US1770675A - Mooring device - Google Patents
Mooring device Download PDFInfo
- Publication number
- US1770675A US1770675A US157054A US15705426A US1770675A US 1770675 A US1770675 A US 1770675A US 157054 A US157054 A US 157054A US 15705426 A US15705426 A US 15705426A US 1770675 A US1770675 A US 1770675A
- Authority
- US
- United States
- Prior art keywords
- airship
- platform
- mooring
- mast
- shelter
- 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.)
- Expired - Lifetime
Links
- 238000000034 method Methods 0.000 description 6
- 238000013459 approach Methods 0.000 description 5
- 230000008569 process Effects 0.000 description 4
- 238000004873 anchoring Methods 0.000 description 3
- 239000004744 fabric Substances 0.000 description 3
- 238000004804 winding Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 230000002542 deteriorative effect Effects 0.000 description 2
- 238000005286 illumination Methods 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 230000008439 repair process Effects 0.000 description 2
- 230000002441 reversible effect Effects 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 240000007839 Kleinhovia hospita Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
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
- Fig. 1 is a perspective .view taken from slightly above one form of theinvention. showing an airship about. to be moored thereto: 7
- FIG. 2 is another view of the invention as showii in Fig. 1, tae View being taken from the astern of the airship, which is in the same position as in 1;
- Fig. 3 is a view taken from the same point as in Fig. 2 but with the airship moored;
- Fig. 4 is a view of a modified form ofthe invention, taken from approximately. the same viewpoint as areFigs. 2 and 3, but without the airship;
- Fig. 5 is a PEISPEClDlVGVlQW, with parts cut away, of the upright member or mooring mast of Figs. 1 toi, inclusive; 1
- Fi is a perspective View of another o the invention, showing an airship iorm 1 in t e initial stages of mooring;
- -ig. 7 is a view of the mooring device ow 'n Fig. 6 taken from the astern of the ,which is moored;
- I Fig. 8 is a perspective view slightly from above of a further form ofthe: lnvention,
- Fig. 9 is a perspective view taken slightly from above showing a still further form of the invention.
- the airship is preferably first made fast to an upright member or special mooring mast that is adapted to raise or lower the airship while attached to a movable fitting on said mast. WVhen lowered, the shelter for the airship is placed about the airship in one of several ways, and so avoids the dangers of attempting to run the airship into a shelter, especially with wind con'di tions not altogether favorable. In this manner, although the airship maybe made fast to the mooring mast under turbulent weather conditions, there is no dange of its striking the shelter, because the latter is opened up wide and. hence entirely out of the way. As the airship is lowered, the shelter may be used as a windbreak to ameliorate air conditions about the airship.
- the upright member or special mooring mast, 11 is directly upwind, and the airship approaches it along the platform 10, and hence, directly into the wind.
- the mast cable, 15, is already in position as shown, lying on the platform 10 in a position convenient for quick use.
- the landing crew on the platform 10 secure the end of the nose cable 2 and fasten itto the endof the mast cable 15. This done, the cables and 2 are wound in through the mooring fixture 51, by means such as shown in Fig. 5, and the airship 1 is brought slowly up to the mooring fixture 51; in the process, the motors of the airship 1 may be reversed or inoperative, or under some wind conditions, still helping to propel the airship forward.
- the airship When the airship is clear up to the mooring fixture 51, it is secured there, preferably with means for quickly letting go in case of emergency, and the mooring fixture and airship are lowered toward the platform 10.
- the auxiliary cables, 3, on the airship are secured by the crew on the platform 10, and may be held manually, or preferably are passed through the hatches, such as 17, to power-operated winding drums or winches, (see Figs. 2, 3, 4, and 7).
- ⁇ Vhen these are secured so that the airship may be held from lateral swinging, the shelte'r walls 12 are raised by power-operated means, which may act on the gear sectors 32 20 (Fig.
- Pro- 35 t'ection from weather is not only beneficial thus defor the airship and the load, including passengers alighting therefrom or boarding it, but also, it permits the thorough inspection of all parts of the airship and the making of minor repairs during the lay-over between flights.
- the upright member or special mooring mast, 11, is preferably supported or strengthened by auxiliary members such as the slantingbrace 11 and the necessary tie members.
- the mast 11 is mounted at one end of the platform 10, which in turn is pivoted about a point in about the center of its length, and mounted on wheels, 14, which run on the series of concentric circular tracks, 16.
- the whole sweeps out an area not much greater than the circle whose diameter is the length of the platform 10, which latter is determined by the length of the longest airship to be accommodated.
- Platform sections are preferably driven about their respectivetracks by electric motors, and it is a simple matter for one skilled in the art to proportion the driving forces and controlling devices therefor in such a manner that relatively small intersection. stresses will have to be cared for by the couplings between sections.
- the fact'that the whole structure is normally kept aligned with the wind direction makes it possible to reduce wind forces on it, and thus to make a lighter and less expensive structure than would be required in a fixed hangar.
- the platform lO may have to be one unit.
- the upright member 11 will be made sufficiently tall so that the airship may fly over obstacles in the imu'iediate neighborhood of the landing field and still be on the level of the top of upright 11, where the airship is first brought to the mooring fixture 51.
- the numeral 19 therefore may represent the ground or the top of a building or other suit able place.
- Fig. 2 shows the mooring process from the viewpoint of an observer following behind the airship 1.
