GB178912A - Improvements in aircraft - Google Patents

Improvements in aircraft

Info

Publication number
GB178912A
GB178912A GB275921A GB275921A GB178912A GB 178912 A GB178912 A GB 178912A GB 275921 A GB275921 A GB 275921A GB 275921 A GB275921 A GB 275921A GB 178912 A GB178912 A GB 178912A
Authority
GB
United Kingdom
Prior art keywords
rear section
hinged
tail skid
section
aircraft
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
GB275921A
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 GB275921A priority Critical patent/GB178912A/en
Publication of GB178912A publication Critical patent/GB178912A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C35/00—Flying-boats; Seaplanes
    • B64C35/005—Flying-boats; Seaplanes with propellers, rudders or brakes acting in the water

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)

Abstract

178,912. Bolas, H., and Parnall, G. G. Jan. 21, 1921. Floats of amphibious aircraft have a rear section which is hinged and resiliently mounted and provided with a tail skid. The Figure shows a central float 1 having a rear section 2 hinged at 3 and resiliently connected to the fuselage 6 through a strut or struts 4 and a shockabsorber 5. The section 2 carries the tail skid and a water rudder 8, or other fins. According to the Provisional Specification, the shock-absorber may be disposed betwen the rear section and the main body.
GB275921A 1921-01-21 1921-01-21 Improvements in aircraft Expired GB178912A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB275921A GB178912A (en) 1921-01-21 1921-01-21 Improvements in aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB275921A GB178912A (en) 1921-01-21 1921-01-21 Improvements in aircraft

Publications (1)

Publication Number Publication Date
GB178912A true GB178912A (en) 1922-04-21

Family

ID=9745342

Family Applications (1)

Application Number Title Priority Date Filing Date
GB275921A Expired GB178912A (en) 1921-01-21 1921-01-21 Improvements in aircraft

Country Status (1)

Country Link
GB (1) GB178912A (en)

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