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GB126437A - Improvements in or ralating to Frame-members for Aeroplanes. - Google Patents

Improvements in or ralating to Frame-members for Aeroplanes.

Info

Publication number
GB126437A
GB126437A GB742918A GB742918A GB126437A GB 126437 A GB126437 A GB 126437A GB 742918 A GB742918 A GB 742918A GB 742918 A GB742918 A GB 742918A GB 126437 A GB126437 A GB 126437A
Authority
GB
United Kingdom
Prior art keywords
frame
ralating
aeroplanes
members
pivoted
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
GB742918A
Inventor
Christian Hamilton Gray
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 GB742918A priority Critical patent/GB126437A/en
Publication of GB126437A publication Critical patent/GB126437A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

126,437. Gray, C. H. May 3, 1918. Framework.-A frame member of streamline or similar section and of inflexible material for use on aircraft, is pivoted at its ends so that it always keeps parallel to the line of draught, or a fairing of inflexible material may be pivoted about the frame member for the same purpose. Fig. 4 shows a streamline fairing pivotally secured to a tubular strut by loops L. The device may be of metal or ebonite, &c.
GB742918A 1918-05-03 1918-05-03 Improvements in or ralating to Frame-members for Aeroplanes. Expired GB126437A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB742918A GB126437A (en) 1918-05-03 1918-05-03 Improvements in or ralating to Frame-members for Aeroplanes.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB742918A GB126437A (en) 1918-05-03 1918-05-03 Improvements in or ralating to Frame-members for Aeroplanes.

Publications (1)

Publication Number Publication Date
GB126437A true GB126437A (en) 1919-05-05

Family

ID=32670498

Family Applications (1)

Application Number Title Priority Date Filing Date
GB742918A Expired GB126437A (en) 1918-05-03 1918-05-03 Improvements in or ralating to Frame-members for Aeroplanes.

Country Status (1)

Country Link
GB (1) GB126437A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2693241A (en) * 1946-01-16 1954-11-02 Charles W Ranson Low drag rotor blade for helicopters
US2949090A (en) * 1955-02-18 1960-08-16 Charles F Gerber Weather-vane streamline fairing

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2693241A (en) * 1946-01-16 1954-11-02 Charles W Ranson Low drag rotor blade for helicopters
US2949090A (en) * 1955-02-18 1960-08-16 Charles F Gerber Weather-vane streamline fairing

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