CH139061A - Plane. - Google Patents
Plane.Info
- Publication number
- CH139061A CH139061A CH139061DA CH139061A CH 139061 A CH139061 A CH 139061A CH 139061D A CH139061D A CH 139061DA CH 139061 A CH139061 A CH 139061A
- Authority
- CH
- Switzerland
- Prior art keywords
- aircraft
- plane
- wings
- view
- flight
- Prior art date
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
Description
Flugzeug. Die vorliegende Erfindung hat ein Flug zeug zum Gegenstand, welches zwei Trägflächen aufweist, deren Längsachsen parallel zur Flugrichtung angeordnet sind, wodurch das Flugzeug im Verhältnis zum heutigen Typ bedeutend länger, und die Spannweite der Tragflächen verkürzt wird.
Diese Anordnung der Trägflächen erzielt besondere Vorteile, indem das Flugzeug be liebig gross gebaut werden kann; auch lässt sich die Erfindung an einem Flugzeugtyp anwenden, der in der Breitendimension ver hältnismässig wenig Raum beansprucht, wel che ihm die Eigenschaft gibt, auf Strassen zu starten und zu landen.
In beiliegender Zeichnung ist der Gegen stand der Erfindung in einem Ausführungs beispiel dargestellt und zeigt: Fig. 1 einen Doppeldecker in Seitenansicht, Fig. 2 in Vorderansicht, Fig. 3 in Draufsicht.
Die Längsachsen der Tragflächen 1 und 3 verlaufen zur Flugrichtung parallel statt quer wie bei den heutigen Flugzeugen.
An der Tragfläche 1 sind die Verwin dungsklappen 2 angebracht, welche von der Tragfläche seitlich vorstehen um beim Ab fangen der Böen grössere Wirkungskraft zu erlangen.
Die Verwindungsklappen 2 können bei grösseren Flugzeugen auch noch an den un tern Tragflächen 3 angebracht sein.
Plane. The present invention has an aircraft as an object which has two support surfaces, the longitudinal axes of which are arranged parallel to the direction of flight, whereby the aircraft is significantly longer compared to today's type, and the span of the wings is shortened.
This arrangement of the support surfaces achieves particular advantages in that the aircraft can be built as large as desired; The invention can also be applied to a type of aircraft that takes up relatively little space in terms of width, which gives it the property of taking off and landing on streets.
In the accompanying drawing, the subject matter of the invention is shown in an embodiment example and shows: Fig. 1 a double decker in side view, Fig. 2 in front view, Fig. 3 in plan view.
The longitudinal axes of the wings 1 and 3 run parallel to the direction of flight instead of transversely as in today's aircraft.
On the wing 1, the twisting flaps 2 are attached, which protrude laterally from the wing in order to achieve greater effectiveness when catching the gusts.
The torsion flaps 2 can also be attached to the un tern wings 3 in larger aircraft.
Claims (1)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH139061T | 1929-09-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CH139061A true CH139061A (en) | 1930-03-31 |
Family
ID=4396357
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CH139061D CH139061A (en) | 1929-09-20 | 1929-09-20 | Plane. |
Country Status (1)
| Country | Link |
|---|---|
| CH (1) | CH139061A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1104741A1 (en) * | 1999-12-01 | 2001-06-06 | Manuel Munoz Saiz | Aircraft lift arrangement |
| ES2245147A1 (en) * | 2002-09-12 | 2005-12-16 | Manuel Muñoz Saiz | Lifting arrangement for aircraft fuselage |
| WO2015187259A1 (en) * | 2014-05-08 | 2015-12-10 | Thomas Mcnally | Convertible payload transport aircraft |
-
1929
- 1929-09-20 CH CH139061D patent/CH139061A/en unknown
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1104741A1 (en) * | 1999-12-01 | 2001-06-06 | Manuel Munoz Saiz | Aircraft lift arrangement |
| ES2174690A1 (en) * | 1999-12-01 | 2002-11-01 | Saiz Manuel Munoz | Aircraft lift arrangement |
| ES2245147A1 (en) * | 2002-09-12 | 2005-12-16 | Manuel Muñoz Saiz | Lifting arrangement for aircraft fuselage |
| WO2015187259A1 (en) * | 2014-05-08 | 2015-12-10 | Thomas Mcnally | Convertible payload transport aircraft |
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