WO2016153328A3 - Аппарат самоперемещения и его составляющие - Google Patents

Аппарат самоперемещения и его составляющие Download PDF

Info

Publication number
WO2016153328A3
WO2016153328A3 PCT/KZ2016/000005 KZ2016000005W WO2016153328A3 WO 2016153328 A3 WO2016153328 A3 WO 2016153328A3 KZ 2016000005 W KZ2016000005 W KZ 2016000005W WO 2016153328 A3 WO2016153328 A3 WO 2016153328A3
Authority
WO
WIPO (PCT)
Prior art keywords
smas
self
novel
propeller
economical
Prior art date
Application number
PCT/KZ2016/000005
Other languages
English (en)
French (fr)
Other versions
WO2016153328A2 (ru
Inventor
Алдан Асанович САПАРГАЛИЕВ
Original Assignee
Алдан Асанович САПАРГАЛИЕВ
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 Алдан Асанович САПАРГАЛИЕВ filed Critical Алдан Асанович САПАРГАЛИЕВ
Priority to AU2016236896A priority Critical patent/AU2016236896A1/en
Priority to US15/559,749 priority patent/US20180044014A1/en
Priority to CA2980117A priority patent/CA2980117A1/en
Priority to EP16769146.8A priority patent/EP3272648A4/en
Publication of WO2016153328A2 publication Critical patent/WO2016153328A2/ru
Publication of WO2016153328A3 publication Critical patent/WO2016153328A3/ru

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
    • B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
    • B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16—Blades
    • B64C11/20—Constructional features
    • B64C11/28—Collapsible or foldable blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • B64C23/069—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/16—Frontal aspect
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/56—Folding or collapsing to reduce overall dimensions of 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/08—Aircraft not otherwise provided for having multiple wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T70/00—Maritime or waterways transport
    • Y02T70/50—Measures to reduce greenhouse gas emissions related to the propulsion system

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
  • Superconductive Dynamoelectric Machines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Настоящее изобретение относится к SMA (SMA - self-moving apparatus) использующие любых видов движителей, в том числе FPGB (FPGB - пропеллерно- приводной блок), содержащий пропеллер FP (FP - пропеллер) и привод для подвода к нему мощности. В частности, данное изобретение описывает: - новые виды энергоэффективных (экономичных) FPGB; - новые концептуальные конструкции SMA, которые позволяют создать экономичные и обладающие большой удельной мощностью SMA. Изобретение может быть использовано для создания новых энергоэффективных видов SMA и для широкомасштабного (массового) использования компактных и экологический чистых электрических двигателей, взамен экологический вредных и громоздких двигателей внутреннего сгорания.
PCT/KZ2016/000005 2015-03-20 2016-03-18 Аппарат самоперемещения и его составляющие WO2016153328A2 (ru)

Priority Applications (4)

Application Number Priority Date Filing Date Title
AU2016236896A AU2016236896A1 (en) 2015-03-20 2016-03-18 Self-moving apparatus and components thereof
US15/559,749 US20180044014A1 (en) 2015-03-20 2016-03-18 Self-moving apparatus and components thereof
CA2980117A CA2980117A1 (en) 2015-03-20 2016-03-18 Self-moving apparatus and components thereof
EP16769146.8A EP3272648A4 (en) 2015-03-20 2016-03-18 Self-moving apparatus and components thereof

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
KZ20150414 2015-03-20
KZ2015/0414.1 2015-03-20

Publications (2)

Publication Number Publication Date
WO2016153328A2 WO2016153328A2 (ru) 2016-09-29
WO2016153328A3 true WO2016153328A3 (ru) 2016-12-15

Family

ID=56977452

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/KZ2016/000005 WO2016153328A2 (ru) 2015-03-20 2016-03-18 Аппарат самоперемещения и его составляющие

Country Status (5)

Country Link
US (1) US20180044014A1 (ru)
EP (1) EP3272648A4 (ru)
AU (1) AU2016236896A1 (ru)
CA (1) CA2980117A1 (ru)
WO (1) WO2016153328A2 (ru)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3036096A1 (fr) * 2015-05-11 2016-11-18 Christian Roger Rene Deslypper Avion convertible a rotors decouvrables
DE102018116147A1 (de) * 2018-07-04 2020-01-09 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
WO2020055221A1 (ru) * 2018-09-10 2020-03-19 Алдан Асанович САПАРГАЛИЕВ Энергоэффективный лопастной винт
CN109798808B (zh) * 2018-12-25 2023-09-26 中国工程物理研究院总体工程研究所 一种箭载发射折叠翼巡飞弹脱伞机构
CN110001944B (zh) * 2019-03-22 2024-01-05 深圳先进技术研究院 一种大型无人机
CN111532402B (zh) * 2020-04-21 2022-02-08 大连理工大学 一种基于普通旋翼和摆线推进器的跨介质航行器

