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Hiduminium Technical Data
HIDUMINIUM TECHNICAL DATA HIGH DUTY ALLOYS LTD SLOUGH F oreword Extensive research carried out in recent years, com bined with an increasing demand for " H ID UM IN IUM " high tensile aluminium alloys, has necessitated the revision and increase of the series of data sheets pre viously issued by the Company. As before, our aim is to place before designers and constructors the fullest possible particulars regarding the physical and mechanical properties of " H ID U M IN IU M ," which will enable them to select the materials most suitable for their requirements and to adapt their designs in accordance with the outstanding character istics of this range of alloys. " HIDUMINIUM" is produced under conditions of strict scientific control and progressive inspection and a staff of expert Metallurgists, Research W orkers and Technicians is always ready to give advice on all problems connected with the use of these alloys. Fresh data, as it is revealed by further research, will be issued on additional sheets. This will ensure that all information contained in this volume is up-to-date and may thus be referred to at all times with complete confidence. HIGH DUTY ALLOYS LIMITED 3 CONTENTS Page Index to Specifications 6-9 Hiduminium 15 10-11 Hiduminium 23 12-13 Hiduminium 33 14-15 Hiduminium 35 16-17 H iduminium 40 & 42 18-19 Hiduminium 45 20-21 Hiduminium R.R. 50 22-23 Hiduminium R.R. 53 24-26 Hiduminium R.R. 53.C 27-29 Hiduminium R.R. 56 30-32 H iduminium R.R. 59 33-35 Hiduminium 72 36-37 Hiduminium R.R. -
LESSON 3 Significant Aircraft of World War II
LESSON 3 Significant Aircraft of World War II ORREST LEE “WOODY” VOSLER of Lyndonville, Quick Write New York, was a radio operator and gunner during F World War ll. He was the second enlisted member of the Army Air Forces to receive the Medal of Honor. Staff Sergeant Vosler was assigned to a bomb group Time and time again we read about heroic acts based in England. On 20 December 1943, fl ying on his accomplished by military fourth combat mission over Bremen, Germany, Vosler’s servicemen and women B-17 was hit by anti-aircraft fi re, severely damaging it during wartime. After reading the story about and forcing it out of formation. Staff Sergeant Vosler, name Vosler was severely wounded in his legs and thighs three things he did to help his crew survive, which by a mortar shell exploding in the radio compartment. earned him the Medal With the tail end of the aircraft destroyed and the tail of Honor. gunner wounded in critical condition, Vosler stepped up and manned the guns. Without a man on the rear guns, the aircraft would have been defenseless against German fi ghters attacking from that direction. Learn About While providing cover fi re from the tail gun, Vosler was • the development of struck in the chest and face. Metal shrapnel was lodged bombers during the war into both of his eyes, impairing his vision. Able only to • the development of see indistinct shapes and blurs, Vosler never left his post fi ghters during the war and continued to fi re. -
Connor Final Highlighted
