WO1988000906A1 - Airship handling system - Google Patents
Airship handling system Download PDFInfo
- Publication number
- WO1988000906A1 WO1988000906A1 PCT/GB1987/000534 GB8700534W WO8800906A1 WO 1988000906 A1 WO1988000906 A1 WO 1988000906A1 GB 8700534 W GB8700534 W GB 8700534W WO 8800906 A1 WO8800906 A1 WO 8800906A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- platform
- airship
- incorporated
- module
- track
- Prior art date
Links
- 239000000725 suspension Substances 0.000 claims description 5
- 238000009434 installation Methods 0.000 claims 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 1
- 230000007935 neutral effect Effects 0.000 description 1
- 230000008707 rearrangement Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/12—Ground or aircraft-carrier-deck installations for anchoring aircraft
- B64F1/14—Towers or masts for mooring airships or balloons
Definitions
- This invention relates to the ground handling of an airship at an operating base.
- Airships generally operate in a condition of either neutral or negative buoyancy.
- a neutrally buoyant airship can hover and hence can operate from a small ground area, but time is lost in manoeuvring at airspeeds too low for precise aerodynamic control in unsteady conditions, and in decelerating to and accelerating from the hovering mode.
- a negatively buoyant or 'heavy' airship cannot hover but must take off and land with an extended ground run which greatly increases the base area requirement, although control problems are less severe. If passengers are to be carried using either mode of operation, a further time penalty is inherent in disembarkation and embarkation, particularly where the mooring facilities are such that a 'one in, one out' sequence must be used to prevent the airship from rising. These factors may not be significant when airship applications permit relatively relaxed scheduling, but become critical if the airship is to be used for high-density scheduled passenger movement.
- This invention is intended to facilitate rapid passenger flow through an airship terminal using a small ground area and permitting operation over an adequate range of weather conditions.
- the invention provides an operating platform which can be rotated upon a circular track for the purpose of aligning it with the wind direction and may incorporate additional articulation to raise, lower or tilt the platform for particular modes of operation and which also incorporates facilities for arresting, mooring and launching a suitably-fitted airship.
- the platform further incorporates means of handling a loaded passenger module such that the module may be detached from or attached to the moored airship and transferred to and from a suitable position for the disembarkation and embarkation of passengers independently of the position of the airship.
- FIG. 1 shows an airship suitably equipped for use with this system:
- Figure 2 shows in simplified form ah elevation of the platform:
- Figure 3 shows in simplified form a partial plan of the platform.
- the airship 1 alights upon and takes off from a platform 2 which is mounted upon a circular track 3 so that it may be rotated by a suitable power unit about a vertical axis 4 and hence aligned with the wind direction.
- the airship carries passengers or cargo in a module 5 which may be readily attached to or detached from the airship body, and is further fitted with a retractable arrester hook 6.
- a sunken rail 7 in the surface of the platform guides an arrester link 8 attached by cable to an arrester unit 9, and an accelerator link 10 attached by cable to an accelerator unit 11. Both links are attached to carriages running in the rail 7 so that upward loading may be resisted.
- Two further sunken rails 12 guide a mooring carriage 13 which carries four retractable mooring stays 14 and i ⁇ *corporates a mooring link 15 running in the rail 7.
- the mooring carriage may be connected to the arrester link 8 or may be moved separately by a separate power unit which is not shown.
- a forward module lift 16 and an.aft module lift 17 transfer loaded modules 5 between the airship and the module rails 18, by means of which a suspended module 21 may be moved within the body of the platform using the powered forward module shunt 19 or the aft module shunt 20, running on the same suspension rails 18.
- a third module lift 22 transfers loaded modules between the rails 18 and ground level, rotating the module in transit to align its axis either with the platform axis or with that of the ground reception unit through which passengers or cargo enter or leave the module.
- the operational sequence commences with the platform aligned with the wind and the airship approaching into wind with the arrester hook 6 extended to engage a cable frame (not shown) and hence the arrester link 8.
- the arrester unit 9 thereby retards the airship so that it comes to rest over the forwardmodule lift 16, final registration being adjusted through movable wheel pads which are not shown.
