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GB190907209A - Improvements in Flying Machines, Air Ships, and the like. - Google Patents

Improvements in Flying Machines, Air Ships, and the like.

Info

Publication number
GB190907209A
GB190907209A GB190907209DA GB190907209A GB 190907209 A GB190907209 A GB 190907209A GB 190907209D A GB190907209D A GB 190907209DA GB 190907209 A GB190907209 A GB 190907209A
Authority
GB
United Kingdom
Prior art keywords
wings
ribs
wing
arms
over pulleys
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
Louis Breguet
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 GB190907209A publication Critical patent/GB190907209A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

7209. BrÚguet, L. Oct. 28, 1908, [Convention date]. Balancing automatically by oppositely tilting wings connected in pairs. The lateral balance of an aerial machine is maintained by so connecting the sustaining-wings that a variation in wind pressure deflecting the wing on one side is balanced by an equal and opposite deflexion of the wing on the other side. The main ribs a of the wings may for this purpose (1) be differentially geared as shown in Fig. 1, or (2) be provided with arms f, Fig. 2, connected with a pivoted beam h; or (3) these arms may be connected to a continuous belt running over pulleys, or (4) a belt may run over pulleys mounted on the ribs a. Planes, construction of.-The fabric &c. of the wings is preferably supported by cross-ribs b, Fig. 7, mounted with limited spring-controlled movement on the rib a.
GB190907209D 1908-10-28 1909-03-25 Improvements in Flying Machines, Air Ships, and the like. Expired GB190907209A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR190907209X 1908-10-28

Publications (1)

Publication Number Publication Date
GB190907209A true GB190907209A (en) 1909-12-02

Family

ID=32407122

Family Applications (1)

Application Number Title Priority Date Filing Date
GB190907209D Expired GB190907209A (en) 1908-10-28 1909-03-25 Improvements in Flying Machines, Air Ships, and the like.

Country Status (1)

Country Link
GB (1) GB190907209A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2584667A (en) * 1947-02-14 1952-02-05 George E Bockrath Gust alleviating control means for airplanes
US3140844A (en) * 1963-03-29 1964-07-14 Alan H Rich Aircraft stabilization device
US4483498A (en) * 1982-07-14 1984-11-20 Mcdonnell Douglas Corporation Flight control surface coupling system
US5280863A (en) * 1991-11-20 1994-01-25 Hugh Schmittle Lockable free wing aircraft
US5340057A (en) * 1991-11-20 1994-08-23 Freewing Aerial Robotics Corporation Thrust vectoring free wing aircraft
US5395073A (en) * 1992-03-13 1995-03-07 Freewing Aerial Robotics Corporation STOL/VTOL free wing aircraft with articulated tail boom
US5769359A (en) * 1993-01-22 1998-06-23 Freewing Aerial Robotics Corporation Active feedback loop to control body pitch in STOL/VTOL free wing aircraft
US5863013A (en) * 1991-11-20 1999-01-26 Freewing Aerial Robotics Corporation STOL/VTOL free wing aircraft with improved shock dampening and absorbing means
USRE36487E (en) * 1989-02-09 2000-01-11 Freewing Aerial Robotics Corporation Airplane with variable-incidence wing

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2584667A (en) * 1947-02-14 1952-02-05 George E Bockrath Gust alleviating control means for airplanes
US3140844A (en) * 1963-03-29 1964-07-14 Alan H Rich Aircraft stabilization device
US4483498A (en) * 1982-07-14 1984-11-20 Mcdonnell Douglas Corporation Flight control surface coupling system
USRE36487E (en) * 1989-02-09 2000-01-11 Freewing Aerial Robotics Corporation Airplane with variable-incidence wing
US5280863A (en) * 1991-11-20 1994-01-25 Hugh Schmittle Lockable free wing aircraft
US5340057A (en) * 1991-11-20 1994-08-23 Freewing Aerial Robotics Corporation Thrust vectoring free wing aircraft
US5863013A (en) * 1991-11-20 1999-01-26 Freewing Aerial Robotics Corporation STOL/VTOL free wing aircraft with improved shock dampening and absorbing means
US5395073A (en) * 1992-03-13 1995-03-07 Freewing Aerial Robotics Corporation STOL/VTOL free wing aircraft with articulated tail boom
US5769359A (en) * 1993-01-22 1998-06-23 Freewing Aerial Robotics Corporation Active feedback loop to control body pitch in STOL/VTOL free wing aircraft

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