Preliminary Development of a PPAM Actuated Pediatric Prosthetic Ankle Connor McNamara-Spackman A thesis submitted in partial fulfilment of the requirements for the degree of Master of Science (Bioengineering) at the University of Otago, Dunedin, New Zealand. February 2021 Abstract The purpose of this research was to develop a preliminary design of a powered pediatric prosthetic ankle. Previous research identified the health risk of improper gait cycle and the lack of powered prosthetic ankle options for children. Costs for powered prosthetic ankles are too high (upwards of $5000 NZD), the sizes are too large and the weight is too significant for a child to benefit from. Current technologies for ankle joint actuation and materials for the prosthetic structure were evaluated and a conclusion of utilizing PPAMs was chosen due to their ability to generate the required 300 N of contraction force. CAD was used to model the structure of a prosthetic ankle and evaluate the FOS of the different material combinations while under static loading and fatigue simulations. HDPE and UHMWPE failed to withstand the simulations, while the aluminium alloy and stainless steel showed minimal faults from the simulations. MatLab was used to simulate the desired PPAM dimensions of 100 mm to determine the contraction force and contraction percentage that can be generated by the PPAM. The smallest PPAM found in research was 110 mm and showed promising results from their mathematical modeling. The overall height of the prosthetic was no greater than 110 mm and the membrane length of the PPAM was no greater than 100 mm, while successfully producing more than 300 N during contraction. -
Military Aircraft Crash Sites in South-West Wales
MILITARY AIRCRAFT CRASH SITES IN SOUTH-WEST WALES Aircraft crashed on Borth beach, shown on RAF aerial photograph 1940 Prepared by Dyfed Archaeological Trust For Cadw DYFED ARCHAEOLOGICAL TRUST RHIF YR ADRODDIAD / REPORT NO. 2012/5 RHIF Y PROSIECT / PROJECT RECORD NO. 105344 DAT 115C Mawrth 2013 March 2013 MILITARY AIRCRAFT CRASH SITES IN SOUTH- WEST WALES Gan / By Felicity Sage, Marion Page & Alice Pyper Paratowyd yr adroddiad yma at ddefnydd y cwsmer yn unig. Ni dderbynnir cyfrifoldeb gan Ymddiriedolaeth Archaeolegol Dyfed Cyf am ei ddefnyddio gan unrhyw berson na phersonau eraill a fydd yn ei ddarllen neu ddibynnu ar y gwybodaeth y mae’n ei gynnwys The report has been prepared for the specific use of the client. Dyfed Archaeological Trust Limited can accept no responsibility for its use by any other person or persons who may read it or rely on the information it contains. Ymddiriedolaeth Archaeolegol Dyfed Cyf Dyfed Archaeological Trust Limited Neuadd y Sir, Stryd Caerfyrddin, Llandeilo, Sir The Shire Hall, Carmarthen Street, Llandeilo, Gaerfyrddin SA19 6AF Carmarthenshire SA19 6AF Ffon: Ymholiadau Cyffredinol 01558 823121 Tel: General Enquiries 01558 823121 Adran Rheoli Treftadaeth 01558 823131 Heritage Management Section 01558 823131 Ffacs: 01558 823133 Fax: 01558 823133 Ebost: [email protected] Email: [email protected] Gwefan: www.archaeolegdyfed.org.uk Website: www.dyfedarchaeology.org.uk Cwmni cyfyngedig (1198990) ynghyd ag elusen gofrestredig (504616) yw’r Ymddiriedolaeth. The Trust is both a Limited Company (No. 1198990) and a Registered Charity (No. 504616) CADEIRYDD CHAIRMAN: Prof. B C Burnham. CYFARWYDDWR DIRECTOR: K MURPHY BA MIFA SUMMARY Discussions amongst the 20th century military structures working group identified a lack of information on military aircraft crash sites in Wales, and various threats had been identified to what is a vulnerable and significant body of evidence which affect all parts of Wales. -
Suomen Ilmailuhistoriallinen Lehti
