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21 system
система; установка; устройство; ркт. комплекс"see to land" system — система посадки с визуальным приземлением
A.S.I. system — система указателя воздушной скорости
ablating heat-protection system — аблирующая [абляционная] система тепловой защиты
ablating heat-shield system — аблирующая [абляционная] система тепловой защиты
active attitude control system — ксм. активная система ориентации
aft-end rocket ignition system — система воспламенения заряда с задней части РДТТ [со стороны сопла]
aircraft response sensing system — система измерений параметров, характеризующих поведение ЛА
air-inlet bypass door system — дв. система перепуска воздуха на входе
antiaircraft guided missile system — ракетная система ПВО; зенитный ракетный комплекс
antiaircraft guided weapons system — ракетная система ПВО; зенитный ракетный комплекс
attenuated intercept satellite rendez-vous system — система безударного соединения спутников на орбите
attitude and azimuth reference system — система измерения или индикации углов тангажа, крена и азимута
automatic departure prevention system — система автоматического предотвращения сваливания или вращения после сваливания
automatic drift kick-off system — система автоматического устранения угла упреждения сноса (перед приземлением)
automatic hovering control system — верт. система автостабилизации на висении
automatic indicating feathering system — автоматическая система флюгирования с индикацией отказа (двигателя)
automatic mixture-ratio control system — система автоматического регулирования состава (топливной) смеси
automatic pitch control system — автомат тангажа; автоматическая система продольного управления [управления по каналу тангажа]
B.L.C. high-lift system — система управления пограничным слоем для повышения подъёмной силы (крыла)
backpack life support system — ксм. ранцевая система жизнеобеспечения
beam-rider (control, guidance) system — ркт. система наведения по лучу
biowaste electric propulsion system — электрический двигатель, работающий на биологических отходах
buddy (refueling, tank) system — (подвесная) автономная система дозаправки топливом в полете
closed(-circuit, -cycle) system — замкнутая система, система с замкнутым контуром или циклом; система с обратной связью
Cooper-Harper pilot rating system — система баллов оценки ЛА лётчиком по Куперу — Харперу
deployable aerodynamic deceleration system — развёртываемая (в атмосфере) аэродинамическая тормозная система
depressurize the fuel system — стравливать избыточное давление (воздуха, газа) в топливной системе
driver gas heating system — аэрд. система подогрева толкающего газа
dry sump (lubrication) system — дв. система смазки с сухим картером [отстойником]
electrically powered hydraulic system — электронасосная гидросистема (в отличие от гидросистемы с насосами, приводимыми от двигателя)
exponential control flare system — система выравнивания с экспоненциальным управлением (перед приземлением)
flywheel attitude control system — ксм. инерционная система ориентации
gas-ejection attitude control system — ксм. газоструйная система ориентация
gas-jet attitude control system — ксм. газоструйная система ориентация
ground proximity extraction system — система извлечения грузов из самолёта, пролетающего на уровне земли
hot-air balloon water recovery system — система спасения путем посадки на воду с помощью баллонов, наполняемых горячими газами
hypersonic air data entry system — система для оценки аэродинамики тела, входящего в атмосферу планеты с гиперзвуковой скоростью
igh-temperature fatigue test system — установка для испытаний на выносливость при высоких температурах
interceptor (directing, vectoring) system — система наведения перехватчиков
ion electrical propulsion system — ксм. ионная двигательная установка
isotope-heated catalytic oxidizer system — система каталитического окислителя с нагревом от изотопного источника
jet vane actuation system — ркт. система привода газового руля
laminar flow pumping system — система насосов [компрессоров] для ламинаризации обтекания
launching range safety system — система безопасности ракетного полигона; система обеспечения безопасности космодрома
leading edge slat system — система выдвижных [отклоняемых] предкрылков
low-altitude parachute extraction system — система беспосадочного десантирования грузов с малых высот с использованием вытяжных парашютов
magnetic attitude control system — ксм. магнитная система ориентации
magnetically slaved compass system — курсовая система с магнитной коррекцией, гироиндукционная курсовая система
mass-expulsion attitude control system — система ориентации за счёт истечения массы (газа, жидкости)
mass-motion attitude control system — ксм. система ориентации за счёт перемещения масс
mass-shifting attitude control system — ксм. система ориентации за счёт перемещения масс
monopropellant rocket propulsion system — двигательная установка с ЖРД на унитарном [однокомпонентном] топливе
nucleonic propellant gauging and utilization system — система измерения и регулирования подачи топлива с использованием радиоактивных изотопов
open(-circuit, -cycle) system — открытая [незамкнутая] система, система с незамкнутым контуром или циклом; система без обратной связи
plenum chamber burning system — дв. система сжигания топлива во втором контуре
positioning system for the landing gear — система регулирования высоты шасси (при стоянке самолёта на земле)
radar altimeter low-altitude control system — система управления на малых высотах с использованием радиовысотомера
radar system for unmanned cooperative rendezvous in space — радиолокационная система для обеспечения встречи (на орбите) беспилотных кооперируемых КЛА
range and orbit determination system — система определения дальностей [расстояний] и орбит
real-time telemetry processing system — система обработки радиотелеметрических данных в реальном масштабе времени
