DE602975C - Glider - Google Patents

Glider

Info

Publication number
DE602975C
DE602975C DEN34837D DEN0034837D DE602975C DE 602975 C DE602975 C DE 602975C DE N34837 D DEN34837 D DE N34837D DE N0034837 D DEN0034837 D DE N0034837D DE 602975 C DE602975 C DE 602975C
Authority
DE
Germany
Prior art keywords
glider
aircraft
tow
tow rope
fuselage
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
DEN34837D
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.)
Individual
Original Assignee
Individual
Publication date
Priority to DEN34837D priority Critical patent/DE602975C/en
Application granted granted Critical
Publication of DE602975C publication Critical patent/DE602975C/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C31/00Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
    • B64C31/02Gliders, e.g. sailplanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Curtains And Furnishings For Windows Or Doors (AREA)
  • Toys (AREA)

Description

Hierzu 1 Blatt Zeichnungen1 sheet of drawings

GEDHDOkT IN DER REIÖHSDRÜfikfiÜfeiGEDHDOkT IN THE REIÖHSDRÜfikfiÜfei

Claims (1)

Patentanspruch :Claim: Segelflugzeug mit Einrichtungen für den Schleppstart, dadurch gekennzeichnet, daß der Angriffspunkt für das Schleppseil unterhalb des Auftriebsmittelpunktes liegt und daß im Rumpf ein an sich bekanntes Laufgewicht vorgesehen ist, dessen Bewegung derart begrenzt ist, daß es in seiner hinteren Stellung das Flugzeug während des Schleppens in der Drachenlage hält und in seiner vorderen Stellung das Flugzeug nach dem Lösen des Schleppseiles in Gleitlage bringt.Glider with devices for the tow start, characterized in that the point of application for the tow rope is below the center of lift and that a known running weight is provided in the fuselage, the movement of which is so limited that in its rearward position it holds the aircraft in the kite position during towing and in its forward position the aircraft after releasing the tow rope brings into sliding position.
DEN34837D Glider Expired DE602975C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEN34837D DE602975C (en) Glider

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEN34837D DE602975C (en) Glider

Publications (1)

Publication Number Publication Date
DE602975C true DE602975C (en) 1934-09-20

Family

ID=7346863

Family Applications (1)

Application Number Title Priority Date Filing Date
DEN34837D Expired DE602975C (en) Glider

Country Status (1)

Country Link
DE (1) DE602975C (en)

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