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WO1998028188A1 - Aeronef combine - Google Patents

Aeronef combine Download PDF

Info

Publication number
WO1998028188A1
WO1998028188A1 PCT/RU1997/000409 RU9700409W WO9828188A1 WO 1998028188 A1 WO1998028188 A1 WO 1998028188A1 RU 9700409 W RU9700409 W RU 9700409W WO 9828188 A1 WO9828188 A1 WO 9828188A1
Authority
WO
WIPO (PCT)
Prior art keywords
gas
rigid
rotor
aerostatic
lighter
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.)
Ceased
Application number
PCT/RU1997/000409
Other languages
English (en)
Russian (ru)
Inventor
Yury Grigorievich Ishkov
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
Publication of WO1998028188A1 publication Critical patent/WO1998028188A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • 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

Definitions

  • the disadvantages of the aforementioned car are a low coefficient of usefulness and a small weight load.
  • the aforementioned task of the invention is achieved in that a combined flammable device containing a filled gas is easier to use than an air inlet of a hot gas unit. ⁇ 97 / 00409
  • Fig. 1 a general view of the com- bined mobile device in a parking lot with a minimum volume of aerospace and compressed is shown in schematic form.
  • Fig. 2 is a view of ⁇ ⁇ in Fig. 1 ; with a minimum volume of aerostatic body and compressed compression.
  • ⁇ a ⁇ ig.Z - view ⁇ ⁇ on ⁇ ig. ⁇ ⁇ i ma ⁇ simaln ⁇ m ⁇ bome ae ⁇ s ⁇ a ⁇ iches ⁇ g ⁇ ⁇ usa and ⁇ azzha ⁇ m sil ⁇ ne.
  • Fig. 4 - view in plan on Fig. 1.
  • Fig. 5 - view of ⁇ ⁇ in Fig. 4.
  • Fig. 6 - view of the ⁇ BB in Fig. 4.
  • ⁇ as ⁇ n ⁇ e ⁇ is ⁇ s ⁇ blenie aerostatic housing 8 is made in the form of a smooth hard drive 11 and its concentric direction ⁇ b ⁇ ymy 12 s ⁇ edinenny ⁇ between s ⁇ b ⁇ y zhes ⁇ imi ⁇ adial- GOVERNMENTAL elemen ⁇ ami 13.
  • the upper and lower 16 are equipped with the corresponding 17 leads and the 18th branch.
  • ⁇ a ⁇ she- dviga ⁇ eli stems 3 are provided in ⁇ v ⁇ nymi ve ⁇ i ⁇ aln ⁇ y ⁇ l ⁇ s ⁇ s ⁇ i gib ⁇ imi na ⁇ avlyayuschimi s ⁇ lami 19 s ⁇ edi- nennymi c ' ⁇ v ⁇ dyaschimi ⁇ a ⁇ ub ⁇ ami 18 nizhneg ⁇ s ⁇ a ⁇ ana 16 ⁇ ubcha ⁇ g ⁇ ⁇ eles ⁇ iches ⁇ g ⁇ ⁇ lle ⁇ a, ve ⁇ ny s ⁇ a ⁇ an 15 ⁇ g ⁇ ⁇ s ⁇ eds ⁇ v ⁇ m ⁇ dv ⁇ dyascheg ⁇ 17 ⁇ a ⁇ ub- ⁇ a s ⁇ edinen with segne ⁇ vym ⁇ les ⁇ m 20 ⁇ iv ⁇ da v ⁇ ascheniya nesuscheg ⁇ ⁇ a,
  • ⁇ e ⁇ s ⁇ a ⁇ iches ⁇ y ⁇ us 8 is provided elas ⁇ ich- n ⁇ y gaz ⁇ ne ⁇ nitsaem ⁇ y na ⁇ l ⁇ nn ⁇ y memb ⁇ an ⁇ y 24 at a fast pace of 11 and a quick 7, additionally connected friends with other flexible components, a long, long-distance the length of the bath, connected to a direct winch (not indicated otherwise on a fixed) with a fixed complete extension of the 6th integral 24-hour 7.
  • ⁇ ab ⁇ ae ⁇ ⁇ mbini ⁇ vanny le ⁇ a ⁇ elny a ⁇ a ⁇ a ⁇ ⁇ b ⁇ az ⁇ m follows: ⁇ e ⁇ ed za ⁇ us ⁇ m ma ⁇ shevy ⁇ dviga ⁇ e- leu 3 and u ⁇ avlyayuscheg ⁇ ⁇ iv ⁇ dn ⁇ g ⁇ vin ⁇ a 2 sil ⁇ n ⁇ m 14 us ⁇ an ⁇ vlivayu ⁇ predetermined ⁇ bem ae ⁇ s ⁇ a ⁇ iches ⁇ g ⁇ ⁇ u- ca 8 and za ⁇ lnyayu ⁇ ⁇ i e ⁇ m ball ⁇ ny 27 gaz ⁇ m easier v ⁇ z- du ⁇ a ⁇ d ⁇ ebuemym pressure ⁇ i e ⁇ m bottom 10 ⁇ b ⁇ - The crate is disposed of, and, in the final version, the hard elements of 25 adjustable lengths are pulled in and secured due to this unavoidable insecurity. 8
  • EXTENDED CAPACITY MUST BE USED AS FOR TRANSPORTATION OF OVERSIZED LOADS ON THE EXTERNAL SUSPENSION (THERE IS NOT CONSUMPTED FOR EXPLOSION),
  • a flying crane is available, and is equipped with an exhaust rotor for the main rotor and the inclusive blowing systems for domestic appliances.

