SU558632A3 - Airship semi-rigid design - Google Patents

Airship semi-rigid design

Info

Publication number
SU558632A3
SU558632A3 SU1264599A SU1264599A SU558632A3 SU 558632 A3 SU558632 A3 SU 558632A3 SU 1264599 A SU1264599 A SU 1264599A SU 1264599 A SU1264599 A SU 1264599A SU 558632 A3 SU558632 A3 SU 558632A3
Authority
SU
USSR - Soviet Union
Prior art keywords
airship
nozzle
power
central body
ship
Prior art date
Application number
SU1264599A
Other languages
Russian (ru)
Inventor
Папст Герман
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 filed Critical
Application granted granted Critical
Publication of SU558632A3 publication Critical patent/SU558632A3/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
    • B64B1/64—Gas valve operating mechanisms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/12—Movable control surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
    • B64B1/60—Gas-bags surrounded by separate containers of inert gas
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
    • B64B1/62—Controlling gas pressure, heating, cooling, or discharging gas

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Circuit Arrangements For Discharge Lamps (AREA)

Description

1one

Изобретение относитс  к воздухоплавательной технике, в частности к управл емым полужестким дирижабл м.FIELD OF THE INVENTION The invention relates to aeronautical engineering, in particular, to controlled semirigid airship meters.

Известен дирижабль полужесткой конструкции , включающий корпус, выполненный из двухстепной эластичной оболочки, укрепленную в нижней его части гондолу, силовую и компрессорную установки, расположенные в килевом каркасе 1.Known airship semi-rigid structure, comprising a housing made of two-step elastic sheath, reinforced in the lower part of the gondola, power and compressor installation, located in the keel frame 1.

Недостатком известного дирижабл   вл етс  то, что его органы управлени  и стабилизации не всегда обеспечивают эффективное управление кораблем, особенно на малых скорост х полета и при плавании.A disadvantage of the known airship is that its control and stabilization bodies do not always provide effective control of the ship, especially at low flight speeds and when sailing.

Цель изобретени  - создание таких ортанов управлени  и стабилизации дирижабл , силова  установка которых позвол ет осуществл ть одновременное управление головной и кормовой част ми дирижабл  даже тогда , когда последний не совершает поступательного движени  в горизонтальной плоскости .The purpose of the invention is the creation of such control or stabilization airships, the propulsion of which allows simultaneous control of the head and aft parts of the airship even when the latter does not perform translational motion in the horizontal plane.

Цель достигаетс  тем, что, по крайней мере в одной из наиболее удаленных точек на продольной оси дирижабл , например носовой , установлено регулируемое силовое сопло с управл емым центральным телом, выполненным с возмол ностью перемещени  параллельно продольной оси силового сопла и снабженным управл ющей конической наружной поверхностью.The goal is achieved by the fact that at least at one of the most distant points on the longitudinal axis of the airship, for example the nose, an adjustable power nozzle is installed with a controlled central body, made with the possibility of moving parallel to the longitudinal axis of the power nozzle and provided with a control conical outer surface .

На фиг. 1 схематически изобрал ен предлагаемый дирижабль, общий вид; на фиг. 2 - носовое сопло, сечение; на фиг. 3 - стабилизирующее силовое сопло кормовой части дирижабл , сечение.FIG. 1 schematically depicted the proposed airship, general view; in fig. 2 - nose nozzle, cross section; in fig. 3 - airship aft power nozzle, cross section.

Дирижабль состоит из удобообтекаемого корпуса 1, наполненного несущим газом, килевого каркаса гондолы 2, в котором установлены силовые и компрессорные установки (на чертеже не показаны), св занные трубопроводами с кормовым силовым и стабилизирующим соплом 3 и НОСОВЫМ 4.The airship consists of a streamlined body 1 filled with a carrier gas, the keel frame of the nacelle 2, in which power and compressor units are installed (not shown) connected by pipelines to the aft power and stabilizing nozzle 3 and the Bow 4.

