AT107348B - Through-flow plate cooler, especially for aircraft decks. - Google Patents

Through-flow plate cooler, especially for aircraft decks.

Info

Publication number
AT107348B
AT107348B AT107348DA AT107348B AT 107348 B AT107348 B AT 107348B AT 107348D A AT107348D A AT 107348DA AT 107348 B AT107348 B AT 107348B
Authority
AT
Austria
Prior art keywords
ribs
cooler
flow plate
aircraft
plate cooler
Prior art date
Application number
Other languages
German (de)
Inventor
Robert Macrez
Original Assignee
Robert Macrez
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 Robert Macrez filed Critical Robert Macrez
Application granted granted Critical
Publication of AT107348B publication Critical patent/AT107348B/en

Links

Landscapes

  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Description

  

   <Desc/Clms Page number 1> 
 



    Durchströmplatten-Kühler,   insbesondere für   Flugzeugtragdecke.   
 EMI1.1 
 deckenden, an den   Kühlerstirnenden   zu Quersammlern für Zu-und Abströmung ausgemuldeten Blechwandung und besteht im Wesen darin, dass in der Deckblechwandung niedere, mit den Mündungen der Durchströmrippen übereinstimmende und in diese etwas hineinragende Versteifungsrippen vorgesehen sind. 



   In der Zeichnung ist ein Ausführungsbeispiel im Schnitt senkrecht zur Länge der   Kühlerrippen   dargestellt. 



   Die Wand, welche die Höhlungen der Rippen a des Rippenbleches T nach unten abdeckt, ist ein Blech T', das mit Rippen n versehen ist, die mit. den Mündungen der Rippen a übereinstimmen und etwas in dieselben hineinragen. Diese Anordnung weist mehrere besondere Vorteile auf. Vor allem erleichtern die Rippen n das richtige Einsetzen des Kühlrippenbleches auf die Wand T'bei der Herstellung des Kühlers und sichern die Aufrechterhaltung der Form der Rippen und ihres gleichen Abstandes voneinander. Weiter verleihen die Rippen n dem Bleche T'selbst eine Steifigkeit, wodurch dieses Blech wesentlich schwächer gehalten werden kann und das Gesamtgewicht des Kühlers herabgesetzt wird. 



  Schliesslich tragen die Rippen n zur Versteifung des ganzen Kühlers bei. 



   Die Form dieser Rippen n von geringer Höhe kann verschieden sein ; sie müssen bloss mit den Mündungen der Rippen a übereinstimmen, können aber auch nur an einem Teile oder nur an bestimmten Teilen der Länge der Rippe a angeordnet oder nur für eine bestimmte Teilzahl der Rippen vorgesehen sein. 

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



   <Desc / Clms Page number 1>
 



    Through-flow plate cooler, especially for aircraft decks.
 EMI1.1
 covering sheet metal wall, hollowed out at the cooler front ends to form transverse collectors for inflow and outflow, and essentially consists in the fact that lower stiffening ribs that coincide with the mouths of the flow ribs and protrude somewhat into them are provided in the cover sheet wall.



   In the drawing, an embodiment is shown in section perpendicular to the length of the radiator fins.



   The wall which covers the cavities of the ribs a of the ribbed plate T downwards is a plate T ', which is provided with ribs n, which are with. the mouths of the ribs a coincide and protrude somewhat into them. This arrangement has several particular advantages. Above all, the ribs n facilitate the correct insertion of the cooling rib sheet on the wall T ′ during the manufacture of the cooler and ensure that the shape of the ribs and their equal spacing from one another are maintained. Furthermore, the ribs n give the sheet metal T's itself a rigidity, as a result of which this sheet can be kept much weaker and the overall weight of the cooler is reduced.



  Finally, the ribs contribute to the stiffening of the entire radiator.



   The shape of these ribs n of small height can be different; they just have to coincide with the mouths of the ribs a, but can also only be arranged on one part or only on certain parts of the length of the rib a or only be provided for a certain number of the ribs.

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

 

Claims (1)

PATENT-ANSPRUCH : Durehströmplatten-Kühler, insbesondere für Flugzeugtragdeeke, bestehend aus einer zu Durchströmplatten-Rippen hochgewellten Blechwandung und einer diese abdeckenden, an den Kühlerstirnenden zu Quersammlern für Zu-und Abströmung ausgemuldeten Blechwandung, dadurch gekennzeichnet, dass in der Deckblechwandung (T') niedere, mit den Mündungen der Durchströmrippen (a) übereinstimmende und in diese etwas hineinragende Versteifungsrippen (n) vorgesehen sind. EMI1.2 **WARNUNG** Ende CLMS Feld Kannt Anfang DESC uberlappen**. PATENT CLAIM: Throughflow plate cooler, in particular for aircraft decking, consisting of a sheet metal wall corrugated up to form flow plate ribs and a sheet metal wall covering this, at the cooler front ends troughed to form transverse collectors for inflow and outflow, characterized in that in the cover sheet wall (T ') lower stiffening ribs (n) that coincide with the mouths of the flow ribs (a) and protrude slightly into them are provided. EMI1.2 ** WARNING ** End of CLMS field may overlap beginning of DESC **.
AT107348D 1925-05-27 1925-05-27 Through-flow plate cooler, especially for aircraft decks. AT107348B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT107348T 1925-05-27

Publications (1)

Publication Number Publication Date
AT107348B true AT107348B (en) 1927-09-26

Family

ID=3624318

Family Applications (1)

Application Number Title Priority Date Filing Date
AT107348D AT107348B (en) 1925-05-27 1925-05-27 Through-flow plate cooler, especially for aircraft decks.

Country Status (1)

Country Link
AT (1) AT107348B (en)

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