GB191108911A - Improvements in or relating to Aeroplanes. - Google Patents

Improvements in or relating to Aeroplanes.

Info

Publication number
GB191108911A
GB191108911A GB191108911DA GB191108911A GB 191108911 A GB191108911 A GB 191108911A GB 191108911D A GB191108911D A GB 191108911DA GB 191108911 A GB191108911 A GB 191108911A
Authority
GB
United Kingdom
Prior art keywords
plane
pivoted
strips
aeroplanes
flaps
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
Inventor
Ludwig Schmidl
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
Application granted granted Critical
Publication of GB191108911A publication Critical patent/GB191108911A/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
    • B64C3/54—Varying in area

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • On-Site Construction Work That Accompanies The Preparation And Application Of Concrete (AREA)
  • Supports For Plants (AREA)
  • Toys (AREA)

Abstract

8911. Schmidl, L. April 9, 1910, [Convention date]. Planes, construction of; steering and balancing.- In aeroplanes having the main planes provided at their extremities with steering- flaps of variable area, these flaps are composed of series of strips pivoted to the main plane and to parallel link-work so that, when drawn in, they overlap each other like scales. Fig. 2 shows a main plane 2 provided with series of strips 1, which are are arranged transversely of the machine and pivoted at 3, 4, 5 to the plane and also to parallel rods 6. In a modification, the strips are disposed longitudinally of the machine, the rods 6 being pivoted to the plane 2.
GB191108911D 1910-04-09 1911-04-10 Improvements in or relating to Aeroplanes. Expired GB191108911A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT49705T 1910-04-09

Publications (1)

Publication Number Publication Date
GB191108911A true GB191108911A (en) 1911-05-25

Family

ID=3570468

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191108911D Expired GB191108911A (en) 1910-04-09 1911-04-10 Improvements in or relating to Aeroplanes.

Country Status (2)

Country Link
AT (1) AT49705B (en)
GB (1) GB191108911A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111959746A (en) * 2020-08-31 2020-11-20 哈尔滨工业大学 Parallel connecting rod type deformation wing framework

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111959746A (en) * 2020-08-31 2020-11-20 哈尔滨工业大学 Parallel connecting rod type deformation wing framework
CN111959746B (en) * 2020-08-31 2022-10-11 哈尔滨工业大学 Parallel connecting rod type deformation wing framework

Also Published As

Publication number Publication date
AT49705B (en) 1911-09-11

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