial 14, BMW 801 Radial 28, Pratt and Whitney Wasp Major R-4360-4A Radial 14, BMW 801C Radial 28, Pratt and Whitney Wasp Major R-4360-B6 Radial 14, Bristol Hercules VI Radial 3, Anzani A 2 Radial 14, Fiat A-74-RC-38 Radial 3, Lawrance L-3 Radial 14, Gnome-Rhone 14M-8 Radial 36, Lycoming XR-7755-3 Radial 14, Gnome-Rhone Mistral Major 14N Radial 4 Radial 14, Mitsubishi Army Type 1, Ha 31 Model 21 (Ha 102) Radial 4 (8), General Motors X-250 Radial 14, Mitsubishi Kasei 11, Ha 32 Model 11 Radial 4 (8), General Motors X-250 Radial 14, Mitsubishi Kasei 12, Ha 32 Model 12 Radial 4, Albisser Radial 14, Mitsubishi Kasei 15, Ha 32 Model 15 Radial 4, Fairchild Caminez 447-C Radial 14, Mitsubishi Kasei 21, Ha 32 Model 21 Radial 4, Fairchild Caminez 447-C Radial 14, Mitsubishi Kasei 22, Ha 32 Model 22 Radial 4, Fairchild Caminez 447-C Radial 14, Mitsubishi Kasei 22, Ha 32 Model 22 (MK4Q) Radial 5, Kinner K-5 Radial 14, Mitsubishi Kasei 26, Ha 32 Model 26 Radial 5, Kinner R-540, Cutaway Radial 14, Mitsubishi Kasei Ha 32 Model 25B Radial 5, Kinner R-540-1M (R-55) Radial 14, Mitsubishi Kasei Ha 34 (Tentative Identification))
Recommended publications
  • Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory figures As of Sept
    Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2014. By Aaron M. U. Church, Associate Editor I 2015 USAF Almanac BOMBER AIRCRAFT flight controls actuate trailing edge surfaces that combine aileron, elevator, and rudder functions. New EHF satcom and high-speed computer upgrade B-1 Lancer recently entered full production. Both are part of the Defensive Management Brief: A long-range bomber capable of penetrating enemy defenses and System-Modernization (DMS-M). Efforts are underway to develop a new VLF delivering the largest weapon load of any aircraft in the inventory. receiver for alternative comms. Weapons integration includes the improved COMMENTARY GBU-57 Massive Ordnance Penetrator and JASSM-ER and future weapons The B-1A was initially proposed as replacement for the B-52, and four pro- such as GBU-53 SDB II, GBU-56 Laser JDAM, JDAM-5000, and LRSO. Flex- totypes were developed and tested in 1970s before program cancellation in ible Strike Package mods will feed GPS data to the weapons bays to allow 1977. The program was revived in 1981 as B-1B. The vastly upgraded aircraft weapons to be guided before release, to thwart jamming. It also will move added 74,000 lb of usable payload, improved radar, and reduced radar cross stores management to a new integrated processor. Phase 2 will allow nuclear section, but cut maximum speed to Mach 1.2. The B-1B first saw combat in and conventional weapons to be carried simultaneously to increase flexibility. Iraq during Desert Fox in December 1998.
    [Show full text]
  • Modelado Del Turborreactor General Electric J85-13 Mediante Catia V5 Ingeniería Aeronáutica
    PROYECTO FIN DE CARRERA MODELADO DEL TURBORREACTOR GENERAL ELECTRIC J85-13 MEDIANTE CATIA V5 INGENIERÍA AERONÁUTICA Página | 1 FÉLIX RENTERO DE LLANO HOJA INTENCIONALMENTE DEJADA EN BLANCO Página | 2 Félix Rentero de Llano MODELADO DEL TURBORREACTOR GENERAL ELECTRIC J85-13 MEDIANTE CATIA V5 MODELADO DEL TURBORREACTOR GENERAL ELECTRIC J85-13 MEDIANTE CATIA V5 PROYECTO FIN DE CARRERA Autor Félix Rentero de Llano Tutores Juan Martínez Palacios María Gloria del Río Cidoncha Departamento de Ingeniería Gráfica Escuela Técnica Superior de Ingeniería Universidad de Sevilla Página | 3 Félix Rentero de Llano MODELADO DEL TURBORREACTOR GENERAL ELECTRIC J85-13 MEDIANTE CATIA V5 HOJA INTENCIONALMENTE DEJADA EN BLANCO Página | 4 Félix Rentero de Llano MODELADO DEL TURBORREACTOR GENERAL ELECTRIC J85-13 MEDIANTE CATIA V5 Índice PARTE I. INTRODUCCIÓN 1. OBJETIVO..................................................................................... 12 2. MOTIVACIÓN Y UTILIDAD ............................................................. 12 3.METODOLOGÍA ............................................................................. 12 4.ESTRUCTURA ................................................................................ 13 PARTE II. GENERAL ELECTRIC J85-13 5.HISTORIA Y MODELOS PREVIOS ...................................................... 16 6.GENERAL ELECTRIC J85 ................................................................. 18 6.1 Desarrollo ........................................................................................................
