JPS6257560B2 - - Google Patents
Info
- Publication number
- JPS6257560B2 JPS6257560B2 JP57088463A JP8846382A JPS6257560B2 JP S6257560 B2 JPS6257560 B2 JP S6257560B2 JP 57088463 A JP57088463 A JP 57088463A JP 8846382 A JP8846382 A JP 8846382A JP S6257560 B2 JPS6257560 B2 JP S6257560B2
- Authority
- JP
- Japan
- Prior art keywords
- hangar
- plates
- top plate
- plate
- rectangular parallelepiped
- 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
Links
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
- B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
- Tents Or Canopies (AREA)
- Auxiliary Methods And Devices For Loading And Unloading (AREA)
Description
【発明の詳細な説明】 本発明は回転翼機の格納庫に関する。[Detailed description of the invention] The present invention relates to a hangar for a rotary wing aircraft.
従来、ヘリコプター等の回転翼機の格納庫は地
上に設けられている。従つて、これらの格納庫は
移動するものではなく、単に格納庫としての働き
をなすだけであつた。 Conventionally, hangars for rotary wing aircraft such as helicopters are provided on the ground. Therefore, these hangars were not mobile, but simply served as hangars.
本発明はこのような従来の回転翼機の格納庫と
は全く異なる新規な格納庫を提供するもので、そ
の特徴とするところは車輌に塔載若しくは牽引さ
れる直方体容器を回転翼機格納可能に構成し、前
記直方体容器の頂板を長手方向の分割線に沿つて
２つに分割し、それぞれの頂板の基端側を直方体
容器の両側板上端に、回動自在に接続し、一方、
直方体の両側板および両端板の下端を台車に回動
自在に接続し、上記接続された側板と頂板および
上記端板を展開させるためのウインチをそれぞれ
有するとともに、その上端面で両頂板を支持可能
でかつ上端側部で端板を支持して位置決めする支
柱を台車の両側端部に挿脱可能に立設し、上記側
板と頂板を展開するためのウインチに巻回され、
両側板内中央部に配設されたガイドシーブを介し
て両頂板の先端側内面に連結された索と、上記端
板を展開するためのウインチに巻回され、端板の
上端部内面に連結されている索とにより直方体容
器の前記側板、頂板および端板を外方に、水平に
展開可能に構成したことにある。このようなもの
によれば、端板を展開させるためのウインチに巻
回された索を巻出すことにより、この端板を水平
状態にまで展開することが可能である。また側板
と頂板を展開させるためのウインチに巻回された
索を巻出せば、この索は側板中央部に配設された
ガイドシーブを介して頂板の先端側内面に連結さ
れていることから、これら側板と頂板とが同時に
水平状態にまで展開される。さらにウインチが取
付けられた支柱は台車に対し挿脱可能であること
から、この支柱を台車から取り去ることにより、
水平に展開された端板、側板および頂板は障害物
のないヘリポートとなる。これにより回転翼機の
格納保管ができるのは勿論、格納庫自体が移動可
能なうえヘリポートとしての働きもなすことがで
きるようにしたものである。 The present invention provides a novel hangar that is completely different from such conventional hangars for rotary-wing aircraft, and its feature is that a rectangular parallelepiped container mounted on or towed by a vehicle is configured to be able to store rotary-wing aircraft. The top plate of the rectangular parallelepiped container is divided into two along the longitudinal dividing line, and the base end side of each top plate is rotatably connected to the upper ends of both side plates of the rectangular parallelepiped container, while,
The lower ends of both side plates and both end plates of the rectangular parallelepiped are rotatably connected to the trolley, each has a winch for deploying the connected side plates, top plate, and end plate, and both top plates can be supported by the upper end surfaces. Supporting columns for supporting and positioning the end plates at the upper end sides are removably installed at both ends of the trolley, and are wound around a winch for deploying the side plates and the top plate,
A cable is connected to the inner surface of the tip side of both top plates via a guide sheave arranged in the center of both side plates, and is wound around a winch for deploying the end plate and connected to the inner surface of the upper end of the end plate. The side plates, top plate, and end plates of the rectangular parallelepiped container are configured to be able to be deployed horizontally outward by means of the cables. According to such a device, by unwinding a cable wound around a winch for deploying the end plate, it is possible to deploy the end plate to a horizontal state. Furthermore, when the cables wound around the winch for deploying the side plates and the top plate are unwound, the cables are connected to the inner surface of the tip side of the top plate via the guide sheave arranged in the center of the side plates. These side plates and top plate are simultaneously expanded to a horizontal state. Furthermore, since the column to which the winch is attached can be inserted into and removed from the truck, by removing this column from the truck,
The horizontally deployed end plates, side plates and top plate create an unobstructed helipad. This not only allows for the storage and storage of rotary-wing aircraft, but also allows the hangar itself to be moved and also function as a helipad.
