DE953937C - Airplane with an annular jack screw - Google Patents
Airplane with an annular jack screwInfo
- Publication number
- DE953937C DE953937C DEB34428A DEB0034428A DE953937C DE 953937 C DE953937 C DE 953937C DE B34428 A DEB34428 A DE B34428A DE B0034428 A DEB0034428 A DE B0034428A DE 953937 C DE953937 C DE 953937C
- Authority
- DE
- Germany
- Prior art keywords
- airplane
- jack screw
- annular jack
- annular
- air duct
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/001—Flying saucers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Description
Die bekannten Hubschrauber erreichen eine Geschwindigkeit von etwa 120 km/Std. Höhere Geschwindigkeiten können nur durch den Einbau von besonderen Motoren, die dem Vortrieb dienen, erreicht werden. Diesen Nachteil. beseitigt die Erfindung. Hat das Flugzeug die erforderliche Flughöhe erreicht, so wird die ringförmige Hubschraube oben und bzw. oder unten durch je eine einen Luftleitkanal bildende Haube mit vorn bzw. hinten liegender düsenförmiger Öffnung abgedeckt. Dadurch entsteht vor der vorn liegenden Düse ein Unterdruck bzw. durch die hinten liegende Düse ein Vorschub. Infolgedessen bewegt sich der Hubschrauber mit einer wesentlich größeren Geschwindigkeit vorwärts, als er ohne die erfindungsgemäße Einrichtung erreichen würde.The known helicopters reach a speed of about 120 km / h Higher speeds can only be achieved by installing special Engines that are used for propulsion can be achieved. This disadvantage. eliminates the Invention. When the aircraft has reached the required altitude, it becomes ring-shaped Lifting screw above and / or below through one each forming an air duct Hood covered with a nozzle-shaped opening at the front or rear. This creates A negative pressure is applied in front of the nozzle in front or through the nozzle in the back Feed. As a result, the helicopter moves at a much larger rate Forward speed than he would achieve without the inventive device would.
Abb. 1 zeigt eine Seitenansicht mit aufgelegtem ringförmigem. Luftleitkanal, Abb. 2 eine Vorderansicht mit geöffnetem geteiltem ringförmigem Luftleitkanal, Abb.3 eine Ansicht von oben mit aufgelegtem ringförmigem Luftleitkanal.Fig. 1 shows a side view with the ring-shaped. Air duct, Fig. 2 is a front view with the split ring-shaped air duct open, Fig.3 a view from above with an applied annular air duct.
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEB34428A DE953937C (en) | 1955-02-09 | 1955-02-09 | Airplane with an annular jack screw |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEB34428A DE953937C (en) | 1955-02-09 | 1955-02-09 | Airplane with an annular jack screw |
Publications (1)
Publication Number | Publication Date |
---|---|
DE953937C true DE953937C (en) | 1956-12-06 |
Family
ID=6964313
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DEB34428A Expired DE953937C (en) | 1955-02-09 | 1955-02-09 | Airplane with an annular jack screw |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE953937C (en) |
-
1955
- 1955-02-09 DE DEB34428A patent/DE953937C/en not_active Expired
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