| dbo:abstract |
Der Hirth HM 515 war ein für die allgemeine Luftfahrt bestimmter Kolbenflugmotor des deutschen Herstellers Hirth. (de) The Hirth HM 515 was a four-cylinder air-cooled inverted inline engine, intended to power light aircraft of the 1940s. Due to World War II, demand for the light aircraft to be powered by the HM 515 dried up and only the Siebel Si 202C Hummel was powered by development engines before further work was abandoned. The HM 515 closely followed the Hirth formula of Elektron (magnesium alloy) castings for the crank case and covers, with roller bearings and metered oil feeds for light weight, smooth running and low oil consumption. Only a small number were produced before the war precluded further production of the light aircraft class that the engine was intended to power. Flight testing was carried out in the Si 202Cs driving a 1.8 m (5 ft 11 in) propeller, but no production ensued. (en) |
| dbo:wikiPageID |
63021864 (xsd:integer) |
| dbo:wikiPageLength |
4174 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID |
1110216061 (xsd:integer) |
| dbo:wikiPageWikiLink |
dbr:Elektron_(alloy) dbr:Light_aircraft dbc:Hirth_aircraft_engines dbc:Inverted_aircraft_piston_engines dbc:Air-cooled_aircraft_piston_engines dbr:Hirth dbr:Hirth_HM_500 dbc:1930s_aircraft_piston_engines dbr:Reciprocating_engine dbr:World_War_II dbr:Inline_engine_(aviation) dbr:80_Octane dbr:Siebel_Si_202C_Hummel |
| dbp:compression |
6.200000 (xsd:double) |
| dbp:coolingsystem |
air-cooled (en) |
| dbp:developedFrom |
dbr:Hirth_HM_500 |
| dbp:fuelsystem |
1 (xsd:integer) |
| dbp:fueltype |
80 (xsd:integer) |
| dbp:majorApplications |
dbr:Siebel_Si_202C_Hummel |
| dbp:manufacturer |
dbr:Hirth |
| dbp:nationalOrigin |
Germany (en) |
| dbp:oilcon |
at max continuous (en) |
| dbp:oilsystem |
dry sump, pressure feed with scavenge (en) |
| dbp:power |
:* at 2,100 rpm for take-off :* at 2,040 rpm at sea level :* at 1,990 rpm at sea level (en) |
| dbp:power/weight |
*B.M.E.P.: (en) |
| dbp:ref |
Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944 (en) |
| dbp:specfuelcon |
at max continuous (en) |
| dbp:type |
4 (xsd:integer) dbr:Reciprocating_engine dbr:Inline_engine_(aviation) |
| dbp:valvetrain |
1 (xsd:integer) |
| dbp:weight |
dry, unequipped :::: wet, equipped (en) |
| dbp:wikiPageUsesTemplate |
dbt:Cite_book dbt:Cvt dbt:Reflist dbt:Short_description dbt:Hirth_aeroengines dbt:Infobox_Aircraft_Engine dbt:Pistonspecs |
| dcterms:subject |
dbc:Hirth_aircraft_engines dbc:Inverted_aircraft_piston_engines dbc:Air-cooled_aircraft_piston_engines dbc:1930s_aircraft_piston_engines |
| rdfs:comment |
Der Hirth HM 515 war ein für die allgemeine Luftfahrt bestimmter Kolbenflugmotor des deutschen Herstellers Hirth. (de) The Hirth HM 515 was a four-cylinder air-cooled inverted inline engine, intended to power light aircraft of the 1940s. Due to World War II, demand for the light aircraft to be powered by the HM 515 dried up and only the Siebel Si 202C Hummel was powered by development engines before further work was abandoned. (en) |
| rdfs:label |
Hirth HM 515 (de) Hirth HM 515 (en) |
| owl:sameAs |
wikidata:Hirth HM 515 dbpedia-de:Hirth HM 515 https://global.dbpedia.org/id/bduT |
| prov:wasDerivedFrom |
wikipedia-en:Hirth_HM_515?oldid=1110216061&ns=0 |
| foaf:isPrimaryTopicOf |
wikipedia-en:Hirth_HM_515 |
| is dbo:wikiPageWikiLink of |
dbr:List_of_aircraft_engines dbr:Siebel_Si_202_Hummel dbr:Hirth dbr:Volksflugzeug |
| is foaf:primaryTopic of |
wikipedia-en:Hirth_HM_515 |