GB119251A - Improvements in and relating to the Construction of the Framework of Aeroplanes. - Google Patents

Improvements in and relating to the Construction of the Framework of Aeroplanes.

Info

Publication number
GB119251A
GB119251A GB10099/17A GB1009917A GB119251A GB 119251 A GB119251 A GB 119251A GB 10099/17 A GB10099/17 A GB 10099/17A GB 1009917 A GB1009917 A GB 1009917A GB 119251 A GB119251 A GB 119251A
Authority
GB
United Kingdom
Prior art keywords
framework
aeroplanes
relating
construction
bulges
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
GB10099/17A
Inventor
Cecil Sandys Walker
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 GB10099/17A priority Critical patent/GB119251A/en
Publication of GB119251A publication Critical patent/GB119251A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/04—Aircraft characterised by the type or position of power plants of piston type

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

119,251. Walker, C. S. July 12, 1917. Framework.-Sheetmetal frame members for use in aircraft are provided with bulged, fluted, or corrugated portions) to strengthen them. Fig. 7 shows the front plate of an aeroplane body having a hole 3 for the passage of the engine shaft. The plate has bulges 4 arranged as shown and is flanged at the edges. Holes may be formed in the bulges for lightness. Where flutings or corrugations are formed they do not extend to the edges of the plates.
GB10099/17A 1917-07-12 1917-07-12 Improvements in and relating to the Construction of the Framework of Aeroplanes. Expired GB119251A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB10099/17A GB119251A (en) 1917-07-12 1917-07-12 Improvements in and relating to the Construction of the Framework of Aeroplanes.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB10099/17A GB119251A (en) 1917-07-12 1917-07-12 Improvements in and relating to the Construction of the Framework of Aeroplanes.

Publications (1)

Publication Number Publication Date
GB119251A true GB119251A (en) 1918-09-12

Family

ID=32408347

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10099/17A Expired GB119251A (en) 1917-07-12 1917-07-12 Improvements in and relating to the Construction of the Framework of Aeroplanes.

Country Status (1)

Country Link
GB (1) GB119251A (en)

Similar Documents

Publication Publication Date Title
GB1120381A (en) Improvements in or relating to the manufacture of aerodynamic structures
GB119251A (en) Improvements in and relating to the Construction of the Framework of Aeroplanes.
GB511650A (en) Improvements relating to arrangements for sucking off the boundary layer from aerofoils
GB132153A (en) Improvements in Metal construction for Aeronautical Machines
GB131065A (en) Improvements in or relating to Spars and like Structural Units for Aircraft.
GB123629A (en) Improvements in and in connection with Internal-combustion Engines for use on Aircraft.
GB229389A (en) Improvements in metal construction for aeronautical machines
GB521881A (en) Improvements in or relating to the construction of aeroplanes
USD137610S (en) Design for an airplane
GB121465A (en) An Improved Metal Fitting for Assembling Longitudinals and Uprights in Aeroplanes.
GB123902A (en) Improvements in the Construction of Aeroplane Spars, Struts, Longerons, Bearers, and the like.
GB734532A (en) Improvements relating to aircraft
GB565235A (en) Improvements in or relating to aircraft wings or the like
GB191206149A (en) Improvements in and relating to Chain and like Driving Arrangements, particularly applicable for Aeroplanes.
GB128651A (en) Improvements in Connection with the Fuselages of Aeronautical Machines.
GB126068A (en) A Hollow Section Aerial Propeller.
GB125019A (en) Improved Means of Securing Fittings to the Spars of Aircraft.
GB191213608A (en) Improvements in Propellers for Aeroplanes.
GB107208A (en) Improvements in or relating to Aeroplanes and other Aerial Machines having Supporting Planes or Wings.
GB121463A (en) Improved Device for Fixing an Engine in an Aeroplane.
GB122710A (en) Improvements in or relating to Means to Receive Strut-ends in Aeroplanes and other Structures.
GB230017A (en) Improvements in or relating to power generating attachments for airplanes
GB561062A (en) Aerofoil construction
GB208701A (en) Improvements in or relating to the construction of aircraft, especially aeroplanes
GB556109A (en) Resilient mountings