    [Show full text]
  • Turbocompound Reheat Gas Turbine Combined Cycle 2015
    INFRASTRUCTURE MINING & METALS NUCLEAR, SECURITY & ENVIRONMENTAL OIL, GAS & CHEMICALS Turbocompound Reheat Gas Turbine Combined Cycle 2015 Turbocompound Reheat Gas Turbine Combined Cycle S. Can Gülen Mark S. Boulden Bechtel Infrastructure Power POWER-GEN INTERNATIONAL 2015 December 8 - 10, 2015 Las Vegas Convention Center Las Vegas, NV USA ABSTRACT This paper discusses a new power generation cycle based on the fundamental thermodynamic concepts of constant volume combustion and reheat. The turbo- compound reheat gas turbine combined cycle (TC-RHT GTCC) comprises three pieces of rotating equipment: A turbo-compressor and two prime movers, i.e., a reciprocating gas engine and an industrial (heavy duty) gas turbine. Ideally, the cycle is proposed as the foundation of a customized power plant design of a given size and performance by combining different prime movers with new "from the blank sheet" designs. Nevertheless, a compact power plant based on the TC-RHT cycle can also be constructed by combining off-the-shelf equipment with modifications for immediate implementation. The paper describes the underlying thermodynamic principles, representative cycle calculations and value proposition as well as requisite modifications to the existing hardware. The operational philosophy governing plant start-up, shut-down and loading is described in detail. Also included in the paper is a 110 MW reference power block concept with 57+% net efficiency. The concept has been developed using a pre-engineered standard block approach and is amenable to simple “module-by-module” construction including easy shipment of individual components. POWER-GEN INTERNATIONAL 2015 Page 1 OF 26 INTRODUCTION Brief History Internal combustion engines can be classified into two major categories based on the heat addition portion of their respective thermodynamic cycles: “constant volume” and “constant pressure” heat addition engines (cycles) [1].
    [Show full text]
  • The TSR-2: a BRITISH STORY with an AUSTRALIAN CHAPTER
    RAAF Radschool Association Magazine – Vol 32 Page 15 The TSR-2: A BRITISH STORY WITH AN AUSTRALIAN CHAPTER With the era of the F-111 coming to a close, it is timely to reflect on the development of this aircraft and the rivals that existed at the time of its selection. The principal competitor was the British Aircraft Corporation’s Tactical Strike and Reconnaissance (TSR-2) aircraft. However, as indicated by Sir Sydney Camm’s comment, the development and subsequent abrupt cancellation of the project in 1965 was politically charged. While it was suggested at the time that Australia played a key role in the demise of the TSR-2, there appears to have been many other contributors to its downfall. From the mid 1950s, the RAF and subsequently the RAAF identified the need to replace the Canberra bomber, focusing on a nuclear-capable aircraft. Given the rapid advances in anti-aircraft weaponry capability, having supersonic strike aircraft that could slip under radar surveillance was seen as a priority. The development of the TSR-2 was also the result of the British Government’s focus in the late 1950s on rationalising the eight main British aircraft manufacturers that then existed. On New Year’s Day 1959, Vickers-Armstrong and English Electric, amalgamated as the new British Aircraft Corporation (BAC), were awarded the contract to combine their earlier individual designs into the TSR-2. Later that year Bristol- Siddeley were awarded the contract for development of the Olympus engines which were to power the aircraft. Like the development of any aircraft, the TSR-2 had its technical problems.