Носовое сопло имеет образованное рулевой конической поверхностью 5 и внешней стенкой оболочки 6 щелевидное выпускное отверстие 7, по которому воздушна  стру  силовой установки направлена назад. Рулева  коническа  поверхность 5 шарнирно установлена на центральном теле 8 носового сопла и может выборочно отклон тьс  вперед, обеспечива  выход струи силовой установки вперед дл  торможени  и управлени  кораблем.The nose nozzle has a slit-like outlet opening 7 formed by the steering conical surface 5 and the outer wall of the shell 6, along which the air jet of the power plant is directed backwards. The rudder conical surface 5 is pivotally mounted on the central body 8 of the nose-nozzle and can be selectively deflected forward, allowing the jet of the propulsion unit to come forward to brake and steer the ship.

Claims (1)

Центральное тело 8 переднего сопла установлено на гидро- или пневмоцилиндрах 9, с помощью которых может мен ть свое положение как аксиально, так и радиально, параллельно продольной оси силового сопла, или полностью, или радиально эксцентрично, увеличива  или уменьша  выпускное отверстие, обеспечива  тем самым движение и управление кораблем. Стабилизирующее и силовое кормовое сопло 3 снабжено установленным на гидро- или нневмоцилиндрах 10 центральным телом И, с помощью которого измен ют силу н направление истечени  газовой струн, обеспечива  тем самым управление кораблем. Кроме того, дл  управлени  кораблем на центральном теле 11 шарнирно установлена управл юща  коническа  поверхность 12, выполненна  в виде пластин. Формула изобретени  Дирижабль полужесткой конструкции, включающий корпус, выполненный из двухстенной эластичной оболочки, укрепленную в нижней его части гондолу, силовую и компрессорную установки, расположенные в кплевом каркасе , отличаю щ и и с   тем, что, с целью повышени  маневренности н улучщени  стабильности полета дирижабл , по крайней мере в одной из наиболее удаленных точек на продольной осн дирижабл , например носовой, установлено регулируемое силовое сопло с управл емым центральным телом, выполненным с возможностью перемещени  параллельно продольной осн силового сопла и снабй енным управл ющей конической наружной поверхностью . Источник информации, прин тый во внимание при экспертизе; 1. Патент СССР № 19926, кл. 62а, 12/02, 1931.The central body 8 of the front nozzle is mounted on hydraulic or pneumatic cylinders 9, with which it can change its position both axially and radially, parallel to the longitudinal axis of the power nozzle, or completely or radially eccentric, increasing or decreasing the outlet orifice, thereby providing movement and control of the ship. The stabilizing and power aft nozzle 3 is provided with a central body I installed on hydraulic or non-cylinders 10, with which the force and direction of the flow of gas strings is changed, thereby controlling the ship. In addition, for controlling the ship, on the central body 11, a control conic surface 12 is pivotally mounted in the form of plates. The invention The airship is a semi-rigid structure, comprising a body made of a double-walled elastic casing, a gondola fixed in its lower part, a power and compressor installation located in the frame frame, and with the aim of improving maneuverability and improving the stability of the airship , at least one of the most distant points on the longitudinal axis of the airship, for example, the nose, has an adjustable power nozzle with a controlled central body that can be moved parallel to the longitudinal axis of the power nozzle and provided with a control conical outer surface. The source of information taken into account in the examination; 1. Patent of the USSR No. 19926, cl. 62a, 12/02, 1931. 10ten ш.Зs.Z
SU1264599A 1966-04-09 1968-08-19 Airship semi-rigid design SU558632A3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DEP0039186 1966-04-09
DEP0041101 1966-12-24

Publications (1)

Publication Number Publication Date
SU558632A3 true SU558632A3 (en) 1977-05-15

Family

ID=25990496

Family Applications (2)

Application Number Title Priority Date Filing Date
SU1147757A SU520896A3 (en) 1966-04-09 1967-04-08 Airship airship shell
SU1264599A SU558632A3 (en) 1966-04-09 1968-08-19 Airship semi-rigid design

Family Applications Before (1)

Application Number Title Priority Date Filing Date
SU1147757A SU520896A3 (en) 1966-04-09 1967-04-08 Airship airship shell