Landscapes

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

Abstract

Cette invention concerne essentiellement un aéronef combiné qui comprend un corps aérostatique, convexe, imperméable aux gaz et en forme de disque, à l'intérieur duquel se trouve le tore creux et rigide d'une installation propulsive. Le tore est connecté par des éléments radiaux à l'enveloppe qui entoure le soufflet du mécanisme permettant de modifier le volume du corps. La cavité du corps est divisée par une membrane inclinée en une section qui renferme des ballons contenant un gaz plus léger que l'air, ainsi qu'en une section de ballastage thermique. L'installation propulsive est équipée d'une roue de Segner assurant la rotation du corps et d'un rotor porteur. Ce rotor se compose de pales horizontales qui sont connectées au tore et qui possèdent des ailettes verticales à leurs extrémités libres. Le tore rigide est connecté par l'intermédiaire d'éléments rigides, longitudinaux et de longueur réglable à un support. Ce dernier possède un palier de support dont l'un des corps est fixé à une nacelle. La nacelle comprend une hélice de commande, un châssis, ainsi que des moteurs de propulsion, lesquels sont connectés par des tuyères directionnelles, souples et rotatives et par l'intermédiaire d'un collecteur télescopique à la roue de Segner.
PCT/RU1997/000409 1996-12-24 1997-12-18 Aeronef combine Ceased WO1998028188A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU96123984A RU2114765C1 (ru) 1996-12-24 1996-12-24 Комбинированный летательный аппарат
RU96123984 1996-12-24

Publications (1)

Publication Number Publication Date
WO1998028188A1 true WO1998028188A1 (fr) 1998-07-02

Family

ID=20188345

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU1997/000409 Ceased WO1998028188A1 (fr) 1996-12-24 1997-12-18 Aeronef combine

Country Status (2)

Country Link
RU (1) RU2114765C1 (fr)
WO (1) WO1998028188A1 (fr)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2830838A1 (fr) * 2001-10-12 2003-04-18 Airstar Dirigeable semi-rigide a carene maintenue en conformation par une poche de gaz porteur comprimee par un coussin d'air
USD583294S1 (en) 2007-03-07 2008-12-23 Lta Corporation Airship
US7866601B2 (en) 2006-10-20 2011-01-11 Lta Corporation Lenticular airship
EA016905B1 (ru) * 2011-06-22 2012-08-30 Николай Федорович Хорьков Универсальный высокоманевренный летательный аппарат
US8297550B2 (en) 2007-08-09 2012-10-30 Lta Corporation Lenticular airship and associated controls
US8596571B2 (en) 2011-03-31 2013-12-03 Lta Corporation Airship including aerodynamic, floatation, and deployable structures
US8894002B2 (en) 2010-07-20 2014-11-25 Lta Corporation System and method for solar-powered airship
US9802690B2 (en) 2013-11-04 2017-10-31 Lta Corporation Cargo airship