- the arrester link 8 is connected to the mooring link 15 and the mooring stays 14 are extended and coupled to the body of the airship to hold it in position.
- the incoming module is now detached from the airship and transferred by the forward module lift 16 to the suspension rails 18, and the arrester unit 9 is activated as a winch to draw the airship back above the aft module lift 17, drawing with it the accelerator link 10 which has meanwhile been attached to the airship body.
- the aft module lift now transfers the outgoing module from the suspension rails 18 to the airship.
- arrester link 8 and the mooring stays 14 are disconnected from the airship which then takes off under the combined impulse of its own power unit and the pull of the accelerator link 10, maintained by the accelerator unit 11.
- the outgoing module after loading at ground level, was raised by the module lift 22 to engage the suspension rails and was then moved by the aft module shunt 20 into a suitable position to await elevation to the airship.
- the incoming module was then moved by the forward module shunt 19 to the module lift 22 and lowered to ground level for unloading.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
- Auxiliary Methods And Devices For Loading And Unloading (AREA)
- Ship Loading And Unloading (AREA)
Abstract
A platform (2) rests upon a circular track (3) such that the platform may be aligned with the wind to facilitate handling of a suitably-equipped airship (1). The platform incorporates arrester gear (8, 9) to bring the airship to rest at a specified point, a mooring system (13, 14, 15) to hold the airship in position for subsequent handling operations, lifts and transfer track (16, 17, 18), to remove the loaded module (5) from the airship and repalce it by a second loaded module, a further lift (22) to transfer modules between the platform and a ground level station for loading and unloading, and an accelerator gear (10, 11) to accelerate the airship to take-off speed within the available length of platform.
Description
AIRSHIP HANDLING SYSTEM This invention relates to the ground handling of an airship at an operating base.
Airships generally operate in a condition of either neutral or negative buoyancy. A neutrally buoyant airship can hover and hence can operate from a small ground area, but time is lost in manoeuvring at airspeeds too low for precise aerodynamic control in unsteady conditions, and in decelerating to and accelerating from the hovering mode. A negatively buoyant or 'heavy' airship cannot hover but must take off and land with an extended ground run which greatly increases the base area requirement, although control problems are less severe. If passengers are to be carried using either mode of operation, a further time penalty is inherent in disembarkation and embarkation, particularly where the mooring facilities are such that a 'one in, one out' sequence must be used to prevent the airship from rising. These factors may not be significant when airship applications permit relatively relaxed scheduling, but become critical if the airship is to be used for high-density scheduled passenger movement.
This invention is intended to facilitate rapid passenger flow through an airship terminal using a small ground area and permitting operation over an adequate range of weather conditions.
The invention provides an operating platform which can be rotated upon a circular track for the purpose of aligning it with the wind direction and may incorporate additional articulation to raise, lower or tilt the platform for particular modes of operation and which also incorporates facilities for arresting, mooring and launching a suitably-fitted airship. The platform further incorporates means of handling a loaded passenger module such that the module may be detached from or attached to the moored airship and transferred to and from a suitable position for the disembarkation and embarkation of passengers independently of the position of the airship.
A specific embodiment of the invention will now be described by way of example with reference to the accompanying drawing in which:- Figure 1 shows an airship suitably equipped for use with this system: Figure 2 shows in simplified form ah elevation of the platform: Figure 3 shows in simplified form a partial plan of the platform.
The airship 1 alights upon and takes off from a platform 2 which is mounted upon a circular track 3 so that it may be rotated by a suitable power unit about a vertical axis 4 and hence aligned with the wind direction.
The airship carries passengers or cargo in a module 5 which may be readily attached to or detached from the airship body, and is further fitted with a retractable arrester hook 6.
A sunken rail 7 in the surface of the platform guides an arrester link 8 attached by cable to an arrester unit 9, and an accelerator link 10 attached by cable to an accelerator unit 11. Both links are attached to carriages running in the rail 7 so that upward loading may be resisted.
Two further sunken rails 12 guide a mooring carriage 13 which carries four retractable mooring stays 14 and iή*corporates a mooring link 15 running in the rail 7. The mooring carriage may be connected to the arrester link 8 or may be moved separately by a separate power unit which is not shown.