    [Show full text]
  • Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept
    Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2011. ■ 2012 USAF Almanac Bombers B-1 Lancer Brief: A long-range, air refuelable multirole bomber capable of flying intercontinental missions and penetrating enemy defenses with the largest payload of guided and unguided weapons in the Air Force inventory. Function: Long-range conventional bomber. Operator: ACC, AFMC. First Flight: Dec. 23, 1974 (B-1A); Oct. 18, 1984 (B-1B). Delivered: June 1985-May 1988. IOC: Oct. 1, 1986, Dyess AFB, Tex. (B-1B). Production: 104. Inventory: 66. Aircraft Location: Dyess AFB, Tex.; Edwards AFB, Calif.; Eglin AFB, Fla.; Ellsworth AFB, S.D. Contractor: Boeing, AIL Systems, General Electric. Power Plant: four General Electric F101-GE-102 turbofans, each 30,780 lb thrust. Accommodation: pilot, copilot, and two WSOs (offensive and defensive), on zero/zero ACES II ejection seats. Dimensions: span 137 ft (spread forward) to 79 ft (swept aft), length 146 ft, height 34 ft. B-1B Lancer (SSgt. Brian Ferguson) Weight: max T-O 477,000 lb. Ceiling: more than 30,000 ft. carriage, improved onboard computers, improved B-2 Spirit Performance: speed 900+ mph at S-L, range communications. Sniper targeting pod added in Brief: Stealthy, long-range multirole bomber that intercontinental. mid-2008. Receiving Fully Integrated Data Link can deliver nuclear and conventional munitions Armament: three internal weapons bays capable of (FIDL) upgrade to include Link 16 and Joint Range anywhere on the globe. accommodating a wide range of weapons incl up to Extension data link, enabling permanent LOS and Function: Long-range heavy bomber.
    [Show full text]
  • The Application Rationale for Applying the Regenerative Rankine Cycle Steam Engine to the Modern Automobile
    THE APPLICATION RATIONALE FOR APPLYING THE REGENERATIVE RANKINE CYCLE STEAM ENGINE TO THE MODERN AUTOMOBILE. The regenerative Rankine cycle positive displacement steam engine is ideal for powering any road vehicle. The engine speed/torque output closely matches vehicle demand; sufficient torque is generated that most vehicles require no transmission. This external combustion engine needs no pollution control hardware or electronics to provide totally clean combustion when burning pure carbon neutral bio fuels. Historically, material limitations have prevented vehicular steam power from receiving the advanced development and higher level of operation needed to compete with internal combustion engines. Only in huge powerhouses has the Rankine steam cycle been taken to the highest level of efficiency possible with existing materials; working with supercritical pressure of 3400-4400 psi and peak superheat temperature of 1400° F. The commercial availability of better materials makes a good reason to reassess the vehicular Rankine cycle steam engine. (Definition: Supercritical steam generators commonly used for electrical power generation typically operate at, or over, the supercritical pressure of 3206 psi at 706°F. At such high pressure and temperature boiling ceases to occur because the pressure is above the critical point where the bubbles form. Supercritical pressure steam generators are classified as “boilers” yet no "boiling" actually occurs.) By James Crank and Ken Helmick 1-25-15 INTRODUCTION. In ancient Greece, Heron of Alexandra used the heat from fire to produce work. Since the 16th Century many working cycles have been invented and used to produce shaft power from heat. The first real steam powered device was invented by Thomas Savery in 1698 to pump water from mines in England.
    [Show full text]
  • Aircraft Collection
    A, AIR & SPA ID SE CE MU REP SEU INT M AIRCRAFT COLLECTION From the Avenger torpedo bomber, a stalwart from Intrepid’s World War II service, to the A-12, the spy plane from the Cold War, this collection reflects some of the GREATEST ACHIEVEMENTS IN MILITARY AVIATION. Photo: Liam Marshall TABLE OF CONTENTS Bombers / Attack Fighters Multirole Helicopters Reconnaissance / Surveillance Trainers OV-101 Enterprise Concorde Aircraft Restoration Hangar Photo: Liam Marshall BOMBERS/ATTACK The basic mission of the aircraft carrier is to project the U.S. Navy’s military strength far beyond our shores. These warships are primarily deployed to deter aggression and protect American strategic interests. Should deterrence fail, the carrier’s bombers and attack aircraft engage in vital operations to support other forces. The collection includes the 1940-designed Grumman TBM Avenger of World War II. Also on display is the Douglas A-1 Skyraider, a true workhorse of the 1950s and ‘60s, as well as the Douglas A-4 Skyhawk and Grumman A-6 Intruder, stalwarts of the Vietnam War. Photo: Collection of the Intrepid Sea, Air & Space Museum GRUMMAN / EASTERNGRUMMAN AIRCRAFT AVENGER TBM-3E GRUMMAN/EASTERN AIRCRAFT TBM-3E AVENGER TORPEDO BOMBER First flown in 1941 and introduced operationally in June 1942, the Avenger became the U.S. Navy’s standard torpedo bomber throughout World War II, with more than 9,836 constructed. Originally built as the TBF by Grumman Aircraft Engineering Corporation, they were affectionately nicknamed “Turkeys” for their somewhat ungainly appearance. Bomber Torpedo In 1943 Grumman was tasked to build the F6F Hellcat fighter for the Navy.
