GB220383A - Improvements in metal framework for aircraft - Google Patents

Improvements in metal framework for aircraft

Info

Publication number
GB220383A
GB220383A GB13170/23A GB1317023A GB220383A GB 220383 A GB220383 A GB 220383A GB 13170/23 A GB13170/23 A GB 13170/23A GB 1317023 A GB1317023 A GB 1317023A GB 220383 A GB220383 A GB 220383A
Authority
GB
United Kingdom
Prior art keywords
strips
aircraft
sides
spars
channel strips
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
GB13170/23A
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
Priority to GB13170/23A priority Critical patent/GB220383A/en
Publication of GB220383A publication Critical patent/GB220383A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064—Stringers; Longerons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/065—Spars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Abstract

220,383. Mooney, D. J. May 17, 1923. Framework.-Metal spars, girders &c. of box form for aircraft are constructed with corrugated flanged strips b to which are riveted channel strips c, with sides and base longitudinally bent, the two composite booms thus formed being joined together by webs e shaped at their edges to fit the sides or bases of the channel strips. Deep spars are formed by attaching additional channel strips g, Fig. 7, to the strips c so as to form a cellular structure. Other forms are described only in the shape and number of the corrugations.
GB13170/23A 1923-05-17 1923-05-17 Improvements in metal framework for aircraft Expired GB220383A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB13170/23A GB220383A (en) 1923-05-17 1923-05-17 Improvements in metal framework for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB13170/23A GB220383A (en) 1923-05-17 1923-05-17 Improvements in metal framework for aircraft

Publications (1)

Publication Number Publication Date
GB220383A true GB220383A (en) 1924-08-18

Family

ID=10018132

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13170/23A Expired GB220383A (en) 1923-05-17 1923-05-17 Improvements in metal framework for aircraft

Country Status (1)

Country Link
GB (1) GB220383A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112839868A (en) * 2018-10-10 2021-05-25 想像航空有限公司 Aircraft spars with integrated power units and associated systems and methods

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112839868A (en) * 2018-10-10 2021-05-25 想像航空有限公司 Aircraft spars with integrated power units and associated systems and methods
KR20210071039A (en) * 2018-10-10 2021-06-15 이매진 에어로 인코포레이티드 Aircraft wing beams with integrated power cells and related systems and methods
EP3863922A4 (en) * 2018-10-10 2022-06-15 Imagine Aero Inc. Aircraft spars with integrated power cells, and associated systems and methods
US11434014B2 (en) 2018-10-10 2022-09-06 Imagine Aero Inc. Aircraft spars with integrated power cells, and associated systems and methods
KR102581305B1 (en) * 2018-10-10 2023-09-22 이매진 에어로 인코포레이티드 Aircraft wing beams with integrated power cells and related systems and methods

Similar Documents

Publication Publication Date Title
GB125748A (en) Improvements in Construction of Metal Spars and Longerons for Aircraft.
GB220383A (en) Improvements in metal framework for aircraft
GB161063A (en) Improvements in metal construction of spars, longerons and the like for aircraft
GB128322A (en) Improvements in Metal Construction for Aircraft.
GB157312A (en) Improvement in airplane spars
GB202761A (en) Improvements in or relating to spars for aircraft
GB180074A (en) Improvements in metal framework for aircraft
GB211606A (en) Improvements in the construction of structural members for aircraft
GB128663A (en) Improvements in Metal Construction for Aircraft.
GB218074A (en) Improvements in or relating to metal spars and the like for aircraft
GB131080A (en) Improvements in the Construction of Metal Spars for Aircraft.
GB162108A (en) Improvements in or relating to the construction of metal spars longerons and the like for aircraft
GB685618A (en) Improvements in or relating to studs for buildings structures
GB225307A (en) Improvements in the construction of metal framework members for aircraft
GB223670A (en) Improvements in or relating to metal spars and the like for aviation
GB194114A (en) Improvements in or relating to metal spars and the like for aviation
GB247313A (en) Improvements in the construction of aircraft members
GB121006A (en) Improvements in Metal Spars for Aircraft.
GB214847A (en) Improvements in or relating to the construction of spars for aircraft
GB128262A (en) Improvements in Girders and similar Structures for Aircraft and other purposes.
GB465246A (en) Improvements relating to metal aeroplane bodies
GB136638A (en) Improvements in or relating to the Construction of Spars for Aircraft.
GB224298A (en) Improvements in metal girders of light construction for aircraft and the like
GB157311A (en) Improvement in spar beams or ribs for airplanes
GB261492A (en) Improvements in the construction of spars, longerons and the like for aircraft