US3858371A - Hard flush airplane shelter - Google Patents
Hard flush airplane shelter Download PDFInfo
- Publication number
- US3858371A US3858371A US442288A US44228874A US3858371A US 3858371 A US3858371 A US 3858371A US 442288 A US442288 A US 442288A US 44228874 A US44228874 A US 44228874A US 3858371 A US3858371 A US 3858371A
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- United States
- Prior art keywords
- movable
- floor
- airplane
- roof
- fixed
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- Expired - Lifetime
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H9/00—Buildings, groups of buildings or shelters adapted to withstand or provide protection against abnormal external influences, e.g. war-like action, earthquake or extreme climate
- E04H9/04—Buildings, groups of buildings or shelters adapted to withstand or provide protection against abnormal external influences, e.g. war-like action, earthquake or extreme climate against air-raid or other war-like actions
- E04H9/10—Independent shelters; Arrangement of independent splinter-proof walls
- E04H9/12—Independent shelters; Arrangement of independent splinter-proof walls entirely underneath the level of the ground, e.g. air-raid galleries
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H6/00—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages
- E04H6/44—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages for storing aircraft
Definitions
- the shelter is comprised of: a reinforced walled subsurface enclosure having a plurality of fixed columns to support a roof located such that an airplane can be lowered between the columns; a roof supported by a plurality of telescoping supports about its periphery such that the roof can be raised to a level higher than an airplane when the airplane is at ground level and lowered to be flush with the ground thus closing the subsurface enclosure and being supported by the fixed columns; and a floor suspended from the roof whereon an airplane can be placed, said floor having holes therein over the fixed columns such that when the roof is raised, the floor and airplane will be at ground level with the tops of the fixed cloumns being below'the floor, and when the roof is lowered, the fixed columns will pass through the holes in the floor as the floor descends passing alongside the airplane to support the roof in its fully lowered position.
- the shelter for airplanes disclosed being further provided with sealable ducts for the intake of air and outlet of exhaust fumes so that the engine of the airplane contained therein may be started when the shelter is
- a flat roof on the other hand, needs numerous supports or columns to resist the energy impact. With standard aircraft, there is insufficient room between columns to more the aircraft. In one typical prior art teaching this problem is solved by having the columns hydraulically retractable. Not only is this a more complex structure than desirable, but it must be open on one side for the airplane to pass in or out with the opening closable with blast-proof doors.
- FIG. I is a partial cut-away drawing showing the presently disclosed airplane shelter in the raised position both above and below ground.
- FIG. 2 is a cut-away front elevation of the present invention in the open or raised position.
- FIG. 3 is a cut-away front elevation of the present invention in the closed or lowered position.
- FIG. 4 is a top plan view of the present invention.
- FIG. 5 is a cut-away side elevation of the present invention in the closed or lowered position.
- FIG. 6 is a cut-away side elevation of the exhaust duct assembly of the present invention.
- FIG. 7 is a top plan view of the exhaust duct assembly of the present invention.
- the airplane shelter which is the subject of the present invention is shown in the open or raised position.
- Airplane 10 sits on movable metal floor 12 at the level of the surrounding ground 14 from where it can be moved unhindered into or out of the shelter.
- a movable roof 16 of steel and concrete is supported above the airplane It) by hydraulically movable columns 18.
- the movable floor 12 is hung by floor hanging columns 20 from movable roof 16.
- the movable floor I2 could be supported, lifted and lowered by hydraulic columns under the movable floor 12, and the movable roof 16 could be supported above the movable floor 12 by support columns replacing the floor hanging columns 20 designed for the compression load of the movable roof 16 rather than the tensile load of the movable floor 12 and airplane 10.
- hydraulically movable columns 18 are housed in actuators 21 contained within the reinforced concrete walls 22 of underground enclosure 24 having fixed floor 26 and reinforced concrete fixed roof support columns 28 and drainage means 30. Roof support columns 28 are topped with guided movable plates 31 which move up with movable floor 12 filling the holes 32 therein.
- FIG. 3 the embodiment shown open in FIG. 2 is now shown in the closed or lowered position.
- Hydraulically movable columns 18 of FIG. 1 have moved into hydraulic actuators 21 contained in walls 22.
