DE584750C - Vertical tail unit for single or multi-engine aircraft - Google Patents

Vertical tail unit for single or multi-engine aircraft

Info

Publication number
DE584750C
DE584750C DEG80907D DEG0080907D DE584750C DE 584750 C DE584750 C DE 584750C DE G80907 D DEG80907 D DE G80907D DE G0080907 D DEG0080907 D DE G0080907D DE 584750 C DE584750 C DE 584750C
Authority
DE
Germany
Prior art keywords
engine aircraft
vertical tail
tail unit
engine
propeller
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
DEG80907D
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.)
KARL GRULICH DR ING
Original Assignee
KARL GRULICH DR ING
Publication date
Priority to DEG80907D priority Critical patent/DE584750C/en
Application granted granted Critical
Publication of DE584750C publication Critical patent/DE584750C/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Description

Hierzu 1 Blatt Zeichnungen1 sheet of drawings

Claims (1)

Patentanspruch :Claim: Seitenleitwerk für ein- oder mehrmotorige Flugzeuge nach Patent 565 020, dadurch gekennzeichnet, daß die als Kielflosse (α) ausgebildete Verkleidung des Triebwerkes in ihrer Höhenausdehnung den Durchmesser der Luftschraube (c) übersteigt und mit diese umfassenden Armen versehen ist, die als Lager für ein hinter der Luftschraube angeordnetes Seitenruder (b) dienen.Vertical stabilizer for single or multi-engine aircraft according to patent 565 020, characterized in that the casing of the engine, designed as a keel fin (α), exceeds the diameter of the propeller (c) in its height and is provided with arms encompassing this, which act as bearings for a rudder (b) located behind the propeller are used.
DEG80907D Vertical tail unit for single or multi-engine aircraft Expired DE584750C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEG80907D DE584750C (en) Vertical tail unit for single or multi-engine aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEG80907D DE584750C (en) Vertical tail unit for single or multi-engine aircraft

Publications (1)

Publication Number Publication Date
DE584750C true DE584750C (en) 1933-09-23

Family

ID=7137206

Family Applications (1)

Application Number Title Priority Date Filing Date
DEG80907D Expired DE584750C (en) Vertical tail unit for single or multi-engine aircraft

Country Status (1)

Country Link
DE (1) DE584750C (en)

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