{"id":2080,"date":"2024-01-01T01:00:00","date_gmt":"2024-01-01T01:00:00","guid":{"rendered":"http:\/\/wp.polot.net\/2024\/07\/13\/aircraft-engines-geared-turbofan-part-23\/"},"modified":"2024-07-13T18:40:28","modified_gmt":"2024-07-13T16:40:28","slug":"aircraft-engines-geared-turbofan-part-23","status":"publish","type":"post","link":"https:\/\/polot.net\/?p=2080&lang=en","title":{"rendered":"Aircraft Engines &#8211; Geared Turbofan &#8211; Part 23"},"content":{"rendered":"<h2 id=\"Engins-geared-turbofan\"  >Engins geared turbofan<\/h2>\n<p><figure class=\"alignleft\">                    <img decoding=\"async\" data-src=\"https:\/\/images.polot.net\/14ba501b0f8bcdfb8d4c5adc4c412eb2df695f68\" src=\"https:\/\/images.polot.net\/14ba501b0f8bcdfb8d4c5adc4c412eb2df695f68\" alt=\"Pratt &amp; Whitney PW1500G. 2014 year. Photo by Karol Placha Hetman\" class=\"lazyload\" data-action=\"zoom\"><figcaption>Pratt &amp; Whitney PW1500G. 2014 year. Photo by Karol Placha Hetman<\/figcaption><\/figure>\n<p><figure class=\"alignleft\">                    <img decoding=\"async\" data-src=\"https:\/\/images.polot.net\/fda3a1490fa6c3bf7a43966354bf855a5fe7e522\" src=\"https:\/\/images.polot.net\/fda3a1490fa6c3bf7a43966354bf855a5fe7e522\" alt=\"Pratt &amp; Whitney PW1500G. 2014 year. Photo by Karol Placha Hetman\" class=\"lazyload\" data-action=\"zoom\"><figcaption>Pratt &amp; Whitney PW1500G. 2014 year. Photo by Karol Placha Hetman<\/figcaption><\/figure>\n<h3 id=\"Pratt-&amp;-Whitney.\"  >Pratt &amp; Whitney.<\/h3>\n<p>Work on turbo-fan engines with a gearbox resumed at the turn of the century. There were several reasons for this decision. First; Such an engine, despite the use of a transmission, has a lower mass in terms of mass-thrust ratio. Secondly; has lower fuel consumption. Thirdly; emits fewer harmful chemicals into the atmosphere. Fourthly; emits less noise. Such an engine is perfectly suited for thrust in the range of 50.00 kN &#8211; 100.00 kN.<\/p>\n<p>Since 2000, the Pratt &amp; Whitney company has been testing turbo-fan-gear engines intended for the propulsion of commercial aircraft of the Purepower 1000G series. In 2008, the engine underwent rigorous testing and experimentation. The engines have been offered by Pratt &amp; Whitney since 2014. According to the company, these engines are suitable for approximately 40% of existing commercial aircraft. Replacing turbo-fan engines with turbo-fan-gear motors reduces the weight of the aircraft by about 10%. Turbo-fan-gear motors reduce fuel consumption by about 16%, reduce NOX emissions by 50%, reduce noise by 75%. All this together reduces the cost of operating a single plane by at least $ 1.5 million per year.<\/p>\n<p>A variation of the PW1100 engines, as opposed to the engines that power business-jets, is such that the new engines are designed for commercial aircraft that take 180 passengers on board. In 2010, Pratt &amp; Whitney announced that it had an order for more than 200 PW1100 engines. Among other things, the engine was dedicated to the Airbus A320NEO.<\/p>\n<p>The PW1000 engine has a cold to hot flow ratio of 12: 1. By comparison, the CFM56 engine has this ratio of 5.5: 1 and its development version LEAP has this ratio of 9: 1 or 11: 1. The transmission was built by Pratt &amp; Whitney in the late 80&#8217;s. It has an efficiency of 99% and is able to deliver a capacity of 25 MW.<\/p>\n<p>The PW1000G engines are dedicated to the following aircraft: Airbus A320NEO (PW1100G), Irkut MC-21 (PW1400G), Bombardier Cseries (PW1500G), Embraer E-Jet E2 family (PW1700G, PW1900G), Mitsubishi Regional Jet (PW1200G), Suchoj Super Jet 130 ( PW1600G).<\/p>\n<p>Written by Karol Placha Hetman<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Work on turbo-fan engines with a gearbox resumed at the turn of the century. There were several reasons for this decision. First; Such an engine, despite the use of a transmission, has a lower mass in terms of mass-thrust ratio. Secondly; has lower fuel consumption. Thirdly; emits fewer harmful chemicals into the atmosphere. Fourthly; emits less noise. Such an engine is perfectly suited for thrust in the range of 50.00 kN &#8211; 100.00 kN.<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"closed","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[17],"tags":[],"class_list":["post-2080","post","type-post","status-publish","format-standard","hentry","category-articles"],"_links":{"self":[{"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts\/2080","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/users\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Fcomments&post=2080"}],"version-history":[{"count":1,"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts\/2080\/revisions"}],"predecessor-version":[{"id":2299,"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts\/2080\/revisions\/2299"}],"wp:attachment":[{"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Fmedia&parent=2080"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Fcategories&post=2080"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Ftags&post=2080"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}