以下本発明の構成をその一実施例を示す図面に
基づいて詳細に説明する。先ず第１図〜第３図を
用いて本発明の概要を述べる。図において、１は
台車２を牽引する牽引車で、前記台車２の上には
例えば回転翼機の一つであるヘリコプター３を格
納保管する格納庫４が設けられている。格納庫４
は直方体容器で、第２図に明らかなようにその外
壁を側方に展開可能に構成されている。すなわち
格納庫頂板５を長手方向に縦中心線で二つに分割
してそれぞれの一端を格納庫両側板６に回動自在
に接続し、一方、格納庫両側板６および格納庫両
端板７の下端も台車２に回動自在に接続して展開
可能としたもので、格納庫４を展開して水平にす
ることによりヘリポートとしても兼ねることがで
きるようにしたものである。なお、格納庫４を展
開するときは、牽引車１は台車２から離脱させて
おく。図中、８は格納庫４内の両側端部に設けら
れた格納庫頂板５を支持する支柱、９は格納庫４
の一方の端板７に設けられた人が出入りするため
の扉である。 DESCRIPTION OF THE PREFERRED EMBODIMENTS The structure of the present invention will be explained in detail below based on the drawings showing one embodiment thereof. First, an outline of the present invention will be described using FIGS. 1 to 3. In the figure, reference numeral 1 denotes a towing vehicle that pulls a truck 2, and a hangar 4 is provided on the truck 2 for storing, for example, a helicopter 3, which is one type of rotary-wing aircraft. Hangar 4
is a rectangular parallelepiped container, and as shown in FIG. 2, its outer wall can be expanded laterally. That is, the hangar top plate 5 is longitudinally divided into two along the vertical center line, and one end of each is rotatably connected to the hangar side plates 6 , while the lower ends of the hangar side plates 6 and the hangar both end plates 7 are also connected to the trolley 2 . The hangar 4 can be unfolded by being rotatably connected to the hangar 4, and can also be used as a helipad by unfolding the hangar 4 and making it horizontal. Note that when the hangar 4 is deployed, the towing vehicle 1 is separated from the truck 2. In the figure, 8 is a column that supports the hangar top plate 5 provided at both ends of the hangar 4, and 9 is a support for the hangar 4.
This is a door provided on one end plate 7 for people to enter and exit.