- Movable roof 16 is supported by walls 22 and fixed roof support columns 28.
- the location of the air plane 10 in relation to support columns 28 is best understood by reference to FIG. 4 which is a top view of the present invention.
- the location of support columns 28 in a particular airplane shelter is a function of the shape of the airplane 10 to be housed therein.
- the support columns 28 must be located to pass through corresponding holes 32 in movable floor I2 and alongside the structures of airplane l0.
- FIG. 5 shows the location and basic structure of the floor locks 33 as well as the air intake duct assembly 34 and exhaust duct assembly 36.
- the air intake duct assembly 34 comprises a closable intake port 38 and an intake pipe 40 leading as close as possible to the engine intake (not shown) or airplane 10.
- Exhaust duct assembly 36 is shown in greater detail in FIG. 6 and FIG. 7.
- Extendable connecting pipes 42 are provided to connect the exhaust pipes of airplane 10 to exhaust duct 44.
- Exhaust duct 44 leads to the outside at ground level where it terminates in exhaust port 46 which can be opened or closed by exhaust port stopper 48 through exhaust port stopper actuator 50.
- Closable intake port 38 would be constructed in the same manner as the closable port of exhaust duct assembly 36 just described.
- floor lock 33 is shown as comprising a locking pin 52 and a lock actuator 54.
- locking pin 52 In the raised position locking pin 52 is extended and engages floor l2 locking it in position.
- control circuitry (not shown) will cause the lock actuator 54 to retract the locking pin 52 from engagement with floor 12 prior to lowering floor 12.
- a shelter for an airplane comprising:
- a substantially vertical wall disposed about the perimeter of said fixed floor, said wall defining an enclosure wherein the airplane can be placed without any member of the airplane extending above the top of said wall;
- a movable roof so shaped as to be supportable about its periphery by the top of said substantially vertical wall and additionally supportable by the tops of said support columns when said movable roof is resting upon the top of said substantially vertical wall;
- a shelter for an airplane comprising:
- a substantially vertical wall disposed about the perimeter of said fixed floor, said wall defining an enclosure wherein the airplane can be placed without any member of the airplane extending above the top of said wall;
- a movable roof so shaped as to be supportable about its periphery by the top of said substantially vertical wall and additionally supportable by the tops of said support columns when said movable roof is resting upon the top of said substantially vertical wall;
- a movable floor above said fixed floor, below said movable roof, and within said enclosure said movable floor being located a sufficient distance below said movable roof to allow the airplane to be placed between said movable roof and said movable floor, said movable floor containing holes for passage therethrough of said fixed support columns as said movable floor is moved up and down, said movable floor being so shaped and movable that in one position the tops of said fixed support columns will be disposed sufficiently close to the surface of said movable floor to allow the airplane to be moved onto and off of said movable floor;
- means for moving said movable roof and said movable floor up and down in combination said means for moving said movable roof and said movable floorup and down in combination being operably attached to lift and lower said movable roof, and, said movable floor being suspended from said movable roof by said means for connecting said movable roof to said movable floor.
- said plurality of fixed support columns have movable plates attached to the top thereof, said movable plates being so shaped as to fill said holes in said movable floor for the passage therethrough of said fixed support columns when said movable floor is in said position to allow the airplane to be moved onto and off of said movable floor.
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- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Environmental & Geological Engineering (AREA)
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
- Pipe Accessories (AREA)
- Separation Using Semi-Permeable Membranes (AREA)
Abstract
A shelter for airplanes characterized by being flush to the ground when closed thereby being virtually invisible, and by being highly resistive to high energy explosive impact. The shelter is comprised of: a reinforced walled subsurface enclosure having a plurality of fixed columns to support a roof located such that an airplane can be lowered between the columns; a roof supported by a plurality of telescoping supports about its periphery such that the roof can be raised to a level higher than an airplane when the airplane is at ground level and lowered to be flush with the ground thus closing the subsurface enclosure and being supported by the fixed columns; and a floor suspended from the roof whereon an airplane can be placed, said floor having holes therein over the fixed columns such that when the roof is raised, the floor and airplane will be at ground level with the tops of the fixed cloumns being below the floor, and when the roof is lowered, the fixed columns will pass through the holes in the floor as the floor descends passing alongside the airplane to support the roof in its fully lowered position. The shelter for airplanes disclosed being further provided with sealable ducts for the intake of air and outlet of exhaust fumes so that the engine of the airplane contained therein may be started when the shelter is in the closed position for maintenance and instant readiness for takeoff after attack.
