GB191417990A - Improvements in Aeroplanes. - Google Patents

Improvements in Aeroplanes.

Info

Publication number
GB191417990A
GB191417990A GB191417990DA GB191417990A GB 191417990 A GB191417990 A GB 191417990A GB 191417990D A GB191417990D A GB 191417990DA GB 191417990 A GB191417990 A GB 191417990A
Authority
GB
United Kingdom
Prior art keywords
plane
keels
machine
main plane
keel
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
Inventor
Hugh D Olley Beningfield
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
Application granted granted Critical
Publication of GB191417990A publication Critical patent/GB191417990A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C17/00—Aircraft stabilisation not otherwise provided for

Abstract

17,990. Beningfield, H. D. July 30. Aerial machines without aerostats; planes, arrangement and construction of; tanks, arrangement of.- The main supporting- surface A of an aeroplane tapers in breadth from the back to the front and has an open front portion to form the two dart-shaped points 1, 2. Two keels B, C increasing in depth and thickness from the front to the rear are secured to the main plane and prevent the machine from side-slipping. The keels may be hollow tapered bodies to serve as floats for supporting the machine on water and as receptacles for supplies of petrol &c. The main plane is cambered longitudinally or transversely. The motor and propeller J are arranged between the keels about one-third of the overall length of the machine from its front end. Keel planes G', G' may be arranged above the plane A, and a keel G<3> above the tailplane D. Steering.-Elevators E<1>, E', F are arranged at the sides of the tail-plane D and between the pointed ends of the main plane.
GB191417990D 1914-07-30 1914-07-30 Improvements in Aeroplanes. Expired GB191417990A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191417990T 1914-07-30

Publications (1)

Publication Number Publication Date
GB191417990A true GB191417990A (en) 1915-04-15

Family

ID=34360962

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191417990D Expired GB191417990A (en) 1914-07-30 1914-07-30 Improvements in Aeroplanes.

Country Status (1)

Country Link
GB (1) GB191417990A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2245147A1 (en) * 2002-09-12 2005-12-16 Manuel Muñoz Saiz Lifting arrangement for aircraft fuselage

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2245147A1 (en) * 2002-09-12 2005-12-16 Manuel Muñoz Saiz Lifting arrangement for aircraft fuselage

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