DE2558992A1 - Large fixed wing aircraft - has several normal size wings in series to minimise span - Google Patents

Large fixed wing aircraft - has several normal size wings in series to minimise span

Info

Publication number
DE2558992A1
DE2558992A1 DE19752558992 DE2558992A DE2558992A1 DE 2558992 A1 DE2558992 A1 DE 2558992A1 DE 19752558992 DE19752558992 DE 19752558992 DE 2558992 A DE2558992 A DE 2558992A DE 2558992 A1 DE2558992 A1 DE 2558992A1
Authority
DE
Germany
Prior art keywords
wing
minimise
span
series
wing aircraft
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.)
Pending
Application number
DE19752558992
Other languages
German (de)
Inventor
Rolf Woerner
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
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 Individual filed Critical Individual
Priority to DE19752558992 priority Critical patent/DE2558992A1/en
Publication of DE2558992A1 publication Critical patent/DE2558992A1/en
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/08—Aircraft not otherwise provided for having multiple wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)

Abstract

The multiple wing arrangement for outsize fixed-wing aircraft consists of several wing units of conventional design and size mounted one behind the other in place of a single wing. This removes the limit currently placed on aircraft size/weight by the limitations of wing dimensions. The arrangement is not restrictive in terms of the characteristics of the wing design used, but wind tunnel tests must be carried out to establish optimum relative positions, angles and distances apart.

Description

Multitraqflüqel für Großflugzeuge Multitraq wing for large aircraft

1. Die Erfindung betrifft einen Tragflügel mit dessen Hilfe man Flugzeuge von fast unbegrenzter Größe bauen kann.1. The invention relates to a wing with the help of which one aircraft of almost unlimited size.

2. Wenn man Großflugzeuge immer größer baut, sc kommt man an eine Grenze, wo man die Flugzeuge nicht mehr größer bauen kann, weil die Tragflächen nicht mehr länger gemacht werden können. Es ist doch so, daß man Tragflächen nicht 100 Meter und noch länger machen kann. Um diese Grenze zu überwinden, habe ich den Multitragflügel gemacht.2. If you build big airplanes bigger and bigger, you get one Limit where the aircraft can no longer be built bigger because the wings can no longer be made. The fact is that you don't have wings Can do 100 meters and even longer. To overcome this limit, I have that Multi-hydrofoil made.

3. Die Erfindung hat die Aufgabe, die Grenzen im Großflugzeugbau zu überwinden.3. The invention has the task of pushing the boundaries in large aircraft construction overcome.

4. Der Multitragflügel besteht aus mehreren Tragflügeln, die hintereinander angeordnet sind. Zwischen den einzelnen Tragflügeln ist ein Abstand A vorhanden, siehe Zeichnung.4. The multi-hydrofoil consists of several hydrofoils, one behind the other are arranged. There is a distance A between the individual wings, see diagram.

5. Die Anzahl der Tragflügel kann beiiebig groß gewählt werden.5. The number of wings can be chosen to be arbitrarily large.

6. Die Konstruktion ist an keine besondere Flügelform gebunden.6. The construction is not tied to any particular wing shape.

Die genaue Anordnung, Stellung und der Abstand zwischen den einzelnen Tragflügeln muß im Windkanal ermittelt werden. The exact arrangement, position and the distance between each Airfoils must be determined in the wind tunnel.

Claims (1)

½) Patentanspruch: a) Multitragflügel bei dem die Tragflügel hintereinander angeordnet sind.½) Claim: a) Multi-hydrofoil in which the hydrofoils one behind the other are arranged. b) Nach Absatz a) mit beliebig großer Anzahl von hintereinander angeordneten Tragflügeln.b) According to paragraph a) with any number of consecutively arranged Hydrofoils.
DE19752558992 1975-12-29 1975-12-29 Large fixed wing aircraft - has several normal size wings in series to minimise span Pending DE2558992A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19752558992 DE2558992A1 (en) 1975-12-29 1975-12-29 Large fixed wing aircraft - has several normal size wings in series to minimise span

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19752558992 DE2558992A1 (en) 1975-12-29 1975-12-29 Large fixed wing aircraft - has several normal size wings in series to minimise span

Publications (1)

Publication Number Publication Date
DE2558992A1 true DE2558992A1 (en) 1977-07-07

Family

ID=5965820

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19752558992 Pending DE2558992A1 (en) 1975-12-29 1975-12-29 Large fixed wing aircraft - has several normal size wings in series to minimise span

Country Status (1)

Country Link
DE (1) DE2558992A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1984001926A1 (en) * 1982-11-15 1984-05-24 Erich Jakob Heincke Transport airplane provided with a plurality of bearing surfaces separated from each other by a distance larger than a width of a bearing surface and provided with braking spoilers as an additional vertical stabilizer
DE3411425A1 (en) * 1984-03-28 1984-12-20 Albrecht G. Prof. Dr. 4600 Dortmund Fischer Foldable, variable high-lift slotted wing for hang-gliders and ultra-light aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1984001926A1 (en) * 1982-11-15 1984-05-24 Erich Jakob Heincke Transport airplane provided with a plurality of bearing surfaces separated from each other by a distance larger than a width of a bearing surface and provided with braking spoilers as an additional vertical stabilizer
DE3411425A1 (en) * 1984-03-28 1984-12-20 Albrecht G. Prof. Dr. 4600 Dortmund Fischer Foldable, variable high-lift slotted wing for hang-gliders and ultra-light aircraft

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