Description
limited J Averill ttes tent [191 .llan.7, 11975 HARD IFLUSH AIRPLANE SHELTER [75] Inventor: Robert L. Averill, Seattle, Wash.
[73] Assignee: The Boeing Company, Seattle,
Wash.
[22] Filed: Feb. 13, 1974 [21] Appl. No.: 442,288
[56] References Cited UNITED STATES PATENTS 3,258,885 7/1966 Lodige 52/64 FOREIGN PATENTS OR APPLICATIONS 581,240 6/1946 Great Britain 52/66 738,418 10/1955 Great Britain 52/67 613,557 11/1948 Great Britain 52/67 Primary Examiner-John E. Murtagh Attorney, Agent, or Firm-Donald A. Streck [57] ABSTRACT A shelter for airplanes characterized by being flush to the ground when closed thereby being virtually invisible, and by being highly resistive to high energy explosive impact. The shelter is comprised of: a reinforced walled subsurface enclosure having a plurality of fixed columns to support a roof located such that an airplane can be lowered between the columns; a roof supported by a plurality of telescoping supports about its periphery such that the roof can be raised to a level higher than an airplane when the airplane is at ground level and lowered to be flush with the ground thus closing the subsurface enclosure and being supported by the fixed columns; and a floor suspended from the roof whereon an airplane can be placed, said floor having holes therein over the fixed columns such that when the roof is raised, the floor and airplane will be at ground level with the tops of the fixed cloumns being below'the floor, and when the roof is lowered, the fixed columns will pass through the holes in the floor as the floor descends passing alongside the airplane to support the roof in its fully lowered position. The shelter for airplanes disclosed being further provided with sealable ducts for the intake of air and outlet of exhaust fumes so that the engine of the airplane contained therein may be started when the shelter is in the closed position for maintenance and instant readiness for takeoff after attack.
3 Claims, 7 Drawing Figures Patented Jan. 7, 1975 4 Sheets-Sheet 1 4 Sheets-Sheet 2 II ill Patented Jan. 7, 1975' Patented Jan. 7, 1975 3,858,371
4 Sheets-Sheet .5
Patented Jan. 7, 1975 3,858,371
4 Sheets-Sheet 4 ll-llAlRll) FLUSH AIRPLANE SHELTER BACKGROUND OF THE INVENTION 1. Field of the Invention Relates to airplane shelters and more particularly to bombproof shelters for military airplanes.
2. Description of the Prior Art In a bomb-proof airplane shelter the primary consideration is making the structure capable of withstanding the energy impulse of an exploding bomb. This is, of course, even more critical when nuclear devices are considered. A curved roof such as a quonset or dome has a natural strength from the shape. Likewise, the shelter can be built into a hillside or mountain for additional strength. Hillsides and mountains, however, are
not always available. Any structure rising above ground level is visible to enemy aircraft or ground observers and, therefore, more likely to receive a direct hit and indicate critical target locations.
A flat roof, on the other hand, needs numerous supports or columns to resist the energy impact. With standard aircraft, there is insufficient room between columns to more the aircraft. In one typical prior art teaching this problem is solved by having the columns hydraulically retractable. Not only is this a more complex structure than desirable, but it must be open on one side for the airplane to pass in or out with the opening closable with blast-proof doors.
Therefore, it is an object of the present invention to provide an airplane shelter of flatroof design wherein the roof can be flush with the ground providing virtually no indication of the existence of the shelter to ground or air observers at a distance.
It is a further object of the present invention to provide an airplane shelter of flatroof design wherein a minimum of movable supports for the roof are required It is another object of the present invention to provide an airplane shelter of flati'oof design not requiring blast-proof doors for the entry and exit of the airplane.
It is yet another object of the present invention to provide an airplane shelter of flatroof design wherein the airplane housed therein can be started with the shelter in the closed position to allow periodic maintenance on the airplane and prior startup for instant exit upon opening the shelter after enemy attack.
