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WO1996036533A1 - Aeroplane a commande par balancier - Google Patents

Aeroplane a commande par balancier Download PDF

Info

Publication number
WO1996036533A1
WO1996036533A1 PCT/RU1995/000093 RU9500093W WO9636533A1 WO 1996036533 A1 WO1996036533 A1 WO 1996036533A1 RU 9500093 W RU9500093 W RU 9500093W WO 9636533 A1 WO9636533 A1 WO 9636533A1
Authority
WO
WIPO (PCT)
Prior art keywords
carrier
πaρy
secured
wing
pair
Prior art date
Application number
PCT/RU1995/000093
Other languages
English (en)
Russian (ru)
Inventor
Mikhail Andreevich Mamykin
Original Assignee
Tovarischestvo S Ogranichennoi Otvetstvennostju 'arkhar'
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 Tovarischestvo S Ogranichennoi Otvetstvennostju 'arkhar' filed Critical Tovarischestvo S Ogranichennoi Otvetstvennostju 'arkhar'
Priority to PCT/RU1995/000093 priority Critical patent/WO1996036533A1/fr
Publication of WO1996036533A1 publication Critical patent/WO1996036533A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
    • B64C31/028—Hang-glider-type aircraft; Microlight-type aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
    • B64C39/068—Aircraft not otherwise provided for having disc- or ring-shaped wings having multiple wings joined at the tips

Definitions

  • the emptying of the aircraft is not available in the aviation industry, or, more precisely, is a flying machine, which is compatible with the electronic signal.
  • the dying invention may be used in connection with the creation of the SSSA ;: lungs :; and sve ⁇ ;; lungs :: flight: aptitude
  • the written-down flying device was performed by aerodynamics-garbage with :: it is the "flying light", which is the traditional for
  • Izves ⁇ en le ⁇ a ⁇ elny a ⁇ a ⁇ a ⁇ with ealansi ⁇ nym ⁇ avleniem Z ⁇ , alpha, 891 501
  • s ⁇ de ⁇ zhaschy ⁇ a ⁇ as ⁇ _ ⁇ az ⁇ vanny ⁇ ' ⁇ ⁇ D ⁇ L ⁇ Y0 ⁇ al ⁇ y
  • This problem is solved by the creation of a flying machine with an unbalanced control unit, which includes a flexible, portable or portable device.
  • the specified operational performance makes it possible to have a stable drive and to reduce the load due to excessive load:
  • each of which has its own end of the GREATest ⁇ il ⁇ of the element of each of the first Christmas trees has been connected to the FEDERAL
  • a medical device with a valency control, performed according to the agreement, contains case 1 (Fig. 1),
  • WELL 3 was performed in the form of a wing for a closed type of aerodynamic scheme "tandem" and has two interconnected carriers ⁇ ve.nosti 4,5.
  • the first front bearing is at least 4 / / tes ⁇ TRANS ⁇ there is a slight slight deformity, while the second is rear
  • angles of the body can be varied in a range of 5 to 45 ° and in ANY case, the device is stable and installed.
  • Front 1 side 3 contains a separate Christmas tree 6 and front and rear rear;; e ⁇ ⁇ inquire ⁇ 7.8.
  • SCAN 32 is secured to the end 1B.
  • the Christmas tree ⁇ of the rear pair in the vicinity of the city is part of the corresponding 7th front of the city.
  • WEDNESDAY 33 END OF STAGE 29 OF THEIR NEAREST SHARN UNIT 34 SEDED'- NOT WITH COMPLIANCE WITH ITS ELEKNA ⁇ -. ⁇ back ⁇ E ⁇ Y with the possibility of sliding along its ⁇ D ⁇ L ⁇ G. oh.
  • the “ShaNnNG” node 34 can be supplied with any of the most famous ⁇ S ⁇ U ⁇ - ⁇ financial ⁇ , intended for similar purposes;
  • the spherical nodes 14 and 34 may be suppressed, for example. neighborly supper ;; element ⁇ 41. Consequently ⁇ Fig. 3); from ⁇ effet ⁇ ⁇ ⁇ .: .:: SH .:U ⁇ .
  • Operation of the appliance is carried out with the following .-: ⁇ && ra .. OPERATION OF THE APPLIANCE IS SIMILAR TO OPERATION OF ANYONE ;: tripod ⁇ ggi ⁇ ggi ⁇ ;;; -; devices with unbalanced control.
  • Lift is created by the front and rear bearing support 4,5, ⁇ and 3, according to the ⁇ tandem ’, its
  • the emptying of the invention may result in the use of the SSSSSY; ;; lungs ;; and over ⁇ l ⁇ g ⁇ i ;; beneficial ;; devices with a balanced balance set to EN, which can be changed only by agricultural means, efficiently and automatically, and ⁇ 10 uchescheny; app.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)