- the nose cable 2 is seen dragging on the platform 10, ready to be picked up by the landing crew.
- the auxiliary cables, 3, are seen still out of reach.
- the location of the series of winches, 20, is seen below the landing stage of the platform 10,
- the completed mooring operation is shown in Fig.
- the shelter walls, 12, have closed over the airship 1, which is secured by the auxiliary cables 3 and winches (and such other means as my seem desirable) to platform 10, and it is convenient for the transfer of passengers, freight, supplies and the like. It will be noted that in the final pulling down of the airship 1 to platform 10, it is desirable to back the former away from the mooring fixture 51, and to allow ample slack on nose cable 2. The airship is then free to swing laterally about the auxiliary cables, 3, without inducing severe stresses at the nose.
- Fig. i shows a form of mooring device very similar to that of Figs. 1, 2 and 3, the prinipal difference being that the platform has upwardly extending wallsofa fixed nature along its sides, and that the horizontal hinges for the roof members 42 are at a height comparable with the height of the airship 1 hinges Screw-jack means, l i, are here shown for manipulating the shelter roof members 42, though any convenient means may be used for'this purpose.
- the mooring fixture 51 is here shown in what is normally its lowest position, such that the airship cars would be close to the platform 40.
- Fig. 5 shows a oetail of a preferred form of mooring fixture, 51, and the elements of the special mooring mast, 11, which co-operate with it.
- the upright member 11 is surmounted by a cap, 53, which serves to hold pulley 52 and permit it to revolve about a substantially horizontal axis.
- Cable passes over pulley 52,-being secured atone end to the top of carriage 5 1, the other passing down and around winch drum 57 thence up again to a point of attachment at the bottom of carriage 5%.
- motor 58 through the non-reversible gear'members, 57,- can drive carriage 5 t'up ordown, and when'at rest, carriage 5iwill not be able to move up.
- the mooring fixture 51 is preferably conic in shape, ofsizeadapted to permit the entry of a member on the nose 0 the airship,which may be a ball-like structure on an extending arm, and this fixture 51 is preferably universally mounted as by means of the gimbal ring 56.
- One of the gimbal ring pivots (preferably the horizontal pivot) is extended clear through both faces of the frame of the carriage 54, and is provided with a gear, 55*, which meshes with the pinion on the shaft of motor 55.
- Mounted on this throughpivot is the winding drum 55", which serves to pull in or to let out the mast cable 15 as required in the mooring of the airship.
- FIG. 6 A form of the invention which. is particularly suited to places where extent of area is not of such importance as would be the case near large centers of population, is shown in Fig. 6.
- the mooring mast 61 is used as the pivot point of the system, the other major elements being adapted to revolve about it. Since the length of the platform 60 is determined by the length of the longest airship to be accommodated, the system will sweep out an area a little larger than the circle whose diameter is twice the length of platform 60; hence, this form of mooring device will require roughly four times the ground area of the type shown in Figs. 1, 2 and 3. On the other hand, the structure would probably not be as costly as the former.
- the mooring mast 61 is built to withstand thrust in any direction, and is preferably approximately, circular in section to permit of the application of revolvable holding bands 63.
- At the top of mooring mast 61 and mounted on two of the revolvable holding bands 63 is mounted the, T-shaped platform 69.
- the upright member 11 is secured to and extends slightly above'the middle or shorter end of platform 69, thus permitting the mooring fixture 51 to come somewhat abovetlie level of said platform. Arailing may be provided around platform 69 for the safety and convenience of. the crew stationed there.
- Bands 63, platform 69 and upright member 11 are caused to revolve as a unit about mooring mast 61, preferably under control of an ly higher level than platform 69.
- the airship 1 Onoe brought up to the mooring fixture 51, the airship 1 is lowered with said mooring fixture down the upright member 11 by means such as that shown in Fig. or the equivalent, coming into the shelter of the open shelter walls 62.
- the platform is revolved about mooring mast 61, being borne by wheels, 64, on the circular rails 67 and 16, until in alignment with the wind and airship, approximately, and when in reach of the landing crew, the auxiliary cables 3 on the airship 1 are caught and when weather conditions permit are passed through hatches, 17 to the Winches 20, below the landing stage, which winches serve to draw the airship down and hold it in place.
- the shelter walls 62 are fgradually clemd about it, giving progressive y greater shelter and making it progressively safer to bring the airship closer to the landing platform 60.
- the shelter walls 62 are completely closed about the airship 1, it will be safe to bring the airshi 3 down to the landing stage or top surface 0 platform 60, but in this final operation it is desirable to back away from mooring fixture 51, leaving a clear space between the nose of the airship 1 and the fixture 51, and allowing ample slack in the nose cable 2; this permits the airship a certain amount of lateral swing about the auxiliary cables 3 without causing severe stresses at the nose of the airship.
- Other attachments may be applied to the airship as required in the final or other stage of the mooring operation.
- end shelter is prefera'bl provided by curtains which are prefera ly secured to the slanting brace membeis, 11", of the special mooring lnast and to the near ends of the shelter walls 12 after the latter have closed over the airship 1, in
- a pluralityof frames are movably attached to the moorlng mast 61 at their tops and are mounted on wheels 68 at their'bottoms and are thus adapted to revolve about the mooring mast 61 as an axis and be supported and guided at their bottoms by the inner circular rail 67.