DESCRIPTION OF THE DRAWINGS FIG. I is a partial cut-away drawing showing the presently disclosed airplane shelter in the raised position both above and below ground.
FIG. 2 is a cut-away front elevation of the present invention in the open or raised position.
FIG. 3 is a cut-away front elevation of the present invention in the closed or lowered position.
FIG. 4 is a top plan view of the present invention.
FIG. 5 is a cut-away side elevation of the present invention in the closed or lowered position.
FIG. 6 is a cut-away side elevation of the exhaust duct assembly of the present invention.
FIG. 7 is a top plan view of the exhaust duct assembly of the present invention.
DESCRIPTION AND OPERATION OF THE INVENTION Referring to FIG. 2, the airplane shelter which is the subject of the present invention is shown in the open or raised position. Airplane 10 sits on movable metal floor 12 at the level of the surrounding ground 14 from where it can be moved unhindered into or out of the shelter. A movable roof 16 of steel and concrete is supported above the airplane It) by hydraulically movable columns 18. In the preferred embodiment as shown, the movable floor 12 is hung by floor hanging columns 20 from movable roof 16. In an alternate embodiment, the movable floor I2 could be supported, lifted and lowered by hydraulic columns under the movable floor 12, and the movable roof 16 could be supported above the movable floor 12 by support columns replacing the floor hanging columns 20 designed for the compression load of the movable roof 16 rather than the tensile load of the movable floor 12 and airplane 10. In the preferred embodiment shown, hydraulically movable columns 18 are housed in actuators 21 contained within the reinforced concrete walls 22 of underground enclosure 24 having fixed floor 26 and reinforced concrete fixed roof support columns 28 and drainage means 30. Roof support columns 28 are topped with guided movable plates 31 which move up with movable floor 12 filling the holes 32 therein.
Referring now to FIG. 3, the embodiment shown open in FIG. 2 is now shown in the closed or lowered position. Hydraulically movable columns 18 of FIG. 1 have moved into hydraulic actuators 21 contained in walls 22. Movable roof 16 is supported by walls 22 and fixed roof support columns 28. The location of the air plane 10 in relation to support columns 28 is best understood by reference to FIG. 4 which is a top view of the present invention. The location of support columns 28 in a particular airplane shelter is a function of the shape of the airplane 10 to be housed therein. The support columns 28 must be located to pass through corresponding holes 32 in movable floor I2 and alongside the structures of airplane l0.
Referring to FIG. 4, the following additional features are shown. Since the-movable floor 12 is suspended from the movable roof 16 by floor hanging columns 20, floor locks 33 are provided to lock the movable floor 12 in place in the raised or open position to prevent lateral'motion or tipping of movable floor 12 during entry or exit of airplane 10. Additionally, air intake duct as sembly 34 and exhaust duct assembly 36 are provided to allow operation of the engines of airplane 10 when the shelter is in the lowered or closed position. These additional features are shown further in FIGS. 5, 6 and 7. FIG. 5 shows the location and basic structure of the floor locks 33 as well as the air intake duct assembly 34 and exhaust duct assembly 36. The air intake duct assembly 34 comprises a closable intake port 38 and an intake pipe 40 leading as close as possible to the engine intake (not shown) or airplane 10.. Exhaust duct assembly 36 is shown in greater detail in FIG. 6 and FIG. 7. Extendable connecting pipes 42 are provided to connect the exhaust pipes of airplane 10 to exhaust duct 44. Exhaust duct 44 leads to the outside at ground level where it terminates in exhaust port 46 which can be opened or closed by exhaust port stopper 48 through exhaust port stopper actuator 50. Closable intake port 38 would be constructed in the same manner as the closable port of exhaust duct assembly 36 just described.
Also referring to FIG. 6, floor lock 33 is shown as comprising a locking pin 52 and a lock actuator 54. In the raised position locking pin 52 is extended and engages floor l2 locking it in position. Upon the command to close the shelter, control circuitry (not shown) will cause the lock actuator 54 to retract the locking pin 52 from engagement with floor 12 prior to lowering floor 12.
