DE649150C - Airplane swing wing - Google Patents

Airplane swing wing

Info

Publication number
DE649150C
DE649150C DEH137022D DEH0137022D DE649150C DE 649150 C DE649150 C DE 649150C DE H137022 D DEH137022 D DE H137022D DE H0137022 D DEH0137022 D DE H0137022D DE 649150 C DE649150 C DE 649150C
Authority
DE
Germany
Prior art keywords
tendons
swing wing
airplane
swing
axis
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
DEH137022D
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.)
HANS WEIRICH
Original Assignee
HANS WEIRICH
Publication date
Priority to DEH137022D priority Critical patent/DE649150C/en
Application granted granted Critical
Publication of DE649150C publication Critical patent/DE649150C/en
Expired legal-status Critical Current

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)
  • Toys (AREA)

Description

Hierzu ι Blatt ZeichnungenFor this purpose ι sheet of drawings

EiiLiX. GEMTtTCKT JN IiKR !IF.tCHSDlU CKKUKIEiiLiX. GEMTtTCKT JN IiKR! IF.tCHSDlU CKKUKI

Claims (3)

Patentansprüche:Patent claims: 1. Flugzeugschwingflügel, um eine vor dem Druckmittelpunkt gelegene Achse drehbar, deren Anstellwinkel sich an den augenblicklichen Strömungszustand mittels sich bei Abwärtsbewegung spannender, bei Aufwärtsbewegung entspannender Glieder (Federn) anpaßt, nach Patent 610023, dadurch gekennzeichnet, daß die Spannung der Spannglieder mit dem Federweg stärker als verhältnisgleich zunimmt.1. Aircraft swing wing, about an axis located in front of the center of pressure rotatable, the angle of which is adapted to the current flow condition by means of adapts itself to the downward movement of tensioning limbs (springs) when moving upward to relax, according to patent 610023, characterized in that the tension of the tendons increases more than proportionally with the spring travel. 2. Schwingflügel nach Anspruch 1, gekennzeichnet durch eine Vereinigung mehrerer Spannglieder zu einer Spanneinheit in solcher Anordnung, daß sie nacheinander in Wirkung treten.2. Swing paddle according to claim 1, characterized by combining several tendons into one tensioning unit in such an arrangement that they take effect one after the other. 3. Schwingflügel nach Anspruch 1 und 2, dadurch gekennzeichnet, daß die Spannglieder verschiedene Abstände von der Drehachse haben.3. oscillating paddle according to claim 1 and 2, characterized in that the tendons have different distances from the axis of rotation. *) Von dem Patentsucher ist als der Erfinder angegeben worden:*) The patent seeker stated as the inventor: Dipl.-Ing. Karl Haenle in Berlin-Britz.Dipl.-Ing. Karl Haenle in Berlin-Britz.
DEH137022D Airplane swing wing Expired DE649150C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEH137022D DE649150C (en) Airplane swing wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEH137022D DE649150C (en) Airplane swing wing

Publications (1)

Publication Number Publication Date
DE649150C true DE649150C (en) 1937-12-23

Family

ID=7177662

Family Applications (1)

Application Number Title Priority Date Filing Date
DEH137022D Expired DE649150C (en) Airplane swing wing

Country Status (1)

Country Link
DE (1) DE649150C (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2584667A (en) * 1947-02-14 1952-02-05 George E Bockrath Gust alleviating control means for airplanes
DE1122677B (en) * 1959-01-19 1962-01-25 Gottlob Widmann & Soehne K G Siebschlaeger coffee grinder operated by an electric motor
DE1275872B (en) * 1965-09-14 1968-08-22 Karl Haenle Dipl Ing Flapping wing plane

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2584667A (en) * 1947-02-14 1952-02-05 George E Bockrath Gust alleviating control means for airplanes
DE1122677B (en) * 1959-01-19 1962-01-25 Gottlob Widmann & Soehne K G Siebschlaeger coffee grinder operated by an electric motor
DE1275872B (en) * 1965-09-14 1968-08-22 Karl Haenle Dipl Ing Flapping wing plane

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