DE375857C - Fuselage - Google Patents

Fuselage

Info

Publication number
DE375857C
DE375857C DEF48966D DEF0048966D DE375857C DE 375857 C DE375857 C DE 375857C DE F48966 D DEF48966 D DE F48966D DE F0048966 D DEF0048966 D DE F0048966D DE 375857 C DE375857 C DE 375857C
Authority
DE
Germany
Prior art keywords
engine
fuselage
driver
seat
central axis
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
Application number
DEF48966D
Other languages
German (de)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
A H G FOKKER
Original Assignee
A H G FOKKER
Publication date
Priority to DEF48966D priority Critical patent/DE375857C/en
Application granted granted Critical
Publication of DE375857C publication Critical patent/DE375857C/en
Expired legal-status Critical Current

Links

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
    • B64D27/08—Aircraft characterised by the type or position of power plants of piston type within, or attached to, fuselages

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Harvester Elements (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)

Description

Der Gegenstand der Erfindung betrifft eine Anordnung des Motors und des Führersitzes im Flugzeug. Es ist üblich, den Motor in die Mittelachse des Flugzeuges zu legen und den Führerplatz hinter dem Motor anzuordnen. The object of the invention relates to an arrangement of the engine and the driver's seat on the plane. It is common to place the engine in the center axis of the aircraft and to arrange the driver's seat behind the engine.

Durch die Erfindung ist es möglich, unter günstiger und vorteilhafter Ausnutzung des im Flugzeugrumpf zur Verfügung stehenden Raumes dem Führer den zur Bedienung des Motors vorteilhaftesten Platz zu schaffen, indem man den Motor nicht in der Mittelachse, sondern etwas seitlich von dieser Achse anordnet. Diese Anordnung ist auch bei mehreren hintereinander geschalteten Motoren ohne Schwierigkeit möglich und gestattet so die beste Raumausnutzung und Unterbringung des Führers im Flugzeugrumpf. Hierdurch ist man imstande, dem Führer links oder rechts neben dem Motor seinen Platz zu geben. Bei zwei oder mehr Motoren erhält ein Führer links und ein Führer rechts seinen Platz.The invention makes it possible, with favorable and advantageous utilization of the in the aircraft fuselage available to the driver to operate the To create the most advantageous space for the motor by not placing the motor in the central axis, but something to the side of this axis. This arrangement also applies to several motors connected in series possible without difficulty and thus allows the best use of space and accommodation of the leader in the fuselage. This enables the driver to take his place on the left or right of the engine give. If there are two or more engines, one leader on the left and one leader on the right receives his Place.

Die Zeichnung zeigt eine beispielsweise schematisch dargestellte Ausführung.The drawing shows an embodiment shown schematically, for example.

α ist der Flugzeugrumpf, b der Führersitz, c der Motor, d die Mittelachse des Flugzeuges.α is the fuselage, b the driver's seat, c the engine, d the central axis of the aircraft.

Claims (1)

Patent-Anspruch:Patent claim: Flugzeugrumpf, dadurch gekennzeichnet, daß der Motor etwas seitlich von der Mittelachse und der Führersitz neben dem Motor angeordnet ist.Aircraft fuselage, characterized in that the engine is somewhat to the side of the Central axis and the driver's seat is arranged next to the engine. Hierzu ι Blatt Zeichnungen.For this purpose ι sheet of drawings. . gedruckt ta heu reiChsuruckerel. printed ta heu rauchuruckerel
DEF48966D Fuselage Expired DE375857C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEF48966D DE375857C (en) Fuselage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEF48966D DE375857C (en) Fuselage

Publications (1)

Publication Number Publication Date
DE375857C true DE375857C (en) 1923-05-19

Family

ID=7102613

Family Applications (1)

Application Number Title Priority Date Filing Date
DEF48966D Expired DE375857C (en) Fuselage

Country Status (1)

Country Link
DE (1) DE375857C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040113785A1 (en) * 1998-09-11 2004-06-17 Key-Trak, Inc. Object carriers for an object control and tracking system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040113785A1 (en) * 1998-09-11 2004-06-17 Key-Trak, Inc. Object carriers for an object control and tracking system

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