A forward module lift 16 and an.aft module lift 17 transfer loaded modules 5 between the airship and the module rails 18, by means of which a suspended module 21 may be moved within the body of the platform using the powered forward module shunt 19 or the aft module shunt 20, running on the same suspension rails 18.
A third module lift 22 transfers loaded modules between the rails 18 and ground level, rotating the module in transit to align its axis either with the platform axis or with that of the ground reception unit through which passengers or cargo enter or leave the module.
The operational sequence commences with the platform aligned with the wind and the airship approaching into wind with the arrester hook 6 extended to engage a cable frame (not shown) and hence the arrester link 8. The arrester unit 9 thereby retards the airship so that it comes to rest over the forwardmodule lift 16, final registration being adjusted through movable wheel pads which are not shown. In this position the arrester link 8 is connected to the mooring link 15 and the mooring stays 14 are extended and coupled to the body of the airship to hold it in position.
The incoming module is now detached from the airship and transferred by the forward module lift 16 to the suspension rails 18, and the arrester unit 9 is activated as a winch to draw the airship back above the aft
module lift 17, drawing with it the accelerator link 10 which has meanwhile been attached to the airship body.
The aft module lift now transfers the outgoing module from the suspension rails 18 to the airship.
Finally the arrester link 8 and the mooring stays 14 are disconnected from the airship which then takes off under the combined impulse of its own power unit and the pull of the accelerator link 10, maintained by the accelerator unit 11.
During these airship movements on the platform, the outgoing module, after loading at ground level, was raised by the module lift 22 to engage the suspension rails and was then moved by the aft module shunt 20 into a suitable position to await elevation to the airship. The incoming module was then moved by the forward module shunt 19 to the module lift 22 and lowered to ground level for unloading.
After take-off all the units decribed are rearranged to receive the next incoming airship, the last incoming module now being serviced as necessary and presented as the next outgoing module.
Alternative arrangements of the system may incorporate:
- a retractable mast or mooring cables attachable to the nose of the airship, in place of the forward pair of the mooring stays 14:
- a single module lift to handle both incoming and outgoing modules, in place of the two module lifts 16 and 17, with an appropriate rearrangement of the handling sequence.
Claims
1 A platform on which an airship may alight and exchange its load, and from which the airship may take off, mounted on a circular track such that the platform may be turned to align its axis with the wind.
2 A platform as claimed in Claim 1, where in incorporated an arrester system such that a suitably equipped airship may be brought to rest on the platform in a shorter distance than would otherwise be normally practicable.
3 A platform as claimed in Claim 1 or Claim 2, wherein is incorporated a mooring system such that whilst moored the airship may have load added or removed and may be moved along the axis of the platform without using its own power.
4 A platform as claimed in Claim 1 or Claim 2 or Claim 3, wherein is incorporated an accelerator system such that a suitably equipped airship may be brought to take-off speed on the platform in a shorter distance than would otherwise be normally practicable.
5 A platform as claimed in Claim 1 or Claim 2 or Claim 3 of Claim 4, wherein is incorporated a suspension track with lifts such that a module containing passengers or cargo may be transferred between a suitably equipped airship and an appropriate exchange point at which passengers or cargo may be loaded and unloaded independently of the position of the airship.
6 A platform as claimed in Claim 1 or Claim 2 or Claim 3 or Claim 4 or Claim 5 wherein as claimed the circular support track on which the platform rotates is mounted upon hydraulic actuators such that the platform may be raised and lowered vertically to facilitate the adherence of the airship to an appropriate flight path on the landing approach.