Sivu 1 Suomen Ilmailuhistoriallinen Lehti Artikkeliluettelo n:ot 1/1994 - 3/2018 Koostanut ja sisältökuvaukset laatinut H Paronen Lehden Alkava Kirjoittaja Artikkelin otsikko Pääsisältö 3-taho- numero sivu nr. piirus- tuksia 1994 1 2 Manninen P BZ-35 Ilmavoimien polttoaineauto BZ-35 tankkausauto on 1994 1 3 Manninen P Pääkirjoitus 1994 1 4 Manninen P Hurricane, venäläiset hävittäjät Sotasaaliskoneet Suomessa 1 1994 1 8 Manninen P Hawker Hurricane Mk. IIA ja IIB Kolmitahopiirros on 1994 1 14 Valtonen H In Memoriam Erkki Jaakkola Henkilöhistoria 1994 1 14 Erkki Jaakkolan albumista Fokker-koneita sodan jälkeen 1994 1 16 Manninen P Talvinaamiovärin keitto-ohje Kolmitahopiirros ja maaliohje on 1994 2 2 Kuva-albumi: Neljä kuvaa sodan jälkeen Erkki Jaakkolan kokoelma / K-SIM 1994 2 3 Manninen P Pääkirjoitus 1994 2 4 Valtonen H JABO/JG5 ja 4.&1./SG5 Petsamon Hävittäjäpommittajalentueen toiminta hävittäjäpommittajalentue (FW 190 A-2 ja A-3) 14.(JABO)/JG5, sekä 4. ja 1./SG5 Petsamossa 31.1.43-30.6.44 1994 2 9 LeR 3:n laivuetunnukset Harakka- ja ilves-tunnusten kesällä 1944 historiaa 1994 2 10 Ritaranta E Suomalainen taitolento 75 vuotta Henkilöhistoria Gunnar Holmqvistin lentäjänura 1994 2 12 Aviatsija Dalnego Deistvija Neuvostoliiton kaukotoiminta- ilmavoimat 1994 2 15 Risut ja ruusut 1994 2 15 Picture History of World War II Kirja-arvostelu American Aircraft Production. Kirj. Joshua Stoff 1994 2 16 Manninen P Junkers Ju 88 A-4 Profiilipiirrokset on 1994 3 2 Ilmavoimat Suursaaren operaatiossa Kuvia s. 4/nr. 2/94 alkavaan artikkeliin 1994 3 3 Manninen P Pääkirjoitus 1994 3 4 Stenman K Suursaari, Suursaaren valtauksen ilmahistoria, Ilmasotatoimet 20.3.-28.3.1942 osallistuneet ohjaajat ja koneet. -
Tribological Behaviours Influenced by Surface Coatings and Morphology
University of Windsor Scholarship at UWindsor Electronic Theses and Dissertations Theses, Dissertations, and Major Papers 7-11-2015 Tribological Behaviours Influenced yb Surface Coatings and Morphology Guang Wang University of Windsor Follow this and additional works at: https://scholar.uwindsor.ca/etd Recommended Citation Wang, Guang, "Tribological Behaviours Influenced yb Surface Coatings and Morphology" (2015). Electronic Theses and Dissertations. 5305. https://scholar.uwindsor.ca/etd/5305 This online database contains the full-text of PhD dissertations and Masters’ theses of University of Windsor students from 1954 forward. These documents are made available for personal study and research purposes only, in accordance with the Canadian Copyright Act and the Creative Commons license—CC BY-NC-ND (Attribution, Non-Commercial, No Derivative Works). Under this license, works must always be attributed to the copyright holder (original author), cannot be used for any commercial purposes, and may not be altered. Any other use would require the permission of the copyright holder. Students may inquire about withdrawing their dissertation and/or thesis from this database. For additional inquiries, please contact the repository administrator via email ([email protected]) or by telephone at 519-253-3000ext. 3208. Tribological Behaviours Influenced by Surface Coatings and Morphology By Guang Wang A thesis Submitted to the Faculty of Graduate Studies through the Department of Mechanical, Automotive & Materials Engineering in Partial Fulfillment of the Requirements for the Degree of Master of Applied Science at the University of Windsor Windsor, Ontario, Canada 2015 ©2015 Guang Wang Tribological Behaviours Influenced by Surface Coatings and Morphology By Guang Wang APPROVED BY: Dr. -
Norske Heinkel He 115