Abstract

La présente invention concerne un aéroplane à commande par balancier comprenant une aile profilée souple (3) fixée à une ossature (1). L'aile (3) se présente sous la forme d'une aile de type fermé ayant une configuration aérodynamique 'tandem', et possède des surfaces portantes avant et arrière (4, 5) reliées entre elles et qui se trouvent respectivement en flèche arrière et en flèche inversée. L'ossature (1) comprend une poutre (6) longitudinale ainsi qu'une paire avant et une paire arrière de poutres latérales opposées (7, 8). Chaque poutre latérale (7) de la paire avant est fixée par sa première extrémité (9) à la partie nez (11) de la poutre longitudinale (6) et forme le bord d'attaque (12) de la surface portante avant (4) de l'aile (3). Chaque poutre latérale (8) de la paire arrière est fixée, d'une part, par sa première extrémité (13) à la partie queue (15) de la poutre longitudinale (6), et, d'autre part, par sa seconde extrémité (18) à la surface inférieure de la poutre latérale correspondante (7) de la paire avant, ceci de manière à former le bord d'attaque (20) de la surface portante arrière (5) de l'aile (3).
PCT/RU1995/000093 1995-05-15 1995-05-15 Aeroplane a commande par balancier WO1996036533A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/RU1995/000093 WO1996036533A1 (fr) 1995-05-15 1995-05-15 Aeroplane a commande par balancier

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/RU1995/000093 WO1996036533A1 (fr) 1995-05-15 1995-05-15 Aeroplane a commande par balancier

Publications (1)

Publication Number Publication Date
WO1996036533A1 true WO1996036533A1 (fr) 1996-11-21

Family

ID=20129924

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU1995/000093 WO1996036533A1 (fr) 1995-05-15 1995-05-15 Aeroplane a commande par balancier

Country Status (1)

Country Link
WO (1) WO1996036533A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005118392A1 (fr) * 2004-03-16 2005-12-15 The Boeing Company Vehicule aerodynamique pourvu d'une aile rapportee coplanaire a geometrie variable
CN106043481A (zh) * 2016-06-02 2016-10-26 北京航空航天大学 一种具有尾翼的扁平式四足滑翔机器人

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3936012A (en) * 1974-05-03 1976-02-03 Murray Stephen C Hang glider
DE2617033A1 (de) * 1976-04-17 1977-11-03 Herbert Weissert Eigenstabiles, durch gewichtsverlagerung steuerbares gleitflugzeug
US4116407A (en) * 1976-10-01 1978-09-26 Murray Stephen C Hang glider with collapsible airfoil
DE2854939A1 (de) * 1978-12-20 1980-07-10 Juergen Hartmann Drachengleiter
US4336913A (en) * 1979-10-02 1982-06-29 Hall Eric B Compound wing aircraft
US4541593A (en) * 1982-03-09 1985-09-17 Lucien Cabrol Aircraft providing with a lift structure incorporating multiple superposed wings

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3936012A (en) * 1974-05-03 1976-02-03 Murray Stephen C Hang glider
DE2617033A1 (de) * 1976-04-17 1977-11-03 Herbert Weissert Eigenstabiles, durch gewichtsverlagerung steuerbares gleitflugzeug
US4116407A (en) * 1976-10-01 1978-09-26 Murray Stephen C Hang glider with collapsible airfoil
DE2854939A1 (de) * 1978-12-20 1980-07-10 Juergen Hartmann Drachengleiter
US4336913A (en) * 1979-10-02 1982-06-29 Hall Eric B Compound wing aircraft
US4541593A (en) * 1982-03-09 1985-09-17 Lucien Cabrol Aircraft providing with a lift structure incorporating multiple superposed wings

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005118392A1 (fr) * 2004-03-16 2005-12-15 The Boeing Company Vehicule aerodynamique pourvu d'une aile rapportee coplanaire a geometrie variable
US7249734B2 (en) 2004-03-16 2007-07-31 The Boeing Company Aerodynamic vehicle having a variable geometry, co-planar, joined wing
CN106043481A (zh) * 2016-06-02 2016-10-26 北京航空航天大学 一种具有尾翼的扁平式四足滑翔机器人
CN106043481B (zh) * 2016-06-02 2018-08-10 北京航空航天大学 一种具有尾翼的扁平式四足滑翔机器人

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