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WO1994000343A1 - Autogire, son procede de transformation pour le stationnement et procede de reglage de son centre de gravite - Google Patents

Autogire, son procede de transformation pour le stationnement et procede de reglage de son centre de gravite Download PDF

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Publication number
WO1994000343A1
WO1994000343A1 PCT/RU1993/000150 RU9300150W WO9400343A1 WO 1994000343 A1 WO1994000343 A1 WO 1994000343A1 RU 9300150 W RU9300150 W RU 9300150W WO 9400343 A1 WO9400343 A1 WO 9400343A1
Authority
WO
WIPO (PCT)
Prior art keywords
carrier
rotor
οsi
gyroplane
uπρavleniya
Prior art date
Application number
PCT/RU1993/000150
Other languages
English (en)
Russian (ru)
Inventor
Kazimir Mikhailovich Zhidovetsky
Original Assignee
Aktsionernoe Obschestvo 'aviatika'
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 Aktsionernoe Obschestvo 'aviatika' filed Critical Aktsionernoe Obschestvo 'aviatika'
Priority to AU45923/93A priority Critical patent/AU4592393A/en
Publication of WO1994000343A1 publication Critical patent/WO1994000343A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/02—Gyroplanes

Definitions

  • the area of the invention is subject to the availability of aviation technology, 5 of which, in part, is missing from the presence of fire.
  • the rear engine of the Siesta “Sieva” S-30 was equipped with a fuselage, a front and rear axle, and a fixed chassis with a 25-speed chassis.
  • the spare parts of the auto-rotary latch are located in the main part of the direct and vertical partitions.
  • ⁇ v ⁇ zhi ⁇ had sis ⁇ emu u ⁇ avleniya av ⁇ i ⁇ uyuschim vin ⁇ m (Zhu ⁇ nal " ⁇ - delis ⁇ - ⁇ ns ⁇ u ⁇ " -w 1987 s ⁇ e 20 - 2 ⁇ )
  • C ⁇ v ⁇ - 2 ⁇ zhi ⁇ Sie ⁇ vy had nesuscheg ⁇ ⁇ yla.
  • ⁇ dn ⁇ v ⁇ emenn ⁇ with ⁇ yshe ⁇ ivedennym av ⁇ zhi ⁇ m Sie ⁇ vy was s ⁇ zdan ⁇ yla ⁇ y av ⁇ zhi ⁇ ⁇ -7-Z ⁇ , which had ⁇ yuzelyazh carrying ⁇ yl ⁇ , ⁇ v ⁇ s ⁇ v ⁇ e g ⁇ iz ⁇ n ⁇ aln ⁇ e and ve ⁇ i ⁇ al- n ⁇ e ⁇ e ⁇ enie, ⁇ e ⁇ n ⁇ e chassis n ⁇ s ⁇ v ⁇ y ⁇ y and 25 ⁇ ed ⁇ ani ⁇ eln ⁇ y ⁇ S ⁇ Y ⁇ y.
  • the directive control unit with the directional control is connected to the control unit with the pedals of the pilot.
  • the self-contained two-piece screw is mounted on a vertical suspension and is connected to the rear control panel of the pilot. Screw blade
  • a task, which is delivered before the eve of the accident, is the creation of such an accident, which would have been set aside from the rest of the terms and conditions of the case; to ⁇ ⁇ 94/00343
  • the ZS is equipped with a common replacement shovel for spare parts, which should be connected to the lever in the control box.
  • Each of the conditions in the Republic of Ecuador is made in the form of a three-dimensional connection to the shared internal, shared international
  • the method of regulating the operation of the data center is switched off in a permanent change of the power supply of the rotor of the main rotor screw of the center of the MSSS. Whether it is an ice-testing or a single remotely, they are not paying, they are decreasing - ⁇ - long-term and additional accessories are provided with a change in the operating condition of the main rotor and, if necessary, is fully operational
  • the device changes the general shags of the main rotor screws; Ka I. & 5 - a car in a compounded parking position.
  • Stabilization 12 in the eastern part of the building is made in the form of three separate connected stables of 26, 27 and 28, connected by the middle ends. Ranges 26 and 27 of their own free ends are mounted on power elements of the 29th pipe of the I fuselage with
  • Stage 28 with its own free end mounted on the pipe I of the fuselage and the left
  • the system has a rotor turn-off system 16. This system comes with a flexible 30% end coupled with a positive coupling through a clutch
  • the flexible shaft 30 (not shown) from the motor 8.
  • the flexible shaft 30 is integral with the leading gear 31 mounted on the drive 18, which is connected to a total of 16, which is 32.
  • section 34 is interconnected with an executive mechanism, 5 is connected to a lever (not by default) in the village.
  • the meaning of 33 through the thrust 36 is mainly associated with the shares (not shown) of the parts 23 and 24.
  • Started dumbbell 8 discharges a loose screw 9, which unloads the horizontal pull. In most cases, when the engine is started or, a bit later, it is necessary to cut off the main rotor 16 through the gnaw shaft 30. To avoid running
  • Sis ⁇ e- ma u ⁇ zvlenzhya ⁇ bschzhm sheg ⁇ m vin ⁇ z 16 s ⁇ e ⁇ i ⁇ vene ⁇ e- ⁇ im ⁇ b ⁇ az ⁇ m, ch ⁇ ⁇ bes ⁇ echivae ⁇ l ⁇ zs ⁇ yam 23 and 24 are two ⁇ ayni ⁇ ⁇ l ⁇ zheniya ⁇ corner us ⁇ an ⁇ v ⁇ i - with a zero angle of the angle and the competition.
  • the method of disassembling a car in a regular place may be made possible by the slitting device.
  • a fixed rotor 16 is not available.