Having thus described my invention, what is claimed 1. A shelter for an airplane comprising:
b. a substantially vertical wall disposed about the perimeter of said fixed floor, said wall defining an enclosure wherein the airplane can be placed without any member of the airplane extending above the top of said wall;
c. a plurality of fixed support columns attached to said fixed floor, said support columns being disposed to pass alongside the members of the airplane when the airplane is in the enclosure while being substantially equally dispersed over said fixed floor;
d. a movable roof so shaped as to be supportable about its periphery by the top of said substantially vertical wall and additionally supportable by the tops of said support columns when said movable roof is resting upon the top of said substantially vertical wall;
e. a movable floor above said fixed floor, below said movable roof, and within said enclosure, said movable floor being located a sufficient distance below said movable roof to allow the airplane to be placed between said movable roof and said movable floor, said movable floor containing holes for the passage therethrough of said fixed support columns as said movable floor is moved up and down, said movable floor being so shaped and movable that in one position the tops of said fixed support columns will be disposed sufficiently close to the surface of said movable floor to allow the airplane to be moved onto and off of said movable floor; means for connecting said movable roof to said movable floor such that said movable roof and said movable floor will move up and down in combination'; and
g. means for moving said movable roof and said movable floor up and down in combination.
2. A shelter for an airplane comprising:
b. a substantially vertical wall disposed about the perimeter of said fixed floor, said wall defining an enclosure wherein the airplane can be placed without any member of the airplane extending above the top of said wall;
c. a plurality of fixed support columns attached to said fixed floor, said support columns being disposed to pass alongside the members of the airplane when the airplane is in the enclosure while being substantially equally dispersed over said fixed floor;
d. a movable roof so shaped as to be supportable about its periphery by the top of said substantially vertical wall and additionally supportable by the tops of said support columns when said movable roof is resting upon the top of said substantially vertical wall;
e. a movable floor above said fixed floor, below said movable roof, and within said enclosure, said movable floor being located a sufficient distance below said movable roof to allow the airplane to be placed between said movable roof and said movable floor, said movable floor containing holes for passage therethrough of said fixed support columns as said movable floor is moved up and down, said movable floor being so shaped and movable that in one position the tops of said fixed support columns will be disposed sufficiently close to the surface of said movable floor to allow the airplane to be moved onto and off of said movable floor;
f. means for connecting said movable roof to said movable floor such that said movable roof and said movable floor will move up and down in combination; and
g. means for moving said movable roof and said movable floor up and down in combination, said means for moving said movable roof and said movable floorup and down in combination being operably attached to lift and lower said movable roof, and, said movable floor being suspended from said movable roof by said means for connecting said movable roof to said movable floor.
3. A shelter for an airplane as claimed in claim 2 wherein additionally:
said plurality of fixed support columns have movable plates attached to the top thereof, said movable plates being so shaped as to fill said holes in said movable floor for the passage therethrough of said fixed support columns when said movable floor is in said position to allow the airplane to be moved onto and off of said movable floor.
Claims (3)
1. A shelter for an airplane comprising: a. a fixed floor; b. a substantially vertical wall disposed about the perimeter of said fixed floor, said wall defining an enclosure wherein the airplane can be placed without any member of the airplane extending above the top of said wall; c. a plurality of fixed support columns attached to said fixed floor, said support columns being disposed to pass alongside the members of the airplane when the airplane is in the enclosure while being substantially equally dispersed over said fixed floor; d. a movable roof so shaped as to be supportable about its periphery by the top of said substantially vertical wall and additionally supportable by the tops of said support columns when said movable roof is resting upon the top of said substantially vertical wall; e. a movable floor above said fixed floor, below said movable roof, and within said enclosure, said movable floor being located a sufficient distance below said movable roof to allow the airplane to be placed between said movable roof and said movable floor, said movable floor containing holes for the passage therethrough of said fixed support columns as said movable floor is moved up and down, said movable floor being so shaped and movable that in one position the tops of said fixed support columns will be disposed sufficiently close to the surface of said movable floor to allow the airplane to be moved onto and off of said movable floor; f. means for connecting said movable roof to said movable floor such that said movable roof and said movable floor will move up and down in combination; and g. means for moving said movable roof and said movable floor up and down in combination.