7 A platform as claimed in Claim 1 or Claim 2 or Claim 3 or Claim 4 of Claim 5 of Claim 6 wherein the circular support track on which the platform rotates is mounted upon actuators which may operate either collectively in order to raise or lower the platform vertically or differentially in order to tilt the platform about the longitudinal and lateral axes for purposes of facilitating water borne installation or on a vessel.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE8787904909T DE3770945D1 (en) | 1986-07-28 | 1987-07-28 | DEVICE FOR THE TREATMENT OF AIRSHIPS. |
AT87904909T ATE64575T1 (en) | 1986-07-28 | 1987-07-28 | DEVICE FOR THE TREATMENT OF AIRSHIPS. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8618319 | 1986-07-28 | ||
GB868618319A GB8618319D0 (en) | 1986-07-28 | 1986-07-28 | Airship handling system |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1988000906A1 true WO1988000906A1 (en) | 1988-02-11 |
Family
ID=10601779
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/GB1987/000534 WO1988000906A1 (en) | 1986-07-28 | 1987-07-28 | Airship handling system |
Country Status (6)
Country | Link |
---|---|
US (1) | US5143323A (en) |
EP (1) | EP0315634B1 (en) |
JP (1) | JPH01503772A (en) |
AU (1) | AU7757887A (en) |
GB (2) | GB8618319D0 (en) |
WO (1) | WO1988000906A1 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0728100A1 (en) * | 1993-11-08 | 1996-08-28 | Lockheed Martin Corporation | A cargo compartment for a lighter-than-air vehicle |
CN104986352A (en) * | 2015-07-10 | 2015-10-21 | 常州市科宏电子电器有限公司 | Lifting mechanism and lifting method for aircraft undercarriage |
WO2022061003A1 (en) * | 2020-09-16 | 2022-03-24 | Galaxy Unmanned Systems LLC | Unmanned airships, aerostats, and hybrid airship-aerostat systems and methods thereof |
USD1002870S1 (en) | 2021-09-16 | 2023-10-24 | Galaxy Unmanned Systems LLC | Hybrid airship-aerostat |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB8618319D0 (en) * | 1986-07-28 | 1986-09-03 | Husain F | Airship handling system |
US5346162A (en) * | 1993-11-08 | 1994-09-13 | Lockheed Corporation | Cargo compartment for a lighter-than-air vehicle |
US5431359A (en) * | 1994-04-04 | 1995-07-11 | Lockheed Corporation | Docking system for a lighter-than-air vehicle |
US5497962A (en) * | 1994-10-11 | 1996-03-12 | Lockheed Corporation | Mooring tower assembly for a lighter-than-air vehicle |
DE19924468A1 (en) * | 1999-05-28 | 2000-11-30 | Uti Holding & Man Ag | Weaning station |
JP2004249954A (en) * | 2003-02-21 | 2004-09-09 | Daigo Fukumoto | Unit type multiple-purpose airship |
US7464650B2 (en) * | 2006-03-17 | 2008-12-16 | Lockheed Martin Corporation | Ground handling system for an airship |
DE102008023698B4 (en) * | 2008-05-09 | 2010-09-23 | Jan Binnebesel | Ground-based device for take-off, landing and taxiing of aircraft |
DE202008010945U1 (en) | 2008-08-16 | 2008-10-23 | Glinberg, Valeriy | Hybrid freight transport system - "rail airship" |
FR3106815B1 (en) * | 2020-01-31 | 2023-08-04 | Flying Whales | Device for controlling the ground clearance of an airship and docking station for an airship incorporating such a device |
CN111516892A (en) * | 2020-05-08 | 2020-08-11 | 中国人民解放军63660部队 | Method for transferring and flying large airship by multi-task rail type combined platform |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR432689A (en) * | 1911-07-17 | 1911-12-12 | Mathias Portz | Device for anchoring airships |
DE498253C (en) * | 1926-09-18 | 1930-05-20 | E H Otto Krell Dr Ing | Equipment for the recovery of airships in fixed halls |
US1867591A (en) * | 1930-11-29 | 1932-07-19 | August S Pranke | Dirigible air dock |
US3605935A (en) * | 1970-01-06 | 1971-09-20 | Richard H Gilbert | Air surface rapid transit vehicle |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1807710A (en) * | 1931-06-02 | schleicher | ||