recuperative cycle regenerable carbon dioxide removal system — система удаления углекислого газа с регенерацией поглотителя, работающая по рекуперативному циклу
rendezvous beacon and command system — маячно-командная система обеспечения встречи («а орбите)
satellite automatic terminal rendezvous and coupling system — автоматическая система сближения и стыковки спутников на орбите
Schuler tuned inertial navigation system — система инерциальной навигации на принципе маятника Шулера
sodium superoxide carbon dioxide removal system — система удаления углекислого газа с помощью надперекиси натрия
space shuttle separation system — система разделения ступеней челночного воздушно-космического аппарата
stellar-monitored astroinertial navigation guidance system — астроинерциальная система навигации и управления с астрокоррекцией
terminal control landing system — система управления посадкой по траектории, связанной с выбранной точкой приземления
terminal descent control system — ксм. система управления на конечном этапе спуска [снижения]
terminal guidance system for a satellite rendezvous — система управления на конечном участке траектории встречи спутников
test cell flow system — ркт. система питания (двигателя) топливом в огневом боксе
vectored thrust (propulsion) system — силовая установка с подъёмно-маршевым двигателем [двигателями]
water to oxygen system — ксм. система добывания кислорода из воды
wind tunnel data acquisition system — система регистрации (и обработки) данных при испытаниях в аэродинамической трубе
— D system -
22 Herbert, Edward Geisler
[br]b. 23 March 1869 Dedham, near Colchester, Essex, Englandd. 9 February 1938 West Didsbury, Manchester, England[br]English engineer, inventor of the Rapidor saw and the Pendulum Hardness Tester, and pioneer of cutting tool research.[br]Edward Geisler Herbert was educated at Nottingham High School in 1876–87, and at University College, London, in 1887–90, graduating with a BSc in Physics in 1889 and remaining for a further year to take an engineering course. He began his career as a premium apprentice at the Nottingham works of Messrs James Hill \& Co, manufacturers of lace machinery. In 1892 he became a partner with Charles Richardson in the firm of Richardson \& Herbert, electrical engineers in Manchester, and when this partnership was dissolved in 1895 he carried on the business in his own name and began to produce machine tools. He remained as Managing Director of this firm, reconstituted in 1902 as a limited liability company styled Edward G.Herbert Ltd, until his retirement in 1928. He was joined by Charles Fletcher (1868–1930), who as joint Managing Director contributed greatly to the commercial success of the firm, which specialized in the manufacture of small machine tools and testing machinery.Around 1900 Herbert had discovered that hacksaw machines cut very much quicker when only a few teeth are in operation, and in 1902 he patented a machine which utilized this concept by automatically changing the angle of incidence of the blade as cutting proceeded. These saws were commercially successful, but by 1912, when his original patents were approaching expiry, Herbert and Fletcher began to develop improved methods of applying the rapid-saw concept. From this work the well-known Rapidor and Manchester saws emerged soon after the First World War. A file-testing machine invented by Herbert before the war made an autographic record of the life and performance of the file and brought him into close contact with the file and tool steel manufacturers of Sheffield. A tool-steel testing machine, working like a lathe, was introduced when high-speed steel had just come into general use, and Herbert became a prominent member of the Cutting Tools Research Committee of the Institution of Mechanical Engineers in 1919, carrying out many investigations for that body and compiling four of its Reports published between 1927 and 1933. He was the first to conceive the idea of the "tool-work" thermocouple which allowed cutting tool temperatures to be accurately measured. For this advance he was awarded the Thomas Hawksley Gold Medal of the Institution in 1926.His best-known invention was the Pendulum Hardness Tester, introduced in 1923. This used a spherical indentor, which was rolled over, rather than being pushed into, the surface being examined, by a small, heavy, inverted pendulum. The period of oscillation of this pendulum provided a sensitive measurement of the specimen's hardness. Following this work Herbert introduced his "Cloudburst" surface hardening process, in which hardened steel engineering components were bombarded by steel balls moving at random in all directions at very high velocities like gaseous molecules. This treatment superhardened the surface of the components, improved their resistance to abrasion, and revealed any surface defects. After bombardment the hardness of the superficially hardened layers increased slowly and spontaneously by a room-temperature ageing process. After his retirement in 1928 Herbert devoted himself to a detailed study of the influence of intense magnetic fields on the hardening of steels.Herbert was a member of several learned societies, including the Manchester Association of Engineers, the Institute of Metals, the American Society of Mechanical Engineers and the Institution of Mechanical Engineers. He retained a seat on the Board of his company from his retirement until the end of his life.[br]Principal Honours and DistinctionsManchester Association of Engineers Butterworth Gold Medal 1923. Institution of Mechanical Engineers Thomas Hawksley Gold Medal 1926.BibliographyE.G.Herbert obtained several British and American patents and was the author of many papers, which are listed in T.M.Herbert (ed.), 1939, "The inventions of Edward Geisler Herbert: an autobiographical note", Proceedings of the Institution of Mechanical Engineers 141: 59–67.ASD / RTSBiographical history of technology > Herbert, Edward Geisler
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