GB2045180A - Thrusters for airship control - Google Patents
Thrusters for airship controlInfo
- Publication number
- GB2045180A GB2045180A GB8019749A GB8019749A GB2045180A GB 2045180 A GB2045180 A GB 2045180A GB 8019749 A GB8019749 A GB 8019749A GB 8019749 A GB8019749 A GB 8019749A GB 2045180 A GB2045180 A GB 2045180A
- Authority
- GB
- United Kingdom
- Prior art keywords
- airship
- thrusters
- control
- contra
- bow
- 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.)
- Granted
Links
Classifications
-
- 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
- B64B1/24—Arrangement of propulsion plant
- B64B1/26—Arrangement of propulsion plant housed in ducts
-
- 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
- B64B1/36—Arrangement of jet reaction apparatus for propulsion or directional control
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Toys (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
Abstract
The object of this invention is to provide thruster control for an airship. The use of thrusters (12, 14, 16, 18, 20, 22, 24, 26) at the bow and stem of an airship for control of the direction, attitude, and orientation of such an airship is described. The thruster utilizes an electric motor (50) or a gas turbine (160, 162) for power. In the electric motor (50) embodiment, the motor (50) utilizes two contra-rotating rotors (110, 112) which each drive a separate and contra-rotating propeller (132, 134) to generate the controlling jet of air. Thrusters (12, 14, 16, 18, 20, 22, 24, 26) are arranged in pairs at the top, bottom, and each side of the bow and stem of the airship. Lifting thrusters (152, 154) directed downwardly and located above the longitudinal extent of the hull are provided to augment the static lift capability of the airship when under heavy load.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US95278378A | 1978-10-19 | 1978-10-19 |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2045180A true GB2045180A (en) | 1980-10-29 |
GB2045180B GB2045180B (en) | 1983-03-09 |
Family
ID=25493233
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8019749A Expired GB2045180B (en) | 1978-10-19 | 1979-10-18 | Thrusters for airship control |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP0020569A4 (en) |
CA (1) | CA1143352A (en) |
GB (1) | GB2045180B (en) |
SE (1) | SE8004563L (en) |
WO (1) | WO1980000825A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2143186A (en) * | 1983-07-11 | 1985-02-06 | Secr Defence | Fuselage side force control |
GB2346593A (en) * | 1999-02-09 | 2000-08-16 | Airship Tech Serv Ltd | Airship bow thruster apparatus |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2251834B (en) * | 1983-02-22 | 1992-12-16 | George Alexander Tarrant | Guided missiles |
DE19745893A1 (en) | 1997-01-16 | 1999-04-22 | Fritz Peter Prof Dr Schaefer | Cruise airship with anchor device and helium liquefaction system |
DE10011319C2 (en) * | 2000-02-23 | 2002-01-24 | Cargolifter Ag | Airship and method for pitch angle trimming of airships |
RU201900U1 (en) * | 2019-04-23 | 2021-01-21 | Юрий Степанович Бойко | Electric airship |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1457024A (en) * | 1920-06-29 | 1923-05-29 | Henry M Franzen | Control for aircraft and the like |
US2214656A (en) * | 1938-01-20 | 1940-09-10 | Henry C Briggs | Mechanism for improving the dirigibility of ships, submarines, and aircraft |
US2494368A (en) * | 1947-04-30 | 1950-01-10 | Curtiss Wright Corp | Arrangement of aircraft propulsion and radio viewing components |
US3346216A (en) * | 1964-07-23 | 1967-10-10 | Desmarteau Paul | Airship |
DE1248503B (en) * | 1966-11-22 | 1967-08-24 | Licentia Gmbh | Electric drive arrangement for two coaxial, opposing ship propellers |
DE2043916A1 (en) * | 1970-09-04 | 1972-03-09 | Veress, Gerrit von, 8000 München | Engine for rigid airships |
DE2548991A1 (en) * | 1975-11-03 | 1977-05-05 | Schmidt Klieber Alexander | Steering control for airship - with vertical and horizontal thruster duct at bows contg. airscrews for stationary manoeuvring |
-
1979
- 1979-06-22 CA CA000330385A patent/CA1143352A/en not_active Expired
- 1979-10-18 WO PCT/US1979/000860 patent/WO1980000825A1/en unknown
- 1979-10-18 GB GB8019749A patent/GB2045180B/en not_active Expired
-
1980
- 1980-05-07 EP EP19790901500 patent/EP0020569A4/en not_active Withdrawn
- 1980-06-19 SE SE8004563A patent/SE8004563L/en not_active Application Discontinuation
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2143186A (en) * | 1983-07-11 | 1985-02-06 | Secr Defence | Fuselage side force control |
GB2346593A (en) * | 1999-02-09 | 2000-08-16 | Airship Tech Serv Ltd | Airship bow thruster apparatus |
GB2346593B (en) * | 1999-02-09 | 2003-01-08 | Airship Tech Serv Ltd | Airship bow thruster apparatus |
Also Published As
Publication number | Publication date |
---|---|
EP0020569A1 (en) | 1981-01-07 |
CA1143352A (en) | 1983-03-22 |
GB2045180B (en) | 1983-03-09 |
WO1980000825A1 (en) | 1980-05-01 |
EP0020569A4 (en) | 1981-03-24 |
SE8004563L (en) | 1980-06-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PE20 | Patent expired after termination of 20 years |
Effective date: 19991017 |