2. A shelter for an airplane comprising: a. a fixed floor; b. a substantially vertical wall disposed about the perimeter of said fixed floor, said wall defining an enclosure wherein the airplane can be placed without any member of the airplane extending above the top of said wall; c. a plurality of fixed support columns attached to said fixed floor, said support columns being disposed to pass alongside the members of the airplane when the airplane is in the enclosure while being substantially equally dispersed over said fixed floor; d. a movable roof so shaped as to be supportable about its periphery by the top of said substantially vertical wall and additionally supportable by the tops of said support columns when said movable roof is resting upon the top of said substantially vertical wall; e. a movable floor above said fixed floor, below said movable roof, and within said enclosure, said movable floor being located a sufficient distance below said movable roof to allow the airplane to be placed between said movable roof and said movable floor, said movable floor containing holes for passage therethrough of said fixed support columns as said movable floor is moved up and down, said movable floor being so shaped and movable that in one position the tops of said fixed support columns will be disposed sufficiently close to the surface of said movable floor to allow the airplane to be moved onto and off of said movable floor; f. meanS for connecting said movable roof to said movable floor such that said movable roof and said movable floor will move up and down in combination; and g. means for moving said movable roof and said movable floor up and down in combination, said means for moving said movable roof and said movable floor up and down in combination being operably attached to lift and lower said movable roof, and, said movable floor being suspended from said movable roof by said means for connecting said movable roof to said movable floor.
3. A shelter for an airplane as claimed in claim 2 wherein additionally: said plurality of fixed support columns have movable plates attached to the top thereof, said movable plates being so shaped as to fill said holes in said movable floor for the passage therethrough of said fixed support columns when said movable floor is in said position to allow the airplane to be moved onto and off of said movable floor.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US442288A US3858371A (en) | 1974-02-13 | 1974-02-13 | Hard flush airplane shelter |
| JP50019403A JPS5194481A (en) | 1974-02-13 | 1975-02-15 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US442288A US3858371A (en) | 1974-02-13 | 1974-02-13 | Hard flush airplane shelter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3858371A true US3858371A (en) | 1975-01-07 |
Family
ID=23756246
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US442288A Expired - Lifetime US3858371A (en) | 1974-02-13 | 1974-02-13 | Hard flush airplane shelter |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US3858371A (en) |
| JP (1) | JPS5194481A (en) |
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4075799A (en) * | 1976-08-30 | 1978-02-28 | Lemelson Jerome H | Building insulation system and method |
| US4149712A (en) * | 1977-09-15 | 1979-04-17 | Murphy Richard J | Physical exercise apparatus |
| US4294308A (en) * | 1979-02-09 | 1981-10-13 | Joseph Spanier | Method and assembly for camouflaging at least one building |
| US4416578A (en) * | 1981-04-20 | 1983-11-22 | Behncke Hahns Juergen | Multi-story elevator-type garage |
| EP0200717A1 (en) * | 1985-05-02 | 1986-11-05 | Waagner-Biro Aktiengesellschaft | Hangar |
| FR2602814A1 (en) * | 1986-07-28 | 1988-02-19 | Sofreavia | Buried shelter particularly for aircraft, such as combat aircraft |
| US4747242A (en) * | 1985-07-01 | 1988-05-31 | Up And Down Garage System A/S | Two level structure for parking vehicles or storing goods |
| US5140786A (en) * | 1990-10-11 | 1992-08-25 | Giancarlo Galeazzi | Waste collection device |
| US5235133A (en) * | 1990-09-10 | 1993-08-10 | Environmental Enclosures International | Housing |
| US5794389A (en) * | 1996-01-16 | 1998-08-18 | Vysma; Erwin L. | Hurricane home shelter |