    [Show full text]
  • EASA AD No.: 2018-0211
    EASA AD No.: 2018-0211 Airworthiness Directive AD No.: 2018-0211 Issued: 28 September 2018 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EU) 2018/1139 on behalf of the European Union, its Member States and of the European third countries that participate in the activities of EASA under Article 129 of that Regulation. This AD is issued in accordance with Regulation (EU) 748/2012, Part 21.A.3B. In accordance with Regulation (EU) 1321/2014 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Consequently, no person may operate an aircraft to which an AD applies, except in accordance with the requirements of that AD, unless otherwise specified by the Agency [Regulation (EU) 1321/2014 Annex I, Part M.A.303] or agreed with the Authority of the State of Registry [Regulation (EU) 2018/1139, Article 71 exemption]. Design Approval Holder’s Name: Type/Model designation(s): CFM INTERNATIONAL S.A. CFM56-7B engines Effective Date: 05 October 2018 TCDS Number(s): EASA.E.004 Foreign AD: Not applicable Supersedure: This AD supersedes EASA AD 2018-0109 dated 17 May 2018. ATA 72 – Engine – Fan Blades – Inspection Manufacturer(s): SAFRAN Aircraft Engines, formerly SNECMA (France); General Electric Aircraft Engines (United States) Applicability: CFM56-7B20, CFM56-7B22, CFM56-7B22/B1, CFM56-7B24, CFM56-7B24/B1, CFM56-7B26, CFM56-7B26/B1, CFM56-7B26/B2, CFM56-7B27, CFM56-7B27/B1, CFM56-7B27/B3, CFM56-7B20/2, CFM56-7B22/2, CFM56-7B24/2, CFM56-7B26/2,
    [Show full text]
  • Design Details of the Mitsubishi Kinsei Engine*
    ! THE CONDITION of the only conversion figures in the hope that physical engine available for study these figures will best serve the and the data readily available can purposes intended. form the basis for only a very The inspection indicates to the meager report. The study has, writer two possible conclusions however, been an interesting one which are presented herewith: and the results are recorded for what 1. That the group responsible for value they may have. The design the design did a very ingenious job comments are, of necessity, of a of combining what they apparently general nature — much the same as believed to be the most desirable those which would be made on the features of a number of products of preliminary layout of a new design. foreign manufacture — proved For the convenience of many of us features all. These features are built who habitually think in term s of into a composite design of the sort English units, these units are used that “has to work the first time” — even though a large portion of the and probably did. work is apparently based on the 2. That manufacturing methods metric system. As a result, the and equipment of manufacturers numerical data are approximate whose features were appropriated ! "# $ %% & ' () "# # *! "# # +, "# & ' % & ' % "# & % $' % % - % * General description of the engine appeared in “Aviation' s” report on the joint meeting of the Society of Automotive Engineering Detroit Section, and the Engineering Society of Detroit, June 8, 1942, in the article War Production of Aircraft, page 104, July, 1942. This additional material is presented through the courtesy of the SAE.
    [Show full text]
  • 2013 KIVA Development
    2013 DOE Merit Review 2013 KIVA Development David Carrington Los Alamos National Laboratory May 13, 2013 Project ID # ACE014 This presentation does not contain any proprietary, confidential, or otherwise restricted information LA-UR-13-21976 2013 DOE Overview Merit Review Timeline Barriers • Improve understanding of the fundamentals of • 10/01/09 fuel injection, fuel-air mixing, thermodynamic combustion losses, and in-cylinder combustion/ • 09/01/14 emission formation processes over a range of combustion temperature for regimes of interest • 65% complete by adequate capability to accurately simulate these processes • Engine efficiency improvement and engine- Budget out emissions reduction • Minimization of engine technology development • Total project funding to date: – User friendly (industry friendly) software, robust, accurate, more predictive, & quick meshing – 2000K – 640K in FY 12 Partners – Contractor (Universities) share ~40% • University of New Mexico- Dr. Juan Heinrich • University of Purdue, Calumet - Dr. Xiuling • Funding to date for FY13 - 210K Wang • Funding anticipated FY13 – 763K • University of Nevada, Las Vegas - Dr. Darrell W. Pepper 2 2013 DOE FY 09 to FY 14 KIVA-Development Merit Review Objectives • Robust, Accurate Algorithms in a Modular Object-Oriented code– • Relevance to accurately predicting engine processes to enable better understanding of, flow, thermodynamics, sprays, in easy to use software for moderate computer platforms – More accurate modeling requires new algorithms and their correct implementation. – Developing more robust and accurate algorithms • To understand better combustion processes in internal engines – Providing a better mainstay tool • improving engine efficiencies and • help in reducing undesirable combustion products. – Newer and mathematically rigorous algorithms will allow KIVA to meet the future and current needs for combustion modeling and engine design.
