AT210278B - Helicopter with load cabin - Google Patents

Helicopter with load cabin

Info

Publication number
AT210278B
AT210278B AT357159A AT357159A AT210278B AT 210278 B AT210278 B AT 210278B AT 357159 A AT357159 A AT 357159A AT 357159 A AT357159 A AT 357159A AT 210278 B AT210278 B AT 210278B
Authority
AT
Austria
Prior art keywords
helicopter
load cabin
cabin
load
fuselage
Prior art date
Application number
AT357159A
Other languages
German (de)
Original Assignee
Agusta Aeronaut Costr
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Agusta Aeronaut Costr filed Critical Agusta Aeronaut Costr
Application granted granted Critical
Publication of AT210278B publication Critical patent/AT210278B/en

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  • Passenger Equipment (AREA)
  • Vehicle Step Arrangements And Article Storage (AREA)

Description

  

   <Desc/Clms Page number 1> 
 



  Helikopter mit Lastkabine 
Es ist bekannt, dass Lasten grösserer Länge durch Helikopter mit normaler Kabine nur schwierig zu transportieren sind. 



   Zur Beseitigung dieses Nachteiles wurde ein Helikopter mit Lastkabine entwickelt, bei welchem erfindungsgemäss die Lastkabine unter dem Führersitz breite Frontfenster und hinten eine breite Öffnung aufweist, die mit der Rumpfform angepassten Klappen verschliessbar sind. 



   Fig. 1 und 2 zeigen Seiten- und Stirnansicht dieses Helikopters. 



   Wie aus der Zeichnung ersichtlich ist, weist die Lastkabine des Helikopters unter dem Führersitz in seiner Breite ein Frontfenster 5 und hinten eine breite Öffnung 6 auf, die mit der Rumpfform angepassten Klappen 2,3 verschliessbar sind. Es ist auf diese Weise möglich, lange, am Bug und Heck herausragende Lasten 4 in der Lastkabine 1 zu laden und sie dem Schwerpunkt entsprechend abzusetzen. 

**WARNUNG** Ende DESC Feld kannt Anfang CLMS uberlappen**.



   <Desc / Clms Page number 1>
 



  Helicopter with load cabin
It is known that loads of greater length are difficult to transport by helicopters with a normal cabin.



   To eliminate this disadvantage, a helicopter with a load cabin was developed in which, according to the invention, the load cabin has wide front windows under the driver's seat and a wide opening at the rear, which can be closed with flaps adapted to the shape of the fuselage.



   Figs. 1 and 2 show side and end views of this helicopter.



   As can be seen from the drawing, the load cabin of the helicopter has a front window 5 in its width under the driver's seat and a wide opening 6 at the rear, which can be closed with flaps 2, 3 adapted to the shape of the fuselage. In this way it is possible to load long loads 4 protruding at the bow and stern in the load cabin 1 and to set them down according to the center of gravity.

** WARNING ** End of DESC field may overlap beginning of CLMS **.

Claims (1)

PATENTANSPRUCH : Helikopter mit Lastkabine, dadurch gekennzeichnet, dass die Lastkabine (1) unter dem Fuhrersitz breite Frontfenster (5) und hinten eine breite Öffnung (6) aufweist, die mit der Rumpfform angepassten Klappen (2, 3) verschliessbar sind. **WARNUNG** Ende CLMS Feld Kannt Anfang DESC uberlappen**. PATENT CLAIM: Helicopter with load cabin, characterized in that the load cabin (1) has wide front windows (5) under the driver's seat and a wide opening (6) at the back, which flaps (2, 3) adapted to the shape of the fuselage can be closed. ** WARNING ** End of CLMS field may overlap beginning of DESC **.
AT357159A 1959-03-27 1959-05-13 Helicopter with load cabin AT210278B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT210278X 1959-03-27

Publications (1)

Publication Number Publication Date
AT210278B true AT210278B (en) 1960-07-25

Family

ID=11175600

Family Applications (1)

Application Number Title Priority Date Filing Date
AT357159A AT210278B (en) 1959-03-27 1959-05-13 Helicopter with load cabin

Country Status (1)

Country Link
AT (1) AT210278B (en)

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