DE458314C - Engine system for aircraft - Google Patents
Engine system for aircraftInfo
- Publication number
- DE458314C DE458314C DES65136D DES0065136D DE458314C DE 458314 C DE458314 C DE 458314C DE S65136 D DES65136 D DE S65136D DE S0065136 D DES0065136 D DE S0065136D DE 458314 C DE458314 C DE 458314C
- Authority
- DE
- Germany
- Prior art keywords
- housing
- engine
- wing
- tank
- propeller
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 239000000446 fuel Substances 0.000 claims description 4
- 238000001816 cooling Methods 0.000 claims 2
- 239000002828 fuel tank Substances 0.000 claims 2
- 238000010276 construction Methods 0.000 claims 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/04—Aircraft characterised by the type or position of power plants of piston type
- B64D27/06—Aircraft characterised by the type or position of power plants of piston type within, or attached to, wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Description
Für Flugzeuge ist es bekannt, zur Erleichterung des Transports die Rumpfspitze samt dem Motor abnehmbar zu machen, und es sind auch auswechselbare Motoraggregate bekannt, bei denen der Motor mit seinem Zubehör zu einem geschlossen für sich handhabungsfähigen Ganzen vereinigt ist. Andererseits hat man auch Motoren unmittelbar in die Tragflügel eingebaut.For aircraft, it is known to have the fuselage tip together to facilitate transport to make the engine removable, and interchangeable engine units are also known, in which the motor and its accessories become a closed and manageable one Whole is united. On the other hand, you also have motors directly in the wings built-in.
ίο Die Erfindung besteht darin, daß der Motor nebst Zubehör in einem Gehäuse zusammengebaut ist, das als .Ganzes auf ein Tragflächenprofil aufsetzbar ist. Hierdurch ergibt sich die Möglichkeit, derartige Motoraggre-ίο The invention consists in that the engine is assembled together with accessories in a housing, which as a whole on a wing profile is attachable. This results in the possibility of such engine assemblies
IS gate leicht an vorhandenen Flugzeugen anzubringen, insbesondere auch an Segelflugzeugen und sonstigen Kleinflugzeugen, indem gerade die Anpassung an ein Tragflächenprofil wegen der weitgehenden Ähnlichkeit sämtlicher solcher Profile in allen Fällen einen einfachen und sicheren Anbau ermöglicht, uild indem bei solchem Anbau auch der mit dem Motor unmittelbar verbundene Propeller in solche Höhenlage kommt, daß er selbst bei sehr niedrigem Fahrgestell vor Bodenberührung gesichert arbeiten kann. Zugleich kommt dabei der Schwerpunkt der Motoranlage in nächste Nähe des Auftriebsmittels, so daß Stabilitätsstörungen vorgebeugt wird. Es ergibt sich so also eine Motoranlage, die leicht an verschiedenartigen Flugzeugen verwendet werden kann und so eine Anpassung der Flugzeuge an verschiedene Betriebsbedingungen ermöglicht, vermöge derer auch wissenschaftliche Untersuchungen in besonders ergiebiger und einfacher Weise durchgeführt werden können.IS gate easily attached to existing aircraft, in particular also on gliders and other small aircraft by just adapting to a wing profile because of the extensive similarity of all such profiles, one in all cases allows simple and safe cultivation, uild by with such an attachment also with the Motor directly connected propeller comes to such an altitude that he himself at very low chassis secured against ground contact. At the same time comes the center of gravity of the engine system in close proximity to the buoyancy device, so that Stability disorders are prevented. The result is an engine system that is lightweight can be used on various types of aircraft and so an adaptation of the Aircraft at different operating conditions made possible, by virtue of which also scientific investigations in particular can be carried out more productively and simply.
Eine wertvolle Einzelheit ergibt sich, indem bei Ausführung des Motors als üblicher Verbrennungsmotor der Vergaser in dem Zwischenraum zwischen Motor oder Tank und den Gehäuseunterkanten vorgesehen ist. Hierdurch kann trotz der aerodynamisch günstigen niedrigen Bauart der ganzen Anlage der Brennstoff unter natürlichem Gefalle zum Vergaser fließen, und es sind alle Verwickelungen und Betriebsunsicherheiten in dieser Hinsicht verhütet.A valuable detail arises by making the engine more common Internal combustion engine, the carburetor is provided in the space between the engine or tank and the lower edges of the housing. As a result, despite the aerodynamically favorable low design of the entire system the fuel flow naturally to the carburetor, and there are all tangles and operational uncertainties in this regard prevented.
Wertvoll ist weiter unter Benutzung eines Zugpropellers die Anbringung des Tanks im hinteren Gehäuseteil und des Motors nebst Stirnkühler im vorderen Gehäuseteil, so daß der Propeller, unmittelbar auf der Motorwelle sitzend, dicht vor der Profilnase läuft. Hier sind Zwischengetriebe erspart, und es ergibt sich für den Propeller eine sehr zuverlässige Lagerung, indem der ihn tragende Motor gerade auf dem widerstandsfähigsten Teile der Tragfläche abgestützt ist.It is also valuable to attach the tank in the using a pull propeller rear housing part and the motor together with front cooler in the front housing part, so that the propeller, sitting directly on the motor shaft, runs close to the profile nose. here intermediate gears are saved, and the propeller is very reliable Storage by placing the engine supporting it straight on the toughest parts the wing is supported.
Eine wertvolle Einzelausgestaltung besteht endlich in Bändern oder Seilen, mittels derer das Gehäuse an Knotenpunkten der Tragfläche festgebolzt werden kann. Diese Befestigungsart ergibt bei einwandfreier ZuverlässigkeitA valuable individual design finally consists of ribbons or ropes, by means of which the housing can be bolted to nodes on the wing. This type of attachment results with impeccable reliability
Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DES65136D DE458314C (en) | 1924-02-20 | 1924-02-20 | Engine system for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DES65136D DE458314C (en) | 1924-02-20 | 1924-02-20 | Engine system for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
DE458314C true DE458314C (en) | 1928-04-03 |
Family
ID=7497789
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DES65136D Expired DE458314C (en) | 1924-02-20 | 1924-02-20 | Engine system for aircraft |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE458314C (en) |
-
1924
- 1924-02-20 DE DES65136D patent/DE458314C/en not_active Expired
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