    [Show full text]
  • Practical-Mechanics
    JET OR REACTION PROPULSION Have YOU Joined the Well -paid Ranks of the TRAINED MEN? MANY THOUSANDS MORE ARE URGENTLY NEEDED. PREPARE YOURSELF FOR A MASTERPIECES 10- BETTER POSITION AND BETTER PAY IN MINIATURE! Ambitious men everywhere have succeeded through Long experience and consummate skillin the art of model making has made the name I.C.S. Home Study Courses. So also can you. We Bassett-Lowke famousfordetailperfect offer you the benefit of our 53 years' matchless ex- scale models ofallkinds.To -day we are fully engaged on work for H.M. Government, perience asthe creative pioneers of but as soon as victory is won we shall be " Building a air,. postal instruction.Since our establish- gaugeFlyingScots- ready to resume production of Model Rail- man," fully illustrated ways, Ships and Engines for all our customers. ment in1891, more than1,000,000 with drawings and photographs, priceII - Our London and Manchester branches are British men and women have enrolled post free. still open and our wartime staff will be pleased Wartime stock list to give assistance on any model matters. for I.C.S. Courses. (L/12) price 4d. post free. The man with an I.C.S. Training in any one of the subjects listedbelow knowsitthoroughly,completely,practically. BASSETT-LOW K E9 Ltd. And heknows how to applyitinhis everydaywork. NORTHAMPTON Accountancy Draughtsmanship Motor Engineering LONDON :112, HighHolborn, W.C.I. Advertising Drawing Office Practice Motor Mechanic MANCHESTER :28, Corporation Street. Aeronautical Engineering Electrical Engineering Moulding Aaro Engine Fitting Engineer in Charge Pattern making Aero Fitting and Rigging Eng. Shop Practice Quantity Surveying Aeroplane Designing Fire Engineering Radio Engineering Air -Conditioning Fitting and Turning Radio Servicing S.
    [Show full text]
  • The Aircraft Propulsion the Aircraft Propulsion
    THE AIRCRAFT PROPULSION Aircraft propulsion Contact: Ing. Miroslav Šplíchal, Ph.D. [email protected] Office: A1/0427 Aircraft propulsion Organization of the course Topics of the lectures: 1. History of AE, basic of thermodynamic of heat engines, 2-stroke and 4-stroke cycle 2. Basic parameters of piston engines, types of piston engines 3. Design of piston engines, crank mechanism, 4. Design of piston engines - auxiliary systems of piston engines, 5. Performance characteristics increase performance, propeller. 6. Turbine engines, introduction, input system, centrifugal compressor. 7. Turbine engines - axial compressor, combustion chamber. 8. Turbine engines – turbine, nozzles. 9. Turbine engines - increasing performance, construction of gas turbine engines, 10. Turbine engines - auxiliary systems, fuel-control system. 11. Turboprop engines, gearboxes, performance. 12. Maintenance of turbine engines 13. Ramjet engines and Rocket engines Aircraft propulsion Organization of the course Topics of the seminars: 1. Basic parameters of piston engine + presentation (1-7)- 3.10.2017 2. Parameters of centrifugal flow compressor + presentation(8-14) - 17.10.2017 3. Loading of turbine blade + presentation (15-21)- 31.10.2017 4. Jet engine cycle + presentation (22-28) - 14.11.2017 5. Presentation alternative date Seminar work: Aircraft engines presentation A short PowerPoint presentation, aprox. 10 minutes long. Content of presentation: - a brief history of the engine - the main innovation introduced by engine - engine drawing / cross-section -
    [Show full text]