| US6467231B1 (en) | 2000-01-27 | 2002-10-22 | Herman Carlinsky | Protective building structure system |
| US20030100988A1 (en) * | 2000-03-15 | 2003-05-29 | Pekka Lehto | System and method specifically intended for the construction of fuel distribution |
| US20040093807A1 (en) * | 2002-11-20 | 2004-05-20 | Richard Ensign | Storage structure for sailplanes and small aircraft |
| US20080279661A1 (en) * | 2007-05-08 | 2008-11-13 | Yung-Ming Chou | Multi-tier parking lot with a waterproof parking space under each ground parking space |
| US20100325973A1 (en) * | 2008-02-17 | 2010-12-30 | Israel Hirshberg | building method and buildings |
| KR101226052B1 (en) * | 2012-06-14 | 2013-01-24 | 김재문 | Tactical hangar apparatus for weapon |
| JP2016516927A (en) * | 2013-04-18 | 2016-06-09 | ヴァサポッロ，ラッファエラ | Underground hangar for helicopter |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5448052U (en) * | 1977-09-12 | 1979-04-03 | ||
| JPS6318409Y2 (en) * | 1980-03-25 | 1988-05-24 | ||
| JPS61107912A (en) * | 1984-10-30 | 1986-05-26 | Mitsui Kensaku Toishi Kk | Filter unit |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3258885A (en) * | 1962-01-08 | 1966-07-05 | Lodige Alois | Conveyor shafts with conveying devices |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3786925A (en) * | 1972-02-14 | 1974-01-22 | Raypak Inc | Means for sealing membrane carrying tubes |
-
1974
- 1974-02-13 US US442288A patent/US3858371A/en not_active Expired - Lifetime
-
1975
- 1975-02-15 JP JP50019403A patent/JPS5194481A/ja active Pending
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3258885A (en) * | 1962-01-08 | 1966-07-05 | Lodige Alois | Conveyor shafts with conveying devices |
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4075799A (en) * | 1976-08-30 | 1978-02-28 | Lemelson Jerome H | Building insulation system and method |
| US4149712A (en) * | 1977-09-15 | 1979-04-17 | Murphy Richard J | Physical exercise apparatus |
| US4294308A (en) * | 1979-02-09 | 1981-10-13 | Joseph Spanier | Method and assembly for camouflaging at least one building |
| US4416578A (en) * | 1981-04-20 | 1983-11-22 | Behncke Hahns Juergen | Multi-story elevator-type garage |
| EP0200717A1 (en) * | 1985-05-02 | 1986-11-05 | Waagner-Biro Aktiengesellschaft | Hangar |
| US4747242A (en) * | 1985-07-01 | 1988-05-31 | Up And Down Garage System A/S | Two level structure for parking vehicles or storing goods |
| FR2602814A1 (en) * | 1986-07-28 | 1988-02-19 | Sofreavia | Buried shelter particularly for aircraft, such as combat aircraft |
| US5235133A (en) * | 1990-09-10 | 1993-08-10 | Environmental Enclosures International | Housing |
| US5140786A (en) * | 1990-10-11 | 1992-08-25 | Giancarlo Galeazzi | Waste collection device |
| US5794389A (en) * | 1996-01-16 | 1998-08-18 | Vysma; Erwin L. | Hurricane home shelter |
| US6467231B1 (en) | 2000-01-27 | 2002-10-22 | Herman Carlinsky | Protective building structure system |
| US20030100988A1 (en) * | 2000-03-15 | 2003-05-29 | Pekka Lehto | System and method specifically intended for the construction of fuel distribution |
| US6820378B2 (en) * | 2000-03-15 | 2004-11-23 | Pekka Lehto | System and method specifically intended for the construction of fuel distribution forecourts |
| US20040093807A1 (en) * | 2002-11-20 | 2004-05-20 | Richard Ensign | Storage structure for sailplanes and small aircraft |
| US6804917B2 (en) * | 2002-11-20 | 2004-10-19 | Richard Ensign | Storage structure for sailplanes and small aircraft |
| US20080279661A1 (en) * | 2007-05-08 | 2008-11-13 | Yung-Ming Chou | Multi-tier parking lot with a waterproof parking space under each ground parking space |
| US20100325973A1 (en) * | 2008-02-17 | 2010-12-30 | Israel Hirshberg | building method and buildings |
| KR101226052B1 (en) * | 2012-06-14 | 2013-01-24 | 김재문 | Tactical hangar apparatus for weapon |
| JP2016516927A (en) * | 2013-04-18 | 2016-06-09 | ヴァサポッロ，ラッファエラ | Underground hangar for helicopter |
| US10071821B2 (en) * | 2013-04-18 | 2018-09-11 | Raffaella Vasapollo | Underground hangar for helicopters |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5194481A (en) | 1976-08-19 |
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