EA200801643A1 - PARAMOTOR - Google Patents

PARAMOTOR

Info

Publication number
EA200801643A1
EA200801643A1 EA200801643A EA200801643A EA200801643A1 EA 200801643 A1 EA200801643 A1 EA 200801643A1 EA 200801643 A EA200801643 A EA 200801643A EA 200801643 A EA200801643 A EA 200801643A EA 200801643 A1 EA200801643 A1 EA 200801643A1
Authority
EA
Eurasian Patent Office
Prior art keywords
pilot
power plant
frame
seat
paramotor
Prior art date
Application number
EA200801643A
Other languages
Russian (ru)
Other versions
EA011142B1 (en
Inventor
Василий Андреевич Уваров
Original Assignee
Василий Андреевич Уваров
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 Василий Андреевич Уваров filed Critical Василий Андреевич Уваров
Priority to EA200801643A priority Critical patent/EA011142B1/en
Priority to EP08874634A priority patent/EP2300320A1/en
Priority to PCT/RU2008/000803 priority patent/WO2009151351A1/en
Publication of EA200801643A1 publication Critical patent/EA200801643A1/en
Publication of EA011142B1 publication Critical patent/EA011142B1/en

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
    • B64C31/036—Hang-glider-type aircraft; Microlight-type aircraft having parachute-type wing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)
  • Catching Or Destruction (AREA)
  • Housing For Livestock And Birds (AREA)
  • Agricultural Machines (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)

Abstract

Техническая проблема, на решение которой направлено настоящее изобретение, заключается в создании разборной конструкции парамотора, которая позволит в разобранном состоянии сформировать компактный багаж, удобный не только для перевозки наземным транспортом, допустимым для перевозки авиационным пассажирским транспортом, но также удобный и для переноски человеком, что позволит транспортировать парамотор без использования транспортных средств и добираться пилоту самостоятельно, пешком до труднодоступных мест взлета и выбираться из подобных мест самостоятельно в случае вынужденной посадки. Парамотор содержит раму, силовую установку и органы управления силовой установкой, съемный воздушный винт, установленный на выходном валу силовой установки, закрепленное на раме место пилота, имеющее сопряженные спинку и сиденье, силовые ремни для стыковки со свободными концами параплана и для страховки пилота, а также распорки для разведения силовых ремней для стыковки со свободными концами параплана над сидением места пилота в направлении его длины. Рама выполнена из моторной, на которой с одной стороны закреплена силовая установка, а с другой - место пилота, и опорной частей. Моторная и опорная части рамы выполнены со сплошными боковыми сторонами и соединены шарнирно или разъемно с возможностью расположения по меньшей мере части длины боковых сторон моторной и опорной частей по геометрическим ребрам, полученным сопряжением плоскостей четырех боковых граней фигуры, в объеме которой располагается силовая установка.The technical problem that the present invention is directed to is to create a collapsible paramotor structure that will allow to form compact luggage in a disassembled state, convenient not only for transportation by land vehicles acceptable for transportation by air passenger transport, but also convenient for carrying by man that allows the paramotor to be transported without the use of vehicles and to get to the pilot on its own, walking to hard-to-reach take-off areas approved places yourself in case of a forced landing. The paramotor contains a frame, a power plant and power plant controls, a removable propeller mounted on the output shaft of the power plant, a pilot seat fixed to the frame, having a mating back and seat, power belts for docking with the free ends of the paraglider and for the pilot insurance, as well as spacers for breeding power belts for docking with the free ends of the paraglider above the pilot's seat in the direction of its length. The frame is made of a motor, on which, on the one hand, the power plant is fixed, and on the other, the pilot's seat, and the supporting part. The motor and support parts of the frame are made with solid sides and are connected pivotally or detachably with the possibility of arranging at least part of the lengths of the sides of the motor and support parts along geometric edges obtained by conjugating the planes of the four lateral faces of the figure in the volume of which the power plant is located.

EA200801643A 2008-06-11 2008-06-11 Paramotor EA011142B1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EA200801643A EA011142B1 (en) 2008-06-11 2008-06-11 Paramotor
EP08874634A EP2300320A1 (en) 2008-06-11 2008-12-26 Paramotor
PCT/RU2008/000803 WO2009151351A1 (en) 2008-06-11 2008-12-26 Paramotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EA200801643A EA011142B1 (en) 2008-06-11 2008-06-11 Paramotor

Publications (2)

Publication Number Publication Date
EA200801643A1 true EA200801643A1 (en) 2009-02-27
EA011142B1 EA011142B1 (en) 2009-02-27

Family

ID=40849085

Family Applications (1)

Application Number Title Priority Date Filing Date
EA200801643A EA011142B1 (en) 2008-06-11 2008-06-11 Paramotor

Country Status (3)

Country Link
EP (1) EP2300320A1 (en)
EA (1) EA011142B1 (en)
WO (1) WO2009151351A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103057704B (en) * 2013-01-07 2015-07-29 南京航空航天大学 Rotor-type one-man aircraft
CN205989812U (en) 2015-06-25 2017-03-01 瑞德利斯技术公司 Many rotor wing unmanned aerial vehicles

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2655017A1 (en) * 1989-11-27 1991-05-31 Jacquot Philippe Motorised microlight flying device
FR2679867A1 (en) * 1991-08-01 1993-02-05 Blottin Georges Propulsion device intended to cause a pilot equipped with a parapent to fly
BE1011923A6 (en) * 1998-05-19 2000-03-07 Schreiner A convertible control system for paramotor
FR2817827A1 (en) 2000-12-08 2002-06-14 Francis Gardeur Auxiliary paraglider motor comprises electric engine which is able to be switched on or off during flight to give a choice of powered or unpowered flight to the user
RU2242402C1 (en) * 2003-08-15 2004-12-20 Бегак Александр Аркадьевич Motorized paraplane

Also Published As

Publication number Publication date
EP2300320A1 (en) 2011-03-30
WO2009151351A1 (en) 2009-12-17
EA011142B1 (en) 2009-02-27

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Legal Events

Date Code Title Description
MM4A Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s)

Designated state(s): AM MD TM

MM4A Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s)

Designated state(s): AZ BY KZ KG TJ

MM4A Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s)

Designated state(s): RU