US1351931A (en) * | 1920-09-07 | ullmann | ||
US1478747A (en) * | 1923-06-14 | 1923-12-25 | Floyd H Kinyoun | Airplane starting and landing device |
GB222310A (en) * | 1923-09-24 | 1924-10-02 | Paul Uhlendahl | Improvements in landing and housing arrangements for airships |
US1560775A (en) * | 1924-01-30 | 1925-11-10 | Mary A Kenney | Aerial landing and launching apparatus |
GB302945A (en) * | 1926-10-05 | 1927-12-23 | Peter Regan | Apparatus for launching aircraft |
GB299698A (en) * | 1927-10-29 | 1929-04-25 | Mary Ann Kenney | Improvements in aeronautical landing and launching apparatus |
GB310104A (en) * | 1928-10-30 | 1929-04-25 | Airship Guarantee Co Ltd | Improvements in or relating to means for berthing airships |
US1854494A (en) * | 1929-09-19 | 1932-04-19 | Nicolas F Thommes | Landing and taking-off mechanism |
US1845229A (en) * | 1930-05-27 | 1932-02-16 | Bradshaw Alfred | Landing gear for dirigible airships |
US1988187A (en) * | 1932-06-30 | 1935-01-15 | Charles J Carlotti | Hangar |
GB413773A (en) * | 1933-02-07 | 1934-07-26 | Charles Frobisher | Improvements in and relating to elevated centrally pivoted rotating aerodromes or airport landing grounds |
US3972493A (en) * | 1975-01-29 | 1976-08-03 | Milne William G | Docking device for a dirigible |
CA1139287A (en) * | 1979-08-02 | 1983-01-11 | Tibor Laky | Mooring system |
GB8618319D0 (en) * | 1986-07-28 | 1986-09-03 | Husain F | Airship handling system |
-
1986
- 1986-07-28 GB GB868618319A patent/GB8618319D0/en active Pending
-
1987
- 1987-07-28 GB GB08717891A patent/GB2198399A/en not_active Withdrawn
- 1987-07-28 EP EP87904909A patent/EP0315634B1/en not_active Expired
- 1987-07-28 WO PCT/GB1987/000534 patent/WO1988000906A1/en active IP Right Grant
- 1987-07-28 JP JP62504689A patent/JPH01503772A/en active Pending
- 1987-07-28 AU AU77578/87A patent/AU7757887A/en not_active Abandoned
-
1990
- 1990-06-18 US US07/539,608 patent/US5143323A/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR432689A (en) * | 1911-07-17 | 1911-12-12 | Mathias Portz | Device for anchoring airships |
DE498253C (en) * | 1926-09-18 | 1930-05-20 | E H Otto Krell Dr Ing | Equipment for the recovery of airships in fixed halls |
US1867591A (en) * | 1930-11-29 | 1932-07-19 | August S Pranke | Dirigible air dock |
US3605935A (en) * | 1970-01-06 | 1971-09-20 | Richard H Gilbert | Air surface rapid transit vehicle |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0728100A1 (en) * | 1993-11-08 | 1996-08-28 | Lockheed Martin Corporation | A cargo compartment for a lighter-than-air vehicle |
EP0728100A4 (en) * | 1993-11-08 | 1997-09-03 | Lockheed Corp | A cargo compartment for a lighter-than-air vehicle |
CN104986352A (en) * | 2015-07-10 | 2015-10-21 | 常州市科宏电子电器有限公司 | Lifting mechanism and lifting method for aircraft undercarriage |
CN104986352B (en) * | 2015-07-10 | 2017-04-26 | 常州市科宏电子电器有限公司 | Lifting mechanism and lifting method for aircraft undercarriage |
WO2022061003A1 (en) * | 2020-09-16 | 2022-03-24 | Galaxy Unmanned Systems LLC | Unmanned airships, aerostats, and hybrid airship-aerostat systems and methods thereof |
US11685500B2 (en) | 2020-09-16 | 2023-06-27 | Galaxy Unmanned Systems LLC | Unmanned airships, aerostats, and hybrid airship-aerostat systems and methods thereof |
USD1002870S1 (en) | 2021-09-16 | 2023-10-24 | Galaxy Unmanned Systems LLC | Hybrid airship-aerostat |
Also Published As
Publication number | Publication date |
---|---|
GB8717891D0 (en) | 1987-09-03 |
GB8618319D0 (en) | 1986-09-03 |
US5143323A (en) | 1992-09-01 |
EP0315634A1 (en) | 1989-05-17 |
EP0315634B1 (en) | 1991-06-19 |
AU7757887A (en) | 1988-02-24 |
JPH01503772A (en) | 1989-12-21 |
GB2198399A (en) | 1988-06-15 |
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