GB392447A - Single spar aircraft wing with auxiliary spars - Google Patents

Single spar aircraft wing with auxiliary spars

Info

Publication number
GB392447A
GB392447A GB30598/32A GB3059832A GB392447A GB 392447 A GB392447 A GB 392447A GB 30598/32 A GB30598/32 A GB 30598/32A GB 3059832 A GB3059832 A GB 3059832A GB 392447 A GB392447 A GB 392447A
Authority
GB
United Kingdom
Prior art keywords
spar
auxiliary
members
aircraft wing
ribs
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
GB30598/32A
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.)
Dornier Metallbauten GmbH
Original Assignee
Dornier Metallbauten GmbH
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 Dornier Metallbauten GmbH filed Critical Dornier Metallbauten GmbH
Publication of GB392447A publication Critical patent/GB392447A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/185—Spars

Abstract

392,447. Aircraft wing structures. DORNIER METALLBAUTEN GES. and DORNIER, C., Friedrichshafen, Lake Constance, Germany. Oct. 31, 1932, No. 30598. Convention date, Dec. 8, 1931. [Class 4.] An aircraft wing having a single main spar a and main ribs b spaced apart at comparatively large distances from one another is provided with auxiliary wing spars c disposed between the ribs b and articulated thereto, one beam of each auxiliary spar being connected at each end to the top and bottom beams of the corresponding section of the spar a by diagonally arranged tension members d, e or diagonally arranged tension or compression members. One end of spar c may be connected to spar a by a compression member or members and the other by a tension member or members. Auxiliary ribs f are yieldingly and/or resiliently connected to the main and auxiliary spars.
GB30598/32A 1931-12-08 1932-10-31 Single spar aircraft wing with auxiliary spars Expired GB392447A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE392447X 1931-12-08

Publications (1)

Publication Number Publication Date
GB392447A true GB392447A (en) 1933-05-18

Family

ID=6385718

Family Applications (1)

Application Number Title Priority Date Filing Date
GB30598/32A Expired GB392447A (en) 1931-12-08 1932-10-31 Single spar aircraft wing with auxiliary spars

Country Status (1)

Country Link
GB (1) GB392447A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2588822A1 (en) * 1985-10-22 1987-04-24 Courthieu Sa Georges Wing for light aircraft
RU2466061C2 (en) * 2010-01-11 2012-11-10 Николай Иванович Максимов Flight vehicle (versions), flight vehicles parts, method of exploiting flight vehicle and its parts

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2588822A1 (en) * 1985-10-22 1987-04-24 Courthieu Sa Georges Wing for light aircraft
RU2466061C2 (en) * 2010-01-11 2012-11-10 Николай Иванович Максимов Flight vehicle (versions), flight vehicles parts, method of exploiting flight vehicle and its parts

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