次に第４図および第５図を用いて前記格納庫４
の具体的機構を説明する。なお、牽引車１は既に
台車２から離脱されているものとする。前記支柱
８は、台車２の両側端部に設けられたソケツト１
０に下端部を挿入して立設されており、上端面で
格納庫両頂板５を支持し、上端側部に突出して設
けられた係止部８Ａで格納庫両端板７を支持する
とともに位置決めしている。格納庫端板７および
格納庫側板６はそれぞれの下端をヒンジ１１を介
して台車２に取付けられており、格納庫側板６の
上端にはそれぞれ格納庫頂板５の一端がヒンジ１
１を介して取付けられている。そして格納庫頂板
５の他端合わせ目どおしが蝶ねじ１２で連結固定
され、また格納庫端板７の上端と格納庫両頂板５
の側端部合わせ目が蝶ねじ１２で連結固定されて
直方体容器の格納庫４が形成されている。１３は
格納庫側板６上端と格納庫頂板５一端との連結部
に取付けられたピン継手で、固定用ピン１４が挿
通されて第５図の仮想線に示すように、格納庫４
の展開時に格納庫側板６と格納庫頂板５とが90゜
の角度を保持した状態で展開し得るようにするた
めのものであり、格納庫頂板５を水平に展開する
場合は、前記固定用ピン１４を抜くと格納庫側板
６の上端および格納庫頂板５の一端に適宜形成さ
れた切欠部１５に入り込む構成とされている。前
記両支柱８には格納庫側板６および格納庫頂板５
を展開させるための手動小形ウインチ１６，１７
と格納庫端板７を展開させるための手動小形ウイ
ンチ１８とが設けられており、格納庫側板６およ
び格納庫頂板５を展開させるためのウインチ１
６，１７に巻回された索１９は、第５図に明らか
なように該ウインチ１６，１７の上方に位置して
支柱８に配設されたガイドシーブ２０および格納
庫両側板６内中央部に配設されたガイドシーブ２
０を介して格納庫両頂板５の他端部内面に連結さ
れ、一方、格納庫端板７を展開させるためのウイ
ンチ１８に巻回された索１９は、第４図に明らか
なように該ウインチ１８の上方に位置して支柱８
に配設されたガイドシーブ２０を介して格納庫端
板７の上端部内面に連結されている。なお図中、
２１は格納庫４を展開した際に、格納庫側板６、
格納庫頂板５および格納庫端板７を支持する積込
式の盤木（支柱式でもよい）、２２は適宜、格納
庫４端板に架設される梯子で、例えば蝶ねじ１２
を解除したり格納庫端板７に設けられた扉９から
出入りするとき等に使用するものである。 Next, using FIGS. 4 and 5, the hangar 4
The specific mechanism will be explained. Note that it is assumed that the towing vehicle 1 has already been detached from the truck 2. The support column 8 is connected to a socket 1 provided at both ends of the truck 2.
It is erected with the lower end inserted into 0, and supports both hangar top plates 5 on the upper end surface, and supports and positions the hangar both end plates 7 with locking parts 8A protruding from the upper end side. There is. The hangar end plate 7 and the hangar side plate 6 are attached to the truck 2 at their lower ends via hinges 11, and one end of the hangar top plate 5 is attached to the upper end of the hangar side plate 6 via the hinge 11.
It is attached via 1. The other end seam of the hangar top plate 5 is connected and fixed with thumbscrews 12, and the upper end of the hangar end plate 7 and the hangar both top plates 5
The joints of the side ends are connected and fixed with thumbscrews 12 to form a storage 4 of a rectangular parallelepiped container. Reference numeral 13 denotes a pin joint attached to the connecting portion between the upper end of the hangar side plate 6 and one end of the hangar top plate 5, through which a fixing pin 14 is inserted and the hangar 4 is inserted as shown in the imaginary line in FIG.
This is so that the hangar side plate 6 and the hangar top plate 5 can be unfolded while maintaining an angle of 90 degrees when the hangar top plate 5 is unfolded.When the hangar top plate 5 is unfolded horizontally, the fixing pin 14 is When pulled out, it is configured to fit into a notch 15 appropriately formed at the upper end of the hangar side plate 6 and one end of the hangar top plate 5. A hangar side plate 6 and a hangar top plate 5 are attached to both the pillars 8.
Small manual winches 16, 17 for deploying
and a small manual winch 18 for deploying the hangar end plate 7, and a winch 1 for deploying the hangar side plate 6 and the hangar top plate 5.