- Between frames 65 is normally provided a liable sheathing, 66, such as waterproofed a c, which is loose enough in the figure to unit of revolving shelter walls 62 (to v9 ch said sheathing is also attached) to close about the airship and when closed to stretch the sheathing 66 to a reasonable deof tightness.
- Fig. 7 shows the airship 1 moored and sheltered by the shelter walls 62, which have closed about it.
- This stern view shows the normal relative positions of shelter walls (32 and platform 60, and it will be noted that in this position it is possible and desirable to link these elements together temporarily, so that in swinging with the wind, the who e may move as a unit.
- One of the circular tracks, 16, is shown resting on the ground 19, and supporting the shelter wall wheels, 14, and the platform wheels, 64.
- the moored position of the auxiliary cables 3 is also shown. held by the winches, 20.
- the platform 60 may be eliminated, and the airship 1 be brought right to the ground 19 for loading or unloading.
- Man-power may be used for pulling the airship down and holding it; sand-bags may be hung on for holding down after landing, or water ballast pumped to the tanks of the airship itself for this purpose; electric or other powerdriven tractors may be utilized for pulling and holding purposes; and other means may be substituted for the functions performed by platform 60 with a saving in first cost.
- the convenience of operation with platform 60, and the saving of time in landing an airship together with the reduction in handling personnel would tend to make the additional cost of platform 60 a good investment.
- a platform such as 60
- means may readily be adapted to the winches 20, such that the upward pull on each of the auxiliary cables 3 may be measured and the excess buoyancy of the airship adjusted properly in amount and in distribution, so that the airship, on being released, will rise at a predetermined rate and on a level keel.
- Provision' or friends of the passengers, visitors, etc. may profitably be made in the spaces within the shelter walls 62, thus keeping them separated from the landing platform 60 until it is desired to let them go onto the latter; whereas during the mooring process such locations would provide excellent views of the procedure while keeping the spectators entirely out of the way.
- FIGs. 8 and 9 show perspective views, slightly from above, of two forms of the device in which the shelter element is independent of the mooring mast.
- the airship, 1 may be moored to a mast, 81, which preferably is provided with a lowerable mooring fixture such as 51 of previous designs.
- the airship 1 When moored to the mast the airship 1 is inclosed by the shelter elements 82 (in Fig. 8), which are adapted to approach. from the sides, independently, being mounted on a series of wheeled trucks, 8%, which may be provided with motive power and interlinked steering arrangements.
- the airship, 1, is provided with shelter after being moored to the mast 81, by a light hanger 92 which is run over the airship from the end, and would preferably inclose the mast 81 as well.
- This hanger 92 is preferably made somewhat collapsible and is shown constructed of the arch members, 95, and brace members, 95, with treated fabric between and at the end 93.
- N heels, 94 provide easy means of moving the hangar to its position and are preferably power-driven individually.
- Brace members 95 are articulated so that they may be bent as shown in the three sections near the end 93 and so bring the corresponding arc-hes 95 closer together and reducing the length of the structure for convenience of handling. When straight, braces 95 hold the frames 95 apart and stretch the connecting fabric to the proper tightness to provide a stable and effective shelter.
- End curtains or doors may be provided for either end of any of the above mooring devices, such closing means being in standard use is not an essential part of this invention.
- any means of bringing the airship to the mooring mast fixture or attachment point which may be in use now or in the future may be considered the equivalent of nose cable 2; and any means such as standard handling ropes of airships of today or other means devised in the future may be considered the equivalent of auxiliary cables 3.
- a combined mooring mast and hangar including a platform, a mast on the platform, a nose cap anchoring member vertically ad justable on the mast and hangar wall sections hinged to the edges of the platform and adapted to be folded about a dirigible after it has been moored to the mast.
- a mooring device for dirigibles including a landing platform, a mooring mast having a fixed location relative to the platform, means for securing an airship to the platform, nose cap anchoring means vertically adjustable on the mast and folding hangar sections hinged to the edges of the platform and swingable to position to cooperatively house adirigible anchored on the platform.
- a hangar including a landing platform and wall sections pivotally connected to the edges thereof adapted to cooperatively define a housing for a dirigible anchored to the platform.
- Apparatus for anchoring and housing a dirigible including an elongated platform, a mooring mast at one end thereof and wall sections movably connected to the edges of the platform for enclosing a dirigible anchored to the mast.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Description
MO'ORING DEVICE Filed Dec. 27, 192 2 SheetS-Sheet'l' AT 'NEY FRANK SHORT Bur -5M July 15, 1930. F, SHORT 1,770,675
MOORING DEVICE Filed Dec. 27, 1926 2 Sheets-Sheet 2 luvzuro FRANK SHORT ATTORNEY Patented July 15, 1939 STATS titans FRANK SHORT, F POUGHKEEPSIE, NEW YORK Application filed December 27, 1926. Serial No. 15?,054.
liketo and from the airship. It has for further objects the protection of the airship from the deteriorating effects of sun and weather while moored, the danger of destruction from excessive winds and the constant wracking of the airship structure by wind when secured to any stationary object. It has for a further object the economy of landing space permitted by certain features of the invention, thus enabling a smaller landing field to be utilized and often thereby making it practicable to land at considerably closer proximity to large centers of population.