Country Status (16)

Country Link
US (1) US3456903A (en)
JP (2) JPS4886298A (en)
AT (3) AT294589B (en)
BE (1) BE696793A (en)
CH (1) CH475125A (en)
DE (1) DE1481222C3 (en)
DK (2) DK133186C (en)
ES (1) ES338923A1 (en)
FI (1) FI49947C (en)
GB (2) GB1191321A (en)
IL (1) IL27731A (en)
LU (1) LU53360A1 (en)
NL (1) NL152804B (en)
NO (1) NO119396B (en)
SE (4) SE363072B (en)
SU (2) SU520896A3 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010011153A1 (en) * 2008-07-23 2010-01-28 Sukharevskiy Vladimir Vladimir Helium airship

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3844507A (en) * 1969-09-09 1974-10-29 H Papst Process for the transportation of impellent gases, for example natural gas, and apparatus for carrying out the process
US3897032A (en) * 1970-02-26 1975-07-29 Hermann Ernst Robert Papst Method for operating airships, particularly by means of hydrocarbon gas or hydrogen
US3791611A (en) * 1972-09-11 1974-02-12 L Babbidge Captive inflated lighter-than-air structures
US4032085A (en) * 1973-03-21 1977-06-28 Papst Hermann E R Dirigible, especially non-rigid dirigible
US3972493A (en) * 1975-01-29 1976-08-03 Milne William G Docking device for a dirigible
US3972492A (en) * 1975-01-29 1976-08-03 Milne William G Airship for transporting gas
USRE30391E (en) 1976-02-23 1980-09-02 Abbott Laboratories Chemical analysis cuvette
US4055316A (en) * 1976-04-07 1977-10-25 John Lester Chipper Method and equipment for aerial transport
DE3008071A1 (en) * 1980-03-03 1981-09-17 Verseidag-Industrietextilien Gmbh, 4150 Krefeld BALLOON FABRIC FOR HOT AIR BALLOONS
FR2581022B1 (en) * 1985-04-25 1987-11-20 Centre Nat Etd Spatiales DEVICE FOR COUPLING AN ENVELOPE WITH AN ELEMENT EXTERNAL TO THE ENVELOPE
US4640474A (en) * 1985-08-05 1987-02-03 Manseth Robert A Method and apparatus for aerially transporting loads
US5743786A (en) * 1996-05-30 1998-04-28 Lindsey; Alan Balloon face polyhedra
GB9718211D0 (en) * 1997-08-29 1997-11-05 James Peter A lighter than air low vacuum air displacement -the bucky balloon
US6119979A (en) * 1997-09-15 2000-09-19 Sky Station International, Inc. Cyclical thermal management system
US5890676A (en) * 1997-11-21 1999-04-06 Coleman; Richard Airship with neutral buoyancy fuel bladder
GB2346593B (en) 1999-02-09 2003-01-08 Airship Tech Serv Ltd Airship bow thruster apparatus
JP3076842B1 (en) * 1999-03-29 2000-08-14 工業技術院長 Super pressure type altitude airship
JP2003054495A (en) 2001-08-08 2003-02-26 Inst Of Space & Astronautical Science Balloon
US7500637B2 (en) * 2005-09-30 2009-03-10 Lockheed Martin Corporation Airship with lifting gas cell system
US8286910B2 (en) * 2006-01-10 2012-10-16 Kamal Alavi Unmanned aircraft for telecommunicative or scientific purposes
US8459589B2 (en) * 2009-05-15 2013-06-11 Lockheed Martin Corporation External pressurization system for lighter than air vehicles
US20110062289A1 (en) * 2009-09-14 2011-03-17 Chu Adam N Envelope With Gas Management System For Lighter-Than-Air Aircraft
BRPI1001654B1 (en) * 2010-06-07 2020-12-15 Hans Georg Kraus SUPER-HARD AIRCRAFT CONTINUOUSLY SELF-SUSTAINABLE, ITS STRUCTURAL CHARACTERISTICS AND ITS CONSTRUCTIVE PROCESS
GB2482340A (en) 2010-07-30 2012-02-01 Davidson Technology Ltd High altitude tethered platform
CN102806988B (en) * 2012-08-30 2015-01-28 湖南航天机电设备与特种材料研究所 Inflatable control surface of large aerostat
RU2578834C2 (en) * 2014-06-18 2016-03-27 Николай Борисович Шульгин Vestaplan-vertostat gliding and deployment methods thereof
US12054235B2 (en) * 2017-07-03 2024-08-06 Lifting Gas Limited Flame arrester for the safer use of hydrogen as a lifting gas in airships
FR3120798A1 (en) * 2021-03-16 2022-09-23 Safran Nacelles Aircraft lattice structure to prevent the spread of fire and aircraft