Landscapes

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

Abstract

L'invention concerne l'industrie aéronautique, notamment la branche des autogires, leurs conception, production et exploitation. Un autogire comporte un fuselage se présentant sous la forme d'un tube (1), un support central vertical (2) se présentant également sous la forme d'un tube de même section que celle du tube du fuselage. Le genou central (3) est fixé rigidement au support (2), au tube du fuselage (1) et au siège (4) du pilote. Le train d'atterrissage est du type à trois points avec un support avant (5). L'unité motrice comprend un moteur (8) ainsi qu'une hélice propulsive (9). L'ensemble de queue est de type normal. Un support supplémentaire (17) est fixé articulé par une de ses extrémités au support (2), et par son autre extrémité il est fixé articulé au sabot de montage (18) du rotor principal. Des membrures de triangulation principale (19) et supplémentaire (21) sont de longueur réglable. Le rotor (16) est monté dans le sabot (18) un axe orienté parallèle à l'axe longitudinal de l'autogire de manière à pouvoir s'écarter de celui-ci. La transmission de commande (22) relie le système porteur et le rotor (16) à un manche (15), et elle permet de réguler la déviation du rotor (16) dans la chaîne de roulis par rapport au manche (15). L'autogire peut être transformé pour le stationnement par pliage et fixation des pales (23 et 24) du rotor (16), et son centre de gravité peut être réglé par changement de la longueur de ses membrures de triangulation principale (19) et supplémentaire (21).
PCT/RU1993/000150 1992-06-30 1993-06-25 Autogire, son procede de transformation pour le stationnement et procede de reglage de son centre de gravite WO1994000343A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU45923/93A AU4592393A (en) 1992-06-30 1993-06-25 Gyroplane, method of its transforming into parking configuration and method of its centre-of-gravity adjustment

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU5050052/23 1992-06-30
SU5005223 1992-06-30

Publications (1)

Publication Number Publication Date
WO1994000343A1 true WO1994000343A1 (fr) 1994-01-06

Family

ID=21586784

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU1993/000150 WO1994000343A1 (fr) 1992-06-30 1993-06-25 Autogire, son procede de transformation pour le stationnement et procede de reglage de son centre de gravite