Norske Heinkel He 115 Tekst: Kjell Dahle Foto: billedmontasjer av modell v/Kjell Dahle Da Tyskland angrep Norge 9. april 1940 disponerte Marinens flyvåpen seks nye og moderne sjøfly. De deltok aktivt i forsvaret av landet, for det meste i oppgaver av typen transport og observasjon. Da Norge kapitulerte ble fire av flyene evakuert til Storbritannia. Teknisk beskrivelse. Utviklingen av Heinkel He 115 startet i 1935 av Ernst Heinkel Flugzeugwerke G.m.b.H. i Rostock i Tyskland. Flyene ble produsert tre serier (-A, -B, -C) i mange varianter. Flyet var designet for rekognosering, torpedobombing og minelegging, og ble produsert i ca 300 eksemplarer. Flyet var i helmetall med to kraftige BMV-motorer, besetning på tre. Flyene ble eksportert til Norge, Sverige, Finland og Bulgaria. Storbritannia overtok fire fly fra Norge. Marinens flyvåpen bestilte en modifisert versjon, med 20mm kanon i nesepartiet, og mitraljøse i bakre cockpit. Spesifikasjoner Heinkel He 115A-2(N): Vingespenn 22,30 m Lengde 17,30 m Høyde 6,60 m Nettovekt 5 300 kg Maksimal startvekt 9 1000 kg Topphastighet 320 km/t Marsjfart 285 km/t Topphøyde 5 500 m Rekkevidde 2500 km 2 stk BMV 132N 9 sylindret Motorer stjernemotor, 975 HK 1 stk mitraljøse Bestykning 1 stk 20 mm kanon En torpedo på 800 kg Våpenlast Tre 250 kgs bomber I norsk tjeneste. De seks flyene skulle erstatte de gamle torpedoflyene Douglas DT2B og MF11-flyene. Flyene ankom Horten august 1939, fløyet hit av norske flygere. Ytterligere seks fly var bestilt for levering i april 1940, men disse ble ikke levert. I september 1939 ble det vedtatt å opprette en nøytralitetsvakt på grunn av den spente situasjon i Europa, og de nye flyene ble fordelt på marinebasene rundt i landet. -
Maec.19 70 (University of London) London
COMPLEX & INCREMENTAL STRESS CREEP OF A HIGH STRENGTH ALUMINIUM ALLOY AT ELEVATED TEMPERATURES (ALLOY: HIDUMINIUM RR58 SPECIFICATION DTD 731) by SURINDAR BAHADUR MATHUR Thesis presented in the Department of Mechanical Engineering for the Award of the Doctor of Philosphy in Mechanical Engineering of the University of London. Mechanical Engineering Department Imperial College of Science and Technology mAec.19 70 (University of London) London. ABSTRACT A theory for creep rates under complex and incremental stresses is deduced from experimental data concerning complex creep at elevated temperatures for the test material HIDUMINIUM RR 58 - Specification DID 731. The most important results are for tubular specimens tested at 150°C and 250°C under incremental loads. The analysis of results relates to steady state creep only. Modified relationships in stress equivalence and strain equivalence are proposed to account for thermal softening, polygonization, recrystallization and the resulting exaggerated flow in the direction of the applied shear. (The original equations are based on the hypothesis of Von Mises). A further relationship is suggested between the immediate total energy of distortion and the subsequent creep work rate. Results of the static tests and the results of the tests for creep behaviour under complex loading are presented and compared with the results of static torsion and simple incremental torsion creep tests on the basis of the proposed equations. An appendix describes the complex creep testing machine, furnace, extensometers -
Inhaltsverzeichnis Seite Schrifttum 5 Abkürzungen 6 Einleitung I Waren