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE316005C (en) *
NL57542C (en) *
US2275771A (en) * 1940-08-14 1942-03-10 Kimbel Guy John Power driven balloon
US2396494A (en) * 1941-07-16 1946-03-12 Wingfoot Corp Airship
US2478792A (en) * 1946-07-02 1949-08-09 Trey Serge Airship
US3346216A (en) * 1964-07-23 1967-10-10 Desmarteau Paul Airship

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010011153A1 (en) * 2008-07-23 2010-01-28 Sukharevskiy Vladimir Vladimir Helium airship

Also Published As

Publication number Publication date
AT293886B (en) 1971-10-25
GB1191322A (en) 1970-05-13
NL152804B (en) 1977-04-15
SE363072B (en) 1974-01-07
JPS4886297A (en) 1973-11-14
NO119396B (en) 1970-05-11
DE1481222C3 (en) 1975-01-23
AT294589B (en) 1971-11-25
ES338923A1 (en) 1968-09-01
DE1481222B2 (en) 1974-05-30
DE1481222A1 (en) 1970-01-15
GB1191321A (en) 1970-05-13
FI49947B (en) 1975-07-31
IL27731A (en) 1971-06-23
FI49947C (en) 1975-11-10
DK133186C (en) 1976-09-06
DK123578B (en) 1972-07-10
AT300581B (en) 1972-07-25
SE347711B (en) 1972-08-14
SU520896A3 (en) 1976-07-05
DK133186B (en) 1976-04-05
US3456903A (en) 1969-07-22
CH475125A (en) 1969-07-15
NL6704983A (en) 1967-10-10
SE357523B (en) 1973-07-02
SE328193B (en) 1970-09-07
BE696793A (en) 1967-10-09
JPS4886298A (en) 1973-11-14
LU53360A1 (en) 1967-10-05

Similar Documents

Publication Publication Date Title
SU558632A3 (en) Airship semi-rigid design
US3041992A (en) Low drag submarine
US2928238A (en) Jet deflector and orifice control
US3779199A (en) Boundary layer control means
US3604661A (en) Boundary layer control means
US4151893A (en) Wing in ground effect vehicle
US2384893A (en) Aircraft
US5294076A (en) Airship and method for controlling its flight
US3302602A (en) Submersible vessels
US2537487A (en) Adjustable exhaust for jetpropelled aircraft
US3361386A (en) Vertical or short take-off and landing aircraft
US3155342A (en) Vtol aircraft construction
US2475786A (en) Airship
US3605672A (en) Directional control apparatus
GB996103A (en) Jet propulsion drive for ships
RU2582505C1 (en) Hovercraft with water-jet propulsor
US2738147A (en) Means for turning and braking jet propelled aircraft
US5765776A (en) Omnidirectional and controllable wing using fluid ejection
US20020130220A1 (en) Airships having simplied construction and improved maneuverability
CN108248809B (en) Stratosphere dynamic balloon
US3063394A (en) Control system for submarine vessel
US3149600A (en) Integrated propulsion and control system for hydrofoil craft
US3807661A (en) Balloon assisted aircraft
CN114644112B (en) Water-air dual-purpose unmanned aerial vehicle
US3196822A (en) Device for permitting deck landings on an aircraft-carrier in misty or foggy weather