With these and other objects in View, I have shown in the appended drawings, described in the following specification and claimed in the claims hereto the preferred embodiment of my invention. In the drawings: V
Fig. 1 is a perspective .view taken from slightly above one form of theinvention. showing an airship about. to be moored thereto: 7
2 is another view of the invention as showii in Fig. 1, tae View being taken from the astern of the airship, which is in the same position as in 1; Fig. 3 is a view taken from the same point as in Fig. 2 but with the airship moored;
Fig. 4 is a view of a modified form ofthe invention, taken from approximately. the same viewpoint as areFigs. 2 and 3, but without the airship;
Fig. 5 is a PEISPEClDlVGVlQW, with parts cut away, of the upright member or mooring mast of Figs. 1 toi, inclusive; 1
Fi is a perspective View of another o the invention, showing an airship iorm 1 in t e initial stages of mooring;
-ig. 7 is a view of the mooring device ow 'n Fig. 6 taken from the astern of the ,which is moored; I Fig. 8 is a perspective view slightly from above of a further form ofthe: lnvention,
showing the airship in the final stages of mooring; and
Fig. 9 is a perspective view taken slightly from above showing a still further form of the invention.
In order to accomplish the objects of the invention, the airship is preferably first made fast to an upright member or special mooring mast that is adapted to raise or lower the airship while attached to a movable fitting on said mast. WVhen lowered, the shelter for the airship is placed about the airship in one of several ways, and so avoids the dangers of attempting to run the airship into a shelter, especially with wind con'di tions not altogether favorable. In this manner, although the airship maybe made fast to the mooring mast under turbulent weather conditions, there is no dange of its striking the shelter, because the latter is opened up wide and. hence entirely out of the way. As the airship is lowered, the shelter may be used as a windbreak to ameliorate air conditions about the airship. And as the shelter is finally closed about the airship, more and the wind, so that the upright member or special mooring mast, 11, is directly upwind, and the airship approaches it along the platform 10, and hence, directly into the wind. The mast cable, 15, is already in position as shown, lying on the platform 10 in a position convenient for quick use. As the airship approaches slowly toward the .mooring fixture, 51, on the mast 11, the landing crew on the platform 10 secure the end of the nose cable 2 and fasten itto the endof the mast cable 15. This done, the cables and 2 are wound in through the mooring fixture 51, by means such as shown in Fig. 5, and the airship 1 is brought slowly up to the mooring fixture 51; in the process, the motors of the airship 1 may be reversed or inoperative, or under some wind conditions, still helping to propel the airship forward.
When the airship is clear up to the mooring fixture 51, it is secured there, preferably with means for quickly letting go in case of emergency, and the mooring fixture and airship are lowered toward the platform 10. \Vhen within reach, the auxiliary cables, 3, on the airship are secured by the crew on the platform 10, and may be held manually, or preferably are passed through the hatches, such as 17, to power-operated winding drums or winches, (see Figs. 2, 3, 4, and 7). \Vhen these are secured so that the airship may be held from lateral swinging, the shelte'r walls 12 are raised by power-operated means, which may act on the gear sectors 32 20 (Fig. 3) and thus cause the shelter walls, 12, to rotate about the horizontal hin cs, 13, until they meet over the airship 1. T e final lowering and securing of the airship to the platform 10 and the raising of the shelter walls, 12, progress together; the higher the walls are at any instant, the more shelter from wind they afford, hence the nearer the latform it is safe to bring the airship. ntil finally, when the walls are closed over 80 the top of the airship and any desired end shelter such as curtains is in place, the airship may be made solidly secure onto platform 10, and passengers and freight, as well as fuel and other supplies, may be trans- 35 ferred to or from the airship cars in much the samemanner as is done in the case of railway trains and the like. This eliminates the tedious rocess of having to transfer assengers, reight and supp ies from the op of a high mooring mast to a swinging airshi and then carrying along a considerable length of passageway within the airshi to their final destination. It further ma es it unnecessary to be constantly on the alert in regard to thebuoyancy of the airship, due to change of load, change of gas pressureor temperature and possib e rain or snow loads.
In addition to the facility gained in handling passengers, freight and supplies, much ter confidence would be felt by passengets boarding the airship cars in much the same manner as the would the cars of a railway train to whic they are already accustamed. F u'rther, the airship itself is protected from sun, wind and weather exceptwhen in actual flying service-the sun is own to have a marked deteriorating ef fect on airship fabrics, the wind causes stresses on the airship structure when moored to a mooring mast which approach those of flying service, and in some cases probably are more severe than normal flight, preciating the airship unnecessarily. Pro- 35 t'ection from weather is not only beneficial thus defor the airship and the load, including passengers alighting therefrom or boarding it, but also, it permits the thorough inspection of all parts of the airship and the making of minor repairs during the lay-over between flights.
The upright member or special mooring mast, 11, is preferably supported or strengthened by auxiliary members such as the slantingbrace 11 and the necessary tie members. In this form of the invention, the mast 11 is mounted at one end of the platform 10, which in turn is pivoted about a point in about the center of its length, and mounted on wheels, 14, which run on the series of concentric circular tracks, 16. Thus, the whole sweeps out an area not much greater than the circle whose diameter is the length of the platform 10, which latter is determined by the length of the longest airship to be accommodated. As it would be structurally diflicult and unnecessarily costl in most instances to make platform 10 in a single rigid unit, Fig. 1 shows this platform sub-divided into sections, as wellastheshelterwalls 12. Platform sections are preferably driven about their respectivetracks by electric motors, and it is a simple matter for one skilled in the art to proportion the driving forces and controlling devices therefor in such a manner that relatively small intersection. stresses will have to be cared for by the couplings between sections. The fact'that the whole structure is normally kept aligned with the wind direction makes it possible to reduce wind forces on it, and thus to make a lighter and less expensive structure than would be required in a fixed hangar.
