DE360880C - Machinery for aircraft - Google Patents
Machinery for aircraftInfo
- Publication number
- DE360880C DE360880C DEZ11304D DEZ0011304D DE360880C DE 360880 C DE360880 C DE 360880C DE Z11304 D DEZ11304 D DE Z11304D DE Z0011304 D DEZ0011304 D DE Z0011304D DE 360880 C DE360880 C DE 360880C
- Authority
- DE
- Germany
- Prior art keywords
- aircraft
- fuselage
- exhaust gases
- engines
- machinery
- 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
- 239000007789 gas Substances 0.000 claims description 13
- 238000010438 heat treatment Methods 0.000 description 5
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000009434 installation 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)
- Exhaust Silencers (AREA)
Description
Maschinenanlage für Luftfahrzeuge. Die Erfindung befaßt sich mit der Kraftanlage von Luftfahrzeugen und versucht diese wirtschaftlicher zu gestalten. Sie löst dies dadurch, daß eine an sich bekannte Abgasturbine zum Antrieb einer Luftschraube verwendet wird und die Abgasturbine im Gegensatz zu den Kolbenverbrennungsmotoren, die beiderseits des Mittelrumpfes auf oder zwischen den Tragdecks untergebracht sind, im Mittelrumpf eingebaut ist.Machine system for aircraft. The invention is concerned with Kraftanlage of aircraft and tries to make them more economical. It solves this in that a known exhaust gas turbine to drive a Propeller is used and the exhaust gas turbine in contrast to the piston internal combustion engines, housed on both sides of the central hull on or between the supporting decks is installed in the central hull.
Die Erfindung nutzt so die in den Abgasen der Motoren .enthaltene Energie zum Vortrieb des Luftfahrzeuges aus, wogegen aus den bisher üblichen Kraftanlagen der Luftfahrzeuge die Abgase meist unbenutzt entweichen.The invention thus uses that contained in the exhaust gases of the engines Energy to propel the aircraft from, whereas from the previously common power plants of the aircraft, the exhaust gases mostly escape unused.
Zugleich ermöglicht die Anordnung den Einbau einer Kraftmaschine im Mittelrumpf, ohne daß die in diesem befindlichen Mitfahrer durch Geräusch und Erschütterungen belästigt werden, wie dies beim Einbau von Kolbenkraftmaschinen im Mittelrumpf eintritt. Des weiteren bilden die Abgase der Turbine ein geeigneteres Heizmittel für den Aufenthaltsraum, als wenn, wie es bekannt ist, die Abgase von Kolbenmotoren zur Heizung benutzt werden, da sie die Turbine mit einer Temperatur verlassen, die für Heizzwecke besser geeignet ist. Auch durchströmen diese Gase die Heizeinrichtung nicht stoßweise, wie hei direktem Anschluß an Kolbenkrafttnaschinen, bei denen das Auspuffgeräusch in den mit den Abgasen geheizten Raum übertragen wird. , In der Zeichnung ist ein Beispiel Barg ° stellt.At the same time, the arrangement enables the installation of a prime mover in the Central fuselage without the passengers located in this being caused by noise and vibrations be annoyed, as occurs when installing piston engines in the central fuselage. Furthermore, the exhaust gases from the turbine form a more suitable heating medium for the living room, as if, as is known, the exhaust gases from piston engines are used for heating, as they leave the turbine at a temperature that is more suitable for heating purposes is. These gases also do not flow through the heating device intermittently, as is the case with direct Connection to piston engines, where the exhaust noise in the with the Exhaust gases heated room is transferred. , In the drawing is an example of Barg ° represents.
hie Abbildung zeigt in Aufsicht schematisch ein Zweimotorenflugzeug mit einer Kraftanlage, die der Erfindung gemäß angeordnet ist. Seitlich vom Rumpf i ist auf dem Flügel 2 links und rechts je ein Kolbenverbrennungsmotor 3 angeordnet, der eine Zug= schraube 4 treibt. Die Auspuffgase werden von den Motoren 3 durch je eine Leitung 5 zur Turbine 6 geleitet, die eine Schraube 7 antreibt.The figure shows a schematic top view of a twin-engine aircraft with a power plant which is arranged according to the invention. To the side of the fuselage i a piston internal combustion engine 3 is arranged on the left and right of the wing 2, which drives a tension screw 4. The exhaust gases are from the engines 3 through One line 5 each is routed to the turbine 6, which drives a screw 7.
Die Abgase der Turbine werden entweder unmittelbar in die das Luftfahrzeug umgebende Luft oder durch ein Heizrohr 8, das beispielsweise im Passagierraum 9 verlegt ist, in die freie Außenluft geführt.The exhaust gases from the turbine are either directly fed into the aircraft surrounding air or through a heating pipe 8, which, for example, in the passenger compartment 9 is laid, led into the open outside air.
Die Erfindung eignet sich sowohl für die Kraftanlagen von Flugzeugen wie für Luftschiffe.The invention is suitable both for the power plants of aircraft as for airships.
Die Zahl der Motoren bzw. Abgasturbinen ist an sich beliebig, sofern sie grundsätzlich der Anordnung der Erfindung entspricht.The number of engines or exhaust gas turbines is arbitrary, provided that it basically corresponds to the arrangement of the invention.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DEZ11304D DE360880C (en) | Machinery for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DEZ11304D DE360880C (en) | Machinery for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE360880C true DE360880C (en) | 1922-10-07 |
Family
ID=7621789
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DEZ11304D Expired DE360880C (en) | Machinery for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| DE (1) | DE360880C (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2465099A (en) * | 1943-11-20 | 1949-03-22 | Allis Chalmers Mfg Co | Propulsion means comprising an internal-combustion engine and a propulsive jet |
-
0
- DE DEZ11304D patent/DE360880C/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2465099A (en) * | 1943-11-20 | 1949-03-22 | Allis Chalmers Mfg Co | Propulsion means comprising an internal-combustion engine and a propulsive jet |
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