GB100532A - Improvements in Alighting and Landing Apparatus for Waterplanes and Aeroplanes. - Google Patents

Improvements in Alighting and Landing Apparatus for Waterplanes and Aeroplanes.

Info

Publication number
GB100532A
GB100532A GB6059/16A GB605916A GB100532A GB 100532 A GB100532 A GB 100532A GB 6059/16 A GB6059/16 A GB 6059/16A GB 605916 A GB605916 A GB 605916A GB 100532 A GB100532 A GB 100532A
Authority
GB
United Kingdom
Prior art keywords
aeroplanes
floats
axles
shock
waterplanes
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
GB6059/16A
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.)
AEROPLANES PAUL SCHMITT SOC NO
Original Assignee
AEROPLANES PAUL SCHMITT SOC NO
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 AEROPLANES PAUL SCHMITT SOC NO filed Critical AEROPLANES PAUL SCHMITT SOC NO
Publication of GB100532A publication Critical patent/GB100532A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C35/00—Flying-boats; Seaplanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Bridges Or Land Bridges (AREA)

Abstract

100,532. Soc. Nouvelle des AÚroplanes P. Schmitt. May 22, 1915, [Convention date]. Shock of landing, deadening; floats, arrangement of; land wheels.-A shock-absorbing device for aeroplanes or hydro-aeroplanes is adapted to resist shock in any direction and is described as applied to a machine having one central and two side floats. The three floats 8, 9, 9 are secured to transverse axles 2 which are connected to longitudinal members 1 on the underframe by rubber bands 7. Pins 6 mounted in plates 3 on the axles 2 are also connected by pairs of rubber loops 4 to brackets 5 on the members 1. The shockabsorbing device may be applied to hydro-aeroplanes having only one float, or the floats 8, 9, 9 may be replaced by land wheels mounted on the axles 2.
GB6059/16A 1915-05-22 1916-04-27 Improvements in Alighting and Landing Apparatus for Waterplanes and Aeroplanes. Expired GB100532A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR100532X 1915-05-22

Publications (1)

Publication Number Publication Date
GB100532A true GB100532A (en) 1917-04-27

Family

ID=32241751

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6059/16A Expired GB100532A (en) 1915-05-22 1916-04-27 Improvements in Alighting and Landing Apparatus for Waterplanes and Aeroplanes.

Country Status (1)

Country Link
GB (1) GB100532A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2641423A (en) * 1951-09-27 1953-06-09 Bell Aircraft Corp Aircraft undercarriage

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2641423A (en) * 1951-09-27 1953-06-09 Bell Aircraft Corp Aircraft undercarriage

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