In special cases, such as Where the mooring device of the above type is to be mounted on the roofs of buildings in a city, the platform lO may have to be one unit.
Ingeneral, the upright member 11 will be made sufficiently tall so that the airship may fly over obstacles in the imu'iediate neighborhood of the landing field and still be on the level of the top of upright 11, where the airship is first brought to the mooring fixture 51. Thus it wouldbepossibleto utilize a space even entirely surrounded by buildings or trees, which would shelter the whole structure to a considerable extent from winds, and which would also permit of the location of the landing field in a built-up section of a city. The numeral 19 therefore may represent the ground or the top of a building or other suit able place.
Fig. 2 shows the mooring process from the viewpoint of an observer following behind the airship 1. The nose cable 2 is seen dragging on the platform 10, ready to be picked up by the landing crew. The auxiliary cables, 3, are seen still out of reach. The location of the series of winches, 20, is seen below the landing stage of the platform 10,
and so out the way of crew and airship. Other elements are as described for Fig. 1.
The completed mooring operation is shown in Fig. The shelter walls, 12, have closed over the airship 1, which is secured by the auxiliary cables 3 and winches (and such other means as my seem desirable) to platform 10, and it is convenient for the transfer of passengers, freight, supplies and the like. It will be noted that in the final pulling down of the airship 1 to platform 10, it is desirable to back the former away from the mooring fixture 51, and to allow ample slack on nose cable 2. The airship is then free to swing laterally about the auxiliary cables, 3, without inducing severe stresses at the nose.
Fig. i shows a form of mooring device very similar to that of Figs. 1, 2 and 3, the prinipal difference being that the platform has upwardly extending wallsofa fixed nature along its sides, and that the horizontal hinges for the roof members 42 are at a height comparable with the height of the airship 1 hinges Screw-jack means, l i, are here shown for manipulating the shelter roof members 42, though any convenient means may be used for'this purpose. The mooring fixture 51 is here shown in what is normally its lowest position, such that the airship cars would be close to the platform 40.
Fig. 5 shows a oetail of a preferred form of mooring fixture, 51, and the elements of the special mooring mast, 11, which co-operate with it. The upright member 11 is surmounted by a cap, 53, which serves to hold pulley 52 and permit it to revolve about a substantially horizontal axis. Cable passes over pulley 52,-being secured atone end to the top of carriage 5 1, the other passing down and around winch drum 57 thence up again to a point of attachment at the bottom of carriage 5%. Thus, motor 58, through the non-reversible gear'members, 57,- can drive carriage 5 t'up ordown, and when'at rest, carriage 5iwill not be able to move up.
or down because of the non-reversible"feature of the gear members 57. The ordinary worm and worm gear combination will fulfill this requirement, and is the preferred means. Thus elevation control of thecarrage 54 is secured positively, and the height of'the airship when in process o-fmooring is consequently positively controlled. Wheels, 5 1*, may be used to facilitate sllding of the carriage 54 when under the pull from theattach d airship. Any other equivalent con-. structon would be satisfactory.
' The mooring fixture 51 is preferably conic in shape, ofsizeadapted to permit the entry of a member on the nose 0 the airship,which may be a ball-like structure on an extending arm, and this fixture 51 is preferably universally mounted as by means of the gimbal ring 56. One of the gimbal ring pivots (preferably the horizontal pivot) is extended clear through both faces of the frame of the carriage 54, and is provided with a gear, 55*, which meshes with the pinion on the shaft of motor 55. Mounted on this throughpivot is the winding drum 55", which serves to pull in or to let out the mast cable 15 as required in the mooring of the airship.
In this manner, means are provided for drawing the airship up to the special mooring mast 11, of holding it there as desired, and of moving the fixture 51 up or down with the airship thus held, in order to fulfill the desirable functions of this invention.
A form of the invention which. is particularly suited to places where extent of area is not of such importance as would be the case near large centers of population, is shown in Fig. 6. Herein, the mooring mast 61 is used as the pivot point of the system, the other major elements being adapted to revolve about it. Since the length of the platform 60 is determined by the length of the longest airship to be accommodated, the system will sweep out an area a little larger than the circle whose diameter is twice the length of platform 60; hence, this form of mooring device will require roughly four times the ground area of the type shown in Figs. 1, 2 and 3. On the other hand, the structure would probably not be as costly as the former.
The mooring mast 61 is built to withstand thrust in any direction, and is preferably approximately, circular in section to permit of the application of revolvable holding bands 63. At the top of mooring mast 61 and mounted on two of the revolvable holding bands 63 is mounted the, T-shaped platform 69. The upright member 11 is secured to and extends slightly above'the middle or shorter end of platform 69, thus permitting the mooring fixture 51 to come somewhat abovetlie level of said platform. Arailing may be provided around platform 69 for the safety and convenience of. the crew stationed there. Bands 63, platform 69 and upright member 11 are caused to revolve as a unit about mooring mast 61, preferably under control of an ly higher level than platform 69. It comes slowly forward and seeks to drag nose cable 2 against one of the laterally extending arms of platform 69, where it is secured by the crew and led into the winding mechanism of the mooring fixture 51. The airship will then back away and let itself be drawn slightly downward to the mooring mast. The approach 18 thus higher, clearance is possible ever higher neighboring obstacles and less danger exists of m ury, in case theairslup at first overshoots the mast-being at a highr level, it can go clear by and swing around for another attempt.
