{"id":2063,"date":"2024-01-01T01:00:00","date_gmt":"2024-01-01T01:00:00","guid":{"rendered":"http:\/\/wp.polot.net\/2024\/07\/13\/aero-engines-inline-and-supercharging-engines-part-6\/"},"modified":"2024-07-13T18:40:29","modified_gmt":"2024-07-13T16:40:29","slug":"aero-engines-inline-and-supercharging-engines-part-6","status":"publish","type":"post","link":"https:\/\/polot.net\/?p=2063&lang=en","title":{"rendered":"Aero engines &#8211; Inline and supercharging engines &#8211; Part 6"},"content":{"rendered":"<h2 id=\"Internal-combustion-piston-engine.\"  >Internal combustion-piston engine.<\/h2>\n<p><figure class=\"alignleft\">                    <img decoding=\"async\" data-src=\"https:\/\/images.polot.net\/525c7cebd4c5f5412d006f6996d0fc9d56006dfb\" src=\"https:\/\/images.polot.net\/525c7cebd4c5f5412d006f6996d0fc9d56006dfb\" alt=\"M-34 from 1933 year. 2017 year. Photo by Karol Placha Hetman\" class=\"lazyload\" data-action=\"zoom\"><figcaption>M-34 from 1933 year. 2017 year. Photo by Karol Placha Hetman<\/figcaption><\/figure>\n<p>Description for the picture: M-34 engine by CCCP, 1933, V-type, 12-cylinder, maximum power 850 HP at 1,800 rpm, capacity 45.8 liters, compression ratio 6.0: 1, engine weight 582 kg. The disadvantage of the engine is its heavy weight, so it was only suitable for propelling large aircraft. The M-34 engines powered, among others, Tupolev TB-3 bombers.<\/p>\n<p><figure class=\"alignleft\">                    <img decoding=\"async\" data-src=\"https:\/\/images.polot.net\/2b50827df46b6c1ea7d7a7b7a64b47aedff0388f\" src=\"https:\/\/images.polot.net\/2b50827df46b6c1ea7d7a7b7a64b47aedff0388f\" alt=\"PZL Pegaz XX. 2011 year. Photo by Karol Placha Hetman\" class=\"lazyload\" data-action=\"zoom\"><figcaption>PZL Pegaz XX. 2011 year. Photo by Karol Placha Hetman<\/figcaption><\/figure>\n<p>Description to the photo: De Havilland Hamilton Standard adjustable, two-stage, three-blade propeller. PZL Pegaz XX engine from 1937, 9-cylinder, left-hand rotation, maximum power 940 HP, capacity 28.6 liters, compression ratio 6.5: 1, engine weight 456 kg, diameter 1.40 m. The engine has a compressor air, reducer and carburetor. Cloudel-Hobson AVT 8OBZ carburetor by Motolux.<\/p>\n<p>Written by Karol Placha Hetman<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Description for the picture: M-34 engine by CCCP, 1933, V-type, 12-cylinder, maximum power 850 HP at 1,800 rpm, capacity 45.8 liters, compression ratio 6.0: 1, engine weight 582 kg. The disadvantage of the engine is its heavy weight, so it was only suitable for propelling large aircraft. The M-34 engines powered, among others, Tupolev TB-3 bombers.<\/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-2063","post","type-post","status-publish","format-standard","hentry","category-articles"],"_links":{"self":[{"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts\/2063","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=2063"}],"version-history":[{"count":1,"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts\/2063\/revisions"}],"predecessor-version":[{"id":2307,"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts\/2063\/revisions\/2307"}],"wp:attachment":[{"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Fmedia&parent=2063"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Fcategories&post=2063"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Ftags&post=2063"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}