DE331772C - Airplane in which the tail surface is adjusted simultaneously with the adjustment of the angle of incidence of the wings - Google Patents
Airplane in which the tail surface is adjusted simultaneously with the adjustment of the angle of incidence of the wingsInfo
- Publication number
- DE331772C DE331772C DENDAT331772D DE331772DD DE331772C DE 331772 C DE331772 C DE 331772C DE NDAT331772 D DENDAT331772 D DE NDAT331772D DE 331772D D DE331772D D DE 331772DD DE 331772 C DE331772 C DE 331772C
- Authority
- DE
- Germany
- Prior art keywords
- wings
- incidence
- angle
- adjustment
- airplane
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/385—Variable incidence wings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
Description
Flugzeug, bei welchem gleichzeitig mit dem Verstellen des Einfallwinkels der Tragflächen die Schwanzfläche verstellt wird. Die Erfindung betrifft ein Flugzeug, bei welchem gleichzeitig mit dem Verstellen des Einfallwinkels der Tragflächen die Schwanzfläche verstellt wird. Von den bekannten Flugzeugen dieser Art unterscheidet sich _ der Erfindungsgegenstand dadurch, daß bei dem Verringern des Einfallwinkels die Tragflächen nach vorn und die Schwanzflächen nach oben verstellt werden. Durch diese Verstellung soll ein günstiger Gleitflug unter Beibehaltung der horizontalen Lage des Flugzeuges herbeigeführt werden.Airplane, in which simultaneously with the adjustment of the angle of incidence of the wings the tail surface is adjusted. The invention relates to an aircraft in which simultaneously with the adjustment of the angle of incidence of the wings the Tail surface is adjusted. It differs from the known aircraft of this type _ the subject matter of the invention in that when reducing the angle of incidence the wings are moved forward and the tail surfaces up. By this adjustment is intended to achieve a more favorable gliding flight while maintaining the horizontal Position of the aircraft.
Auf der Zeichnung ist eine beispielsweise Ausführungsform des Erfindungsgegenstandes dargestellt. Fig. z zeigt eine Seitenansicht des Flugzeuges mit angehobenem Schwanzsteuer und nach vorn verstellten Tragflächen, Fig. 2 eine Seitenansicht des Flugzeuges mit -in der normalen Fluglage befindlichen Tragflächen und Schwanzsteuer. Bei beiden Figuren ist die rechts liegende Tragfläche nicht mitgezeichnet. Fig. 3 zeigt eine Draufsicht, und Fig. q. eine Vorderansicht des Flugzeuges. Die Tragflächen a sind an einem Tragflächengestell l3 angeordnet, das im Flugzeugkörper c um die Achse d drehbar gelagert ist. Durch mechanische Einrichtungen, wie Hebel, Rollen, Seile, ist eine derartige Verbindung zwischen den Tragflächen und dem Schwanzsteuer hergestellt, daß bei Verstellung der Tragflächen in eine weniger geneigte Lage, wobei die Tragflächen zugleich nach vorn bewegt werden, das Schwanzsteuer gehoben wird.The drawing shows an example of an embodiment of the subject matter of the invention shown. Fig. Z shows a side view of the aircraft with the tail control raised and wings displaced forwards, FIG. 2 is a side view of the aircraft with wings and tail control in normal flight position. By both Figures, the wing on the right is not drawn. Fig. 3 shows a Plan view, and Fig. Q. a front view of the aircraft. The wings are a arranged on a wing frame l3, which is in the aircraft body c around the axis d is rotatably mounted. Mechanical devices such as levers, rollers, ropes, such a connection is established between the wings and the tail rudder, that when adjusting the wings in a less inclined position, the wings be moved forward at the same time, the tail rudder is raised.
Beim Zurückführen der Tragflächen in die frühere Lage wird das Schwanzsteuer ebenfalls wieder in seine normale Lage zurückgeführt. Die Propeller l sind unterhalb der Tragflächen am Tragflächengestell gelagert.When the wings are returned to their previous position, the tail rudder becomes also returned to its normal position. The propellers l are below of the wings stored on the wing frame.
Claims (1)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE331772T |
Publications (1)
Publication Number | Publication Date |
---|---|
DE331772C true DE331772C (en) | 1921-01-12 |
Family
ID=6199060
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DENDAT331772D Expired DE331772C (en) | Airplane in which the tail surface is adjusted simultaneously with the adjustment of the angle of incidence of the wings |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE331772C (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2510959A (en) * | 1942-04-16 | 1950-06-13 | Willard R Custer | Airplane with high-lift channeled wings |
-
0
- DE DENDAT331772D patent/DE331772C/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2510959A (en) * | 1942-04-16 | 1950-06-13 | Willard R Custer | Airplane with high-lift channeled wings |
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