Inhaltsverzeichnis Seite Schrifttum 5 Abkürzungen 6 Einleitung i Waren. — Warenkunde. — Einteilung der Waren. — Hilfs- wissenschaften der Warenkunde 7— 8 I. Metalle und Metallwaren 8 A. Edelmetalle. 1. Gold. — 2. Silber. — 3. Platin. — 4. Queck- silber 10—18 B. Unedle Schwermetalle. 1. Eisen und Eisenwaren (Roh- eisen, schmiedbares Eisen, Erzeugnisse aus Eisen und Stahl). — 2. Kupfer. — 3. Blei. — 4. Zink. — 5. Zinn. — 6. Nickel. — 7. Arsen. — 8. Antimon. — 9. Wismut 18—35 C. Leichtmetalle. 1. Aluminium. — 2. Magnesium 35—37 D. Legierungen. 1. Bronze. — 2. Tombak. — 3. Messing. — 4. Neusilber. — 5. Konstantan .— 6. Britanniametall. — 7. Schriftmetall. — 8. Lagermetalle. — 9. Duralumin. — lO.Hydronalium. — 11. Silumin. —12. Elektron. — 13. Heus- ler'sche Legierungen 37—40 II. Edelsteine und Schmucksteine 40 A. Edelsteine. 1. Diamant. — 2. Rubin und Saphir. — 3. Spinell. — 4. Chrysoberyll. — 5. Smaragd. — 6. Topas. — 7. Zirkon. — 8. Granat. — 9. Türkis. — 10. Edelopal 41—46 B. Schmucksteine. 1. Quarz. — 2. Chalcedon. — S.Mond- stein. — 4. Lasurstein. — 5. Malachit. — 6. Blutstein. — 7. Bernstein 46—48 III. Bildhauersteine 48 1. Marmor. — 2. Alabaster. — 3. Serpentin. — 4. Meer- schaum. — 5. Talk 48—51 IV. Baustoffe 51 A. Bausteine. 1. Kalkstein. — 2. Sandsteine. — 3. Granit. — 4. Porphyr. — 5. Basalt. — 6. Magnesit. — 7. Kunststeine .... 51—53 B. Bindemittel. 1. Branntkalk. — 2. Zement. — 3. Gips 54—56 V. Schleif- und Glättemittel, Mühlsteine 57 1. Schleifsteine. — 2. Schmirgel. — 3. Gemeiner Korund. — 4. Siliziumkarbid. — 5. Bimsstein. — 6. Tripel. — 7. Polier- rot. — 8. Zinnasche. — 9. Wiener Kalk. — 10. Schlämm- kreide.—11. Mühlsteine 67—58 VI. Tonwaren 59 Ton. — 1. Porzellan. — 2. Steinzeug. — 3. Steingut. — 4. Töpferware. — 5. Ziegel. — 6. Feuerfeste Steine 59—67 VII. -
Extruded Aluminium Profiles
Aluminium Al Product format: Extruded Technical characteristics : Flats, rods, tubes and extruded aluminium profiles www.bronmetal.com Aluminium Al Product format: Extruded Technical Characteristics: Flats, rods, tubes and extruded aluminium profiles EQUIVALENCES 1050 PURE ALUMINIUM (99,5%) EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES ISO SPAIN GERMANY CANADA E.E.U.U. FRANCE UNITED KINGDOM ITALY OTHERS Al-99,5 L-3051 Al-99,5 Al-99,5 A5 1B 9001/2 17010 Puraltok 99,5 3,0255 1S Durcilium T 4007 WG-1S Hiduminium A1 1150/55 Impalco 0,5 Aluran 99,5 EQUIVALENCES 1200 PURE ALUMINIUM (99 %) EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES ISO SPAIN GERMANY CANADA E.E.U.U. FRANCE UNITED KINGDOM ITALY OTHERS Al 99,0 L-3001 Al 99,0 2S 1100 A-4 1C 3567 4010 Puraltok 99 3,0205 2S 1100 5090 WG-2S Birmetal 2 9001/1 17005 90 Hiduminium-1C 1008 1010 NA-2S 1191 2584 A0 Aluran 99 www.bronmetal.com Aluminium Al Product format: Extruded Technical Characteristics: Flats, rods, tubes and extruded aluminium profiles EQUIVALENCES 2007 ALUMINIUM-COPPER EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES SPAIN GERMANY FRANCE SUIZA L-3121 DIN 1725 A U4Pb Al-CuMgPb Cobreltok 07 DIN 1746 Al-CuMgCd DIN 1747 Decotal 200 Tordal 1970 Aludur D 505 Spanal 320 MFK Aludur 570 A Automat EQUIVALENCES 2011 ALUMINIUM-COPPER COMMERCIAL EQUIVALENT SPAIN CANADA E.E.U.U. FRANCE SUIZA ITALY UNITED KINGDOM L-3192 CB 60 2011 A-U5PbBi Decotal 500 Recidal 11 28 S 28-S CSA HA,5 ASTM B 211 Fortal 2011 28 S QQ-R-225/3 QQ-R-365 WW-P-471 Ty III QQ-R-566 www.bronmetal.com Aluminium Al Product format: Extruded Technical Characteristics: Flats, rods, tubes and extruded aluminium profiles EQUIVALENCES 2030 ALUMINIUM-COPPER EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES SPAIN GERMANY FRANCE SUIZA L-3121 Al CuMgPb A U4Pb Al-CuMgPb 3,1645 NF A 57.350 Al-CuMgCd DIN 1725 Fortal D Decotal 200 DIN 1746 Fortal 2030 Aludur D 505 DIN 1747 Carbium al Pbl MFK Tordal 1970 Duralumin DE Spanal 320 Aludur 570 A Automat EQUIVALENCES2014 ALUMINIUM-COPPER EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES ISO SPAIN GERMANY CANADA E.E.U.U. -