Onoe brought up to the mooring fixture 51, the airship 1 is lowered with said mooring fixture down the upright member 11 by means such as that shown in Fig. or the equivalent, coming into the shelter of the open shelter walls 62. The platform is revolved about mooring mast 61, being borne by wheels, 64, on the circular rails 67 and 16, until in alignment with the wind and airship, approximately, and when in reach of the landing crew, the auxiliary cables 3 on the airship 1 are caught and when weather conditions permit are passed through hatches, 17 to the Winches 20, below the landing stage, which winches serve to draw the airship down and hold it in place. As the airship comes lower, the shelter walls 62 are fgradually clemd about it, giving progressive y greater shelter and making it progressively safer to bring the airship closer to the landing platform 60. When finally the shelter walls 62 are completely closed about the airship 1, it will be safe to bring the airshi 3 down to the landing stage or top surface 0 platform 60, but in this final operation it is desirable to back away from mooring fixture 51, leaving a clear space between the nose of the airship 1 and the fixture 51, and allowing ample slack in the nose cable 2; this permits the airship a certain amount of lateral swing about the auxiliary cables 3 without causing severe stresses at the nose of the airship. Other attachments may be applied to the airship as required in the final or other stage of the mooring operation.
Whereas, in Fig. 1, end shelter is prefera'bl provided by curtains which are prefera ly secured to the slanting brace membeis, 11", of the special mooring lnast and to the near ends of the shelter walls 12 after the latter have closed over the airship 1, in
the mooring device of Fig. 6 a pluralityof frames are movably attached to the moorlng mast 61 at their tops and are mounted on wheels 68 at their'bottoms and are thus adapted to revolve about the mooring mast 61 as an axis and be supported and guided at their bottoms by the inner circular rail 67. Between frames 65 is normally provided a liable sheathing, 66, such as waterproofed a c, which is loose enough in the figure to unit of revolving shelter walls 62 (to v9 ch said sheathing is also attached) to close about the airship and when closed to stretch the sheathing 66 to a reasonable deof tightness. Thus it will be seen in the of the invention shown in Fig. 6, there is always a continuous surface from one excreme end of one shelter wall to the extreme end of the other shelter wall, making a large dead airspace for the reception of the airship, as opposed to the type shown in Fig.
Fig. 7 shows the airship 1 moored and sheltered by the shelter walls 62, which have closed about it. This stern view shows the normal relative positions of shelter walls (32 and platform 60, and it will be noted that in this position it is possible and desirable to link these elements together temporarily, so that in swinging with the wind, the who e may move as a unit. One of the circular tracks, 16, is shown resting on the ground 19, and supporting the shelter wall wheels, 14, and the platform wheels, 64. The moored position of the auxiliary cables 3 is also shown. held by the winches, 20.
It will be noted further, that in the above type of mooring device, the platform 60 may be eliminated, and the airship 1 be brought right to the ground 19 for loading or unloading. Man-power may be used for pulling the airship down and holding it; sand-bags may be hung on for holding down after landing, or water ballast pumped to the tanks of the airship itself for this purpose; electric or other powerdriven tractors may be utilized for pulling and holding purposes; and other means may be substituted for the functions performed by platform 60 with a saving in first cost. On the other hand, the convenience of operation with platform 60, and the saving of time in landing an airship together with the reduction in handling personnel would tend to make the additional cost of platform 60 a good investment.
Using a platform such as 60, means may readily be adapted to the winches 20, such that the upward pull on each of the auxiliary cables 3 may be measured and the excess buoyancy of the airship adjusted properly in amount and in distribution, so that the airship, on being released, will rise at a predetermined rate and on a level keel. This would be more difficult of accom lishment without the platform, which would constitute a permanent housing for the landing equipment as well as for repair parts, supplies, handling equipment for passengers, baggage, etc., rooms for night crews, customs, and for many other purposes connected with tran ortation activities of the sort. Provision' or friends of the passengers, visitors, etc., may profitably be made in the spaces within the shelter walls 62, thus keeping them separated from the landing platform 60 until it is desired to let them go onto the latter; whereas during the mooring process such locations would provide excellent views of the procedure while keeping the spectators entirely out of the way.
Provision would be made for the illumination of the elements of the mooring devices described and the obvious and desirable location of the main illuminating device would be on the mooring masts or the platform 69, from which locations a strong top illumination of the platform 10 or 60, as the case may be, would be provided and would serve as a guide and wind direction index for an airship landing at night.
Although the mooring devices described above maintain certain space relations between' the elements thereof, this space relation is not'essential to the design of a mooring device involving the principles of the invention. Figs. 8 and 9 show perspective views, slightly from above, of two forms of the device in which the shelter element is independent of the mooring mast. In either case, the airship, 1, may be moored to a mast, 81, which preferably is provided with a lowerable mooring fixture such as 51 of previous designs.
When moored to the mast the airship 1 is inclosed by the shelter elements 82 (in Fig. 8), which are adapted to approach. from the sides, independently, being mounted on a series of wheeled trucks, 8%, which may be provided with motive power and interlinked steering arrangements.