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2475416C2 (ru) * 2011-02-07 2013-02-20 Анатолий Тимофеевич Кожанов Летательный аппарат
WO2021091521A1 (fr) * 2019-11-05 2021-05-14 Titov Dmytro Multicoptère avec mécanisme intégré d'aspiration d'air et de soufflage d'air

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4114837A (en) * 1977-03-24 1978-09-19 Skagit Corporation Air transport and lifting vehicle
US4685640A (en) * 1985-05-06 1987-08-11 Hystar Aerospace Development Corporation Air vehicle
US4695012A (en) * 1983-06-08 1987-09-22 Bernard Lindenbaum Aerial load-lifting system
US5082205A (en) * 1990-08-09 1992-01-21 Caufman Robert L Semi-buoyant composite aircraft with non-rotating aerostat

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3976265A (en) * 1973-05-07 1976-08-24 All American Industries, Inc. Semibuoyant composite aircraft
RU2059530C1 (ru) * 1992-12-14 1996-05-10 Александр Иосифович Филимонов Гибридный дирижабль конструкции а.и.филимонова
RU2066661C1 (ru) * 1993-01-11 1996-09-20 Евгений Анисимович Кирсанов Вертостат

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4114837A (en) * 1977-03-24 1978-09-19 Skagit Corporation Air transport and lifting vehicle
US4695012A (en) * 1983-06-08 1987-09-22 Bernard Lindenbaum Aerial load-lifting system
US4685640A (en) * 1985-05-06 1987-08-11 Hystar Aerospace Development Corporation Air vehicle
US5082205A (en) * 1990-08-09 1992-01-21 Caufman Robert L Semi-buoyant composite aircraft with non-rotating aerostat

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2830838A1 (fr) * 2001-10-12 2003-04-18 Airstar Dirigeable semi-rigide a carene maintenue en conformation par une poche de gaz porteur comprimee par un coussin d'air
US7866601B2 (en) 2006-10-20 2011-01-11 Lta Corporation Lenticular airship
US8109462B2 (en) 2006-10-20 2012-02-07 Lta Corporation Lenticular airship
USD583294S1 (en) 2007-03-07 2008-12-23 Lta Corporation Airship
US9840318B2 (en) 2007-08-09 2017-12-12 Pierre Balaskovic Lenticular airship and associated controls
US8297550B2 (en) 2007-08-09 2012-10-30 Lta Corporation Lenticular airship and associated controls
US8616503B2 (en) 2007-08-09 2013-12-31 Lta Corporation Lenticular airship and associated controls
US9828082B2 (en) 2007-10-18 2017-11-28 Lta Corporation Airship having a cargo compartment
US8899514B2 (en) 2010-07-20 2014-12-02 Lta Corporation System and method for varying airship aerostatic buoyancy
US8894002B2 (en) 2010-07-20 2014-11-25 Lta Corporation System and method for solar-powered airship
US9745042B2 (en) 2011-03-31 2017-08-29 Lta Corporation Airship including aerodynamic, floatation, and deployable structures
US8596571B2 (en) 2011-03-31 2013-12-03 Lta Corporation Airship including aerodynamic, floatation, and deployable structures
EA016905B1 (ru) * 2011-06-22 2012-08-30 Николай Федорович Хорьков Универсальный высокоманевренный летательный аппарат
US9802690B2 (en) 2013-11-04 2017-10-31 Lta Corporation Cargo airship

Also Published As

Publication number Publication date
RU2114765C1 (ru) 1998-07-10

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