Country Status (1)

Country Link
WO (1) WO1994000343A1 (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU713610B2 (en) * 1996-03-29 1999-12-09 Board Of Regents, The University Of Texas System Biomarkers for detection, diagnosis and prognosis of prostate cancer
US6089501A (en) * 1998-06-22 2000-07-18 Frost; Stanley A. Tandem-rotor gyroplane
US6435453B1 (en) * 1999-08-20 2002-08-20 Cartercopters, L.L.C. High speed rotor aircraft
WO2011131733A2 (fr) 2010-04-22 2011-10-27 Desaulniers Jean-Marc Joseph Engin gyropendulaire à propulsion compensatoire et collimation de gradient fluidique, multi-milieux, multimodal, à décollage et atterrissage vertical
US20120248240A1 (en) * 2008-04-21 2012-10-04 Boris Andreevich Polovinkin Vertical take-off and vertical landing gyroplane
WO2013060693A2 (fr) 2011-10-27 2013-05-02 Desaulniers Jean-Marc Joseph Exosquelette geometrique actif a carenage annulaire pseudo-rhomboedrique pour engin gyropendulaire

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1989544A (en) * 1931-04-08 1935-01-29 Autogiro Co Of America Aircraft of the rotative sustainingblade type
US3149802A (en) * 1961-09-11 1964-09-22 Voorhis F Wigal Autogiro
FR2251473A1 (en) * 1973-11-21 1975-06-13 Dudouyt Jean Paul Tubular framework gyroplane or autogyro - sliding section and seat adjust trim for varying component weights
GB2152461A (en) * 1984-01-10 1985-08-07 Kenneth Horatio Wallis Autogyros
US4653705A (en) * 1979-04-24 1987-03-31 Bensen Igor B Autogyro with auxiliary rotor drive

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1989544A (en) * 1931-04-08 1935-01-29 Autogiro Co Of America Aircraft of the rotative sustainingblade type
US3149802A (en) * 1961-09-11 1964-09-22 Voorhis F Wigal Autogiro
FR2251473A1 (en) * 1973-11-21 1975-06-13 Dudouyt Jean Paul Tubular framework gyroplane or autogyro - sliding section and seat adjust trim for varying component weights
US4653705A (en) * 1979-04-24 1987-03-31 Bensen Igor B Autogyro with auxiliary rotor drive
GB2152461A (en) * 1984-01-10 1985-08-07 Kenneth Horatio Wallis Autogyros

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
GORBENKO K.S. et al., "Samolety Stroim Sami", 1989, MASHINOSTROENIE, (Moscow), pages 86, 87, 186. *
KRYLYA RODINY, No. 2, 1990, "DOSAAFSSSR", (Moscow), page 26. *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU713610B2 (en) * 1996-03-29 1999-12-09 Board Of Regents, The University Of Texas System Biomarkers for detection, diagnosis and prognosis of prostate cancer
US6089501A (en) * 1998-06-22 2000-07-18 Frost; Stanley A. Tandem-rotor gyroplane
US6435453B1 (en) * 1999-08-20 2002-08-20 Cartercopters, L.L.C. High speed rotor aircraft
US20120248240A1 (en) * 2008-04-21 2012-10-04 Boris Andreevich Polovinkin Vertical take-off and vertical landing gyroplane
US8573528B2 (en) * 2008-04-21 2013-11-05 Boris Andreevich Polovinkin Vertical take-off and vertical landing gyroplane
WO2011131733A2 (fr) 2010-04-22 2011-10-27 Desaulniers Jean-Marc Joseph Engin gyropendulaire à propulsion compensatoire et collimation de gradient fluidique, multi-milieux, multimodal, à décollage et atterrissage vertical
WO2013060693A2 (fr) 2011-10-27 2013-05-02 Desaulniers Jean-Marc Joseph Exosquelette geometrique actif a carenage annulaire pseudo-rhomboedrique pour engin gyropendulaire

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