No. 138 Squadron Arrived Flying Whitleys, Halifaxes and Lysanders Joined the Following Month by No
Life Of Colin Frederick Chambers. Son of Frederick John And Mary Maud Chambers, Of 66 Pretoria Road Edmonton London N18. Born 11 April 1917. Occupation Process Engraver Printing Block Maker. ( A protected occupation) Married 9th July 1938 To Frances Eileen Macbeath. And RAFVR SERVICE CAREER OF Sergeant 656382 Colin Frederick Chambers Navigator / Bomb Aimer Died Monday 15th March 1943 Buried FJELIE CEMETERY Sweden Also Remembered With Crew of Halifax DT620-NF-T On A Memorial Stone At Bygaden 37, Hojerup. 4660 Store Heddinge Denmark Father Of Michael John Chambers Grandfather Of Nathan Tristan Chambers Abigail Esther Chambers Matheu Gidion Chambers MJC 2012/13 Part 1 1 Dad as a young boy with Mother and Grandmother Dad at school age outside 66 Pretoria Road Edmonton London N18 His Father and Mothers House MJC 2012/13 Part 1 2 Dad with his dad as a working man. Mum and Dad’s Wedding 9th July 1938 MJC 2012/13 Part 1 3 The full Wedding Group Dad (top right) with Mum (sitting centre) at 49 Pembroke Road Palmers Green London N13 where they lived. MJC 2012/13 Part 1 4 After Volunteering Basic Training Some Bits From Dads Training And Operational Scrapbook TRAINING MJC 2012/13 Part 1 5 Dad second from left, no names for rest of people in photograph OPERATIONS MJC 2012/13 Part 1 6 The Plane is a Bristol Blenheim On leave from operations MJC 2012/13 Part 1 7 The plane is a Wellington Colin, Ken, Johnny, Wally. Before being posted to Tempsford Navigators had to served on at least 30 operations. -
Friction Stir Welding of Dissimilar Materials Between Aluminium Alloys and Copper - an Overview
Proceedings of the World Congress on Engineering 2013 Vol III, WCE 2013, July 3 - 5, 2013, London, U.K. Friction Stir Welding of Dissimilar Materials between Aluminium Alloys and Copper - An Overview Mukuna P. Mubiayi. Member, IAENG and Esther T. Akinlabi, Member, IAENG flow in the material, forming a solid state weld. Abstract—Friction Stir Welding (FSW) is a solid state welding process used for welding similar and dissimilar materials. The process is widely used because it produces sound welds and does not have common problems such as solidification and liquefaction cracking associated with the fusion welding techniques. The FSW of Aluminium and its alloys has been commercialised; and recent interest is focused on joining dissimilar materials. However, in order to commercialise the process, research studies are required to characterise and establish process windows. In particular, FSW has inspired researchers to attempt joining dissimilar materials such as aluminium to copper which differ in properties and sound welds with none or limited intermetallic compounds has been produced. In this paper, we review the current research state of FSW between aluminium and copper with a focus on the resulting weld microstructure, mechanical testing and the tools employed to produce the welds and also an insight into future research in this field of study. Fig.1. Schematic diagram of the Friction Stir Welding process [2] Keywords: Aluminium, copper, dissimilar materials, intermetallic compounds, microstructure. It was realised in the development of the FSW process that the tool design is critical in producing sound welds [3]. A basic and conventional design for a FSW tool is shown in I.