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5433400A (en) * 1991-11-27 1995-07-18 Singhal; Tara C. Aircraft design
RU2209746C1 (ru) * 2002-07-23 2003-08-10 Макаров Игорь Альбертович Летательный аппарат
US20100264256A1 (en) * 2009-04-16 2010-10-21 The Trustees Of The University Of Pennsylvania Counter-rotational inertial control of rotorcraft
US20110272520A1 (en) * 2009-10-30 2011-11-10 Beijing University Of Technology Electrical driven flying saucer based on magnetic suspension
RU2482010C2 (ru) * 2010-11-01 2013-05-20 Владимир Михайлович Палецких Способ образования махов и устройство для его осуществления в виде машущего винта

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5433400A (en) * 1991-11-27 1995-07-18 Singhal; Tara C. Aircraft design
RU2209746C1 (ru) * 2002-07-23 2003-08-10 Макаров Игорь Альбертович Летательный аппарат
US20100264256A1 (en) * 2009-04-16 2010-10-21 The Trustees Of The University Of Pennsylvania Counter-rotational inertial control of rotorcraft
US20110272520A1 (en) * 2009-10-30 2011-11-10 Beijing University Of Technology Electrical driven flying saucer based on magnetic suspension
RU2482010C2 (ru) * 2010-11-01 2013-05-20 Владимир Михайлович Палецких Способ образования махов и устройство для его осуществления в виде машущего винта

Also Published As

Publication number Publication date
WO2016153328A2 (ru) 2016-09-29
US20180044014A1 (en) 2018-02-15
EP3272648A4 (en) 2018-12-19
AU2016236896A1 (en) 2017-11-02
CA2980117A1 (en) 2016-09-29
EP3272648A2 (en) 2018-01-24

Similar Documents

Publication Publication Date Title
WO2016153328A3 (ru) Аппарат самоперемещения и его составляющие
GB2551552B (en) An aircraft gas turbine engine comprising non-coaxial propulsors driven by an engine core comprising two axially spaced core modules
CA2956697C (fr) Dispositif d'assistance rapide pour une turbomachine a turbine libre d'un aeronef
WO2013103542A3 (en) Flexible fuel generator and methods of use thereof
MX364927B (es) Motor de combustión interna que usa como combustible una mezcla a base de agua y método para operar el mismo.
EP3209871A4 (en) Internal combustion engines including electric starting system powered by lithium-ion battery
MY182276A (en) Propulsion system for a vessel
MX364294B (es) Dispositivo compensador para un motor de combustion interna.
GB2540093A (en) Vehicle with a start-stop system wherein the starter-generator is directly coupled to the internal combustion engine
MX344767B (es) Volante de inercia de motor generador de energía eléctrica con control de par de torsión activo.
EP3472442A4 (en) POWER SUPPLY SYSTEM WITH INTERNAL COMBUSTION ENGINE
MX355460B (es) Procedimiento de producción de un pistón para un motor de combustión interna.
UY35647A (es) Aparato para mejorar la combustión del combustible de motores de combustión interna
JP2016037909A5 (ru)
EP3494300A4 (en) INTERNAL COMBUSTION ENGINE INTAKE POWER AMPLIFIER SYSTEM
JP2017190736A5 (ru)
PH12013000317A1 (en) Engine
EP3327268A4 (en) COMBUSTION ENGINE WITH WATER AS A AUXILIARY DRIVE
RU2012140156A (ru) Двигательная установка с электромеханическим приводом винтов воздушного судна (вс)
EP2806135A3 (en) Cooling apparatus for internal combustion engine and motorcycle including same
PL410274A1 (pl) Napęd statku
WO2011141944A3 (en) Apparatus for independent instant production of freshwater from desalination of seawater aboard seafaring craft
AU2016903259A0 (en) Invention on improving an Engine's efficiency by heat preservation, and engines employing this invention
EP2765287A3 (en) Additional power supply apparatus, in particular for electric vehicles or the like
GR1008662B (el) Πιεζοηλεκτρικος κινητηρας

Legal Events

Date Code Title Description
ENP Entry into the national phase

Ref document number: 2980117

Country of ref document: CA

WWE Wipo information: entry into national phase

Ref document number: 15559749

Country of ref document: US

NENP Non-entry into the national phase

Ref country code: DE

REEP Request for entry into the european phase

Ref document number: 2016769146

Country of ref document: EP

ENP Entry into the national phase

Ref document number: 2016236896

Country of ref document: AU

Date of ref document: 20160318

Kind code of ref document: A

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 16769146

Country of ref document: EP

Kind code of ref document: A2