In Fig. 9, the airship, 1, is provided with shelter after being moored to the mast 81, by a light hanger 92 which is run over the airship from the end, and would preferably inclose the mast 81 as well. This hanger 92 is preferably made somewhat collapsible and is shown constructed of the arch members, 95, and brace members, 95, with treated fabric between and at the end 93. N heels, 94, provide easy means of moving the hangar to its position and are preferably power-driven individually. Brace members 95 are articulated so that they may be bent as shown in the three sections near the end 93 and so bring the corresponding arc-hes 95 closer together and reducing the length of the structure for convenience of handling. When straight, braces 95 hold the frames 95 apart and stretch the connecting fabric to the proper tightness to provide a stable and effective shelter.
End curtains or doors may be provided for either end of any of the above mooring devices, such closing means being in standard use is not an essential part of this invention.
In the figures, such standard closing means have been omitted for the sake of clarity. Other features of standard equipment may be used in conjunction with the principles of the invention, and modifications of the above described devices or equivalent means substituted therefore may combine to make up the mooring device of practice without avoiding the principles claimed as my invention in the appended claims. Electrical power devices and other motive power together with their control mechanisms and methods of application to the elements of the invention can readily be designed by one skilled in the art and are therefore not made a part of these specifications.
Although it is preferred that the airship be provided with nose cable such as 2 and auxiliary cables such as 3, any means of bringing the airship to the mooring mast fixture or attachment point which may be in use now or in the future may be considered the equivalent of nose cable 2; and any means such as standard handling ropes of airships of today or other means devised in the future may be considered the equivalent of auxiliary cables 3.
I claim: 1. In a hangar a landing platform, and a plurality of wall sections hingedly connected to the edges of said platform and adapted to I be swung upwardly to house a dirigible on said platform.
2. A combined mooring mast and hangar including a platform, a mast on the platform, a nose cap anchoring member vertically ad justable on the mast and hangar wall sections hinged to the edges of the platform and adapted to be folded about a dirigible after it has been moored to the mast.
3. A mooring device for dirigibles including a landing platform, a mooring mast having a fixed location relative to the platform, means for securing an airship to the platform, nose cap anchoring means vertically adjustable on the mast and folding hangar sections hinged to the edges of the platform and swingable to position to cooperatively house adirigible anchored on the platform.
4. A hangar including a landing platform and wall sections pivotally connected to the edges thereof adapted to cooperatively define a housing for a dirigible anchored to the platform.
5. Apparatus for anchoring and housing a dirigible including an elongated platform, a mooring mast at one end thereof and wall sections movably connected to the edges of the platform for enclosing a dirigible anchored to the mast.
Signed at Poughkeepsie, in the county of Dutchess and State of New York this twentythird day of December, A. D. 1926.
FRANK SHORT.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US157054A US1770675A (en) | 1926-12-27 | 1926-12-27 | Mooring device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US157054A US1770675A (en) | 1926-12-27 | 1926-12-27 | Mooring device |
Publications (1)
Publication Number | Publication Date |
---|---|
US1770675A true US1770675A (en) | 1930-07-15 |
Family
ID=22562170
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US157054A Expired - Lifetime US1770675A (en) | 1926-12-27 | 1926-12-27 | Mooring device |
Country Status (1)
Country | Link |
---|---|
US (1) | US1770675A (en) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2939657A (en) * | 1957-02-25 | 1960-06-07 | Cleveland Pneumatic Ind Inc | Aircraft landing mechanism |
US3147940A (en) * | 1962-11-03 | 1964-09-08 | Dornier Werke Gmbh | Portable heliport and transporting vehicle for a foldable helicopter |
US3521836A (en) * | 1968-08-06 | 1970-07-28 | Arthur D Struble Jr | Inflated buoyant wing |
US3972493A (en) * | 1975-01-29 | 1976-08-03 | Milne William G | Docking device for a dirigible |
US5431359A (en) * | 1994-04-04 | 1995-07-11 | Lockheed Corporation | Docking system for a lighter-than-air vehicle |
US5564653A (en) * | 1994-06-20 | 1996-10-15 | Ohayon; Shalom | High performance anti-weather protection system for space shuttles and launching vehicles |
WO2000073144A1 (en) * | 1999-05-28 | 2000-12-07 | Uti Holding + Management Ag | Set-down station |
US6231007B1 (en) * | 1996-06-25 | 2001-05-15 | Cargolifter Ag | Method for the precise setting down or picking up of cargo from airships |
US20100200694A1 (en) * | 2007-02-05 | 2010-08-12 | Xavier Tripier-Larivaud | Landing area for air machines or vehicles comprising extendable reception means |
US20150367959A1 (en) * | 2013-01-18 | 2015-12-24 | Altave Indústria, Comércio E Exportação De Aeronaves Ltda- Me | Airship-mooring device |
JP2016040157A (en) * | 2014-08-13 | 2016-03-24 | ソフトバンク株式会社 | Balloon storage box, balloon transport device, and method for releasing mooring balloon |
WO2016072239A1 (en) * | 2014-11-07 | 2016-05-12 | ソフトバンク株式会社 | Balloon storage box, balloon transportation device, and method for releasing anchored balloons |
JP2016088391A (en) * | 2014-11-07 | 2016-05-23 | ソフトバンク株式会社 | Balloon mooring device, balloon storage box, and balloon transport device |
JP2016088392A (en) * | 2014-11-07 | 2016-05-23 | ソフトバンク株式会社 | Balloon mooring device, balloon transport device and balloon mooring ship |
US10232955B2 (en) * | 2016-03-18 | 2019-03-19 | Loon Llc | Portable balloon launch rig |
-
1926
- 1926-12-27 US US157054A patent/US1770675A/en not_active Expired - Lifetime
Cited By (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2939657A (en) * | 1957-02-25 | 1960-06-07 | Cleveland Pneumatic Ind Inc | Aircraft landing mechanism |
US3147940A (en) * | 1962-11-03 | 1964-09-08 | Dornier Werke Gmbh | Portable heliport and transporting vehicle for a foldable helicopter |
US3521836A (en) * | 1968-08-06 | 1970-07-28 | Arthur D Struble Jr | Inflated buoyant wing |
US3972493A (en) * | 1975-01-29 | 1976-08-03 | Milne William G | Docking device for a dirigible |
CN1063398C (en) * | 1994-04-04 | 2001-03-21 | 洛克希德·马丁公司 | A docking systemf for a lighter-than-air vehicle |
WO1995026903A1 (en) * | 1994-04-04 | 1995-10-12 | Lockheed Martin Corporation | A docking system for a lighter-than-air vehicle |
EP0754140A1 (en) * | 1994-04-04 | 1997-01-22 | Lockheed Martin Corporation | A docking system for a lighter-than-air vehicle |
EP0754140A4 (en) * | 1994-04-04 | 1999-03-24 | Lockheed Corp | A docking system for a lighter-than-air vehicle |
US5431359A (en) * | 1994-04-04 | 1995-07-11 | Lockheed Corporation | Docking system for a lighter-than-air vehicle |
US5564653A (en) * | 1994-06-20 | 1996-10-15 | Ohayon; Shalom | High performance anti-weather protection system for space shuttles and launching vehicles |
US6231007B1 (en) * | 1996-06-25 | 2001-05-15 | Cargolifter Ag | Method for the precise setting down or picking up of cargo from airships |
WO2000073144A1 (en) * | 1999-05-28 | 2000-12-07 | Uti Holding + Management Ag | Set-down station |
US8424802B2 (en) * | 2007-02-05 | 2013-04-23 | Xavier Tripier-Larivaud | Landing area for air machines or vehicles comprising extendable reception means |
US20100200694A1 (en) * | 2007-02-05 | 2010-08-12 | Xavier Tripier-Larivaud | Landing area for air machines or vehicles comprising extendable reception means |
US20150367959A1 (en) * | 2013-01-18 | 2015-12-24 | Altave Indústria, Comércio E Exportação De Aeronaves Ltda- Me | Airship-mooring device |
US9981755B2 (en) * | 2013-01-18 | 2018-05-29 | ALTAVE INDÚSTRIA, COMÉRCIO E EXPORTAçÃO DE AERONAVES LTDA-ME | Airship-mooring device |
JP2016040157A (en) * | 2014-08-13 | 2016-03-24 | ソフトバンク株式会社 | Balloon storage box, balloon transport device, and method for releasing mooring balloon |
WO2016072239A1 (en) * | 2014-11-07 | 2016-05-12 | ソフトバンク株式会社 | Balloon storage box, balloon transportation device, and method for releasing anchored balloons |
JP2016088391A (en) * | 2014-11-07 | 2016-05-23 | ソフトバンク株式会社 | Balloon mooring device, balloon storage box, and balloon transport device |
JP2016088392A (en) * | 2014-11-07 | 2016-05-23 | ソフトバンク株式会社 | Balloon mooring device, balloon transport device and balloon mooring ship |
US10232955B2 (en) * | 2016-03-18 | 2019-03-19 | Loon Llc | Portable balloon launch rig |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US1770675A (en) | Mooring device | |
US4402479A (en) | Small tethered aerostat relocatable system | |
RU2126347C1 (en) | Mooring tower for lighter-than-air flying vehicle | |
US4269375A (en) | Hybrid annular airship | |
EP2001738B1 (en) | Aerial transporter | |
BRPI0609162A2 (en) | mobile captive balloon in a tower | |
US3248830A (en) | Retractable hangar | |
CN110481753A (en) | A kind of quick delivery system of aerostat motor driven | |
US1861069A (en) | Dirigible airship hangar | |
US1748500A (en) | Mooring of airships | |
CN111470027B (en) | Method for directly issuing airship based on top openable and closable boat warehouse | |
US1843640A (en) | Elevated airport | |
US2187436A (en) | Portable structure | |
US1861983A (en) | Mooring equipment | |
US1853777A (en) | Method of and apparatus for berthing airships | |
US2481343A (en) | Helicopter station | |
RU2339548C1 (en) | Mobil device for lighter-than-air craft holding | |
US1446440A (en) | Airship turn and transfer table | |
CN110001996B (en) | Mobile corridor for airport | |
US1867591A (en) | Dirigible air dock | |
US1823063A (en) | Means for mooring and housing airships | |
GB234169A (en) | Improvements in or relating to mooring masts and mooring gear for lighter-than-air aircraft | |
US1856446A (en) | Airplane loading station | |
US1806939A (en) | Starting and landing device fob airships of the lighter than air type | |
CN217439377U (en) | Adjustable open-close type ventilation clerestory structure |