As is clear from FIG. 5, the cable 19 wound around the winches 16 and 17 is attached to a guide sheave 20 located above the winches 16 and 17 and arranged on the support column 8, and to the central part of the hangar side panels 6. Guide sheave 2 installed
4, the cable 19 is connected to the inner surface of the other end of the hangar top plate 5 through the cable 19, and is wound around the winch 18 for deploying the hangar end plate 7, as shown in FIG. Post 8 is located above the
It is connected to the inner surface of the upper end of the hangar end plate 7 via a guide sheave 20 disposed in the hangar end plate 7. In addition, in the figure,
21, when the hangar 4 is expanded, the hangar side plate 6,
A loading-type board (supporting type may be used) that supports the hangar top plate 5 and the hangar end plate 7; 22 is a ladder installed on the hangar 4 end plate, for example, a thumbscrew 12;
It is used when releasing the hangar or when entering and exiting through the door 9 provided on the end plate 7 of the hangar.
係る構成で動作を説明する。先ず第１図に示す
ように、既にヘリコプター３が本発明に係る格納
庫４に格納されている場合、必要があれば目的地
まで牽引車１で運ぶ。このとき、盤木２１も一諸
に運ぶ。そして目的地で牽引車１を台車２から離
脱する。次に、第４図および第５図の仮想線に示
すように格納庫４を展開する場合、前述の梯子２
２を用いて格納庫４に登り、各蝶ねじ１２を解除
する。次に格納庫端板７の扉９から格納庫４内に
入つて、格納庫両端板７を人力で外方に押しなが
らウインチ１８を巻出し側にゆるめる。索１９を
伸ばして格納庫端板７が水平にほぼ倒れた時点
で、地面上に置いた盤木２１を調整して確実に端
板７の重量を盤木２１に受けさせるようにする。
次いで、格納庫両側板６を人力で外方に押しなが
らウインチ１６，１７を巻出し側にゆるめ索１９
を伸ばす。そして格納庫側板６と格納庫頂板５が
90゜の角度をなして倒れてきてほぼ側板６が水平
になつた時点で、側板６の上端部に対応する位置
に置いた盤木２１を調整して確実に側板６の重量
を盤木２１に受けさせるようにする。次にピン継
手１３の固定用ピン１４を引き抜いた後、さらに
格納庫頂板５を人力で外方に押しながらウインチ
１６，１７を巻出し側にゆるめ索１９を伸ばす。
頂板５が水平になつたところで盤木２１で支持す
る。これらの展開作業が終ると、各索１９を全て
取り外し、ソケツト１０から支柱８を人力で抜き
取ることにより、格納庫４は障害物のないヘリポ
ートとなる。再び格納庫４を構成するときは、上
述と反対の手順で行なう。 The operation of this configuration will be explained. First, as shown in FIG. 1, when a helicopter 3 is already stored in a hangar 4 according to the present invention, it is transported by a towing vehicle 1 to a destination if necessary. At this time, the board 21 is also carried to Moro. Then, the towing vehicle 1 is separated from the truck 2 at the destination. Next, when deploying the hangar 4 as shown in the imaginary lines in FIGS. 4 and 5, the ladder 2 described above is
2 to climb into the hangar 4 and release each thumbscrew 12. Next, the user enters the hangar 4 through the door 9 of the hangar end plate 7, and loosens the winch 18 toward the unwinding side while manually pushing both end plates 7 of the hangar outward. When the cable 19 is stretched and the hangar end plate 7 falls down almost horizontally, the board 21 placed on the ground is adjusted to ensure that the weight of the end board 7 is received by the board 21.
Next, while manually pushing the hangar side panels 6 outward, the winches 16 and 17 are loosened to the unwinding side.
Stretch. Then, the hangar side plate 6 and the hangar top plate 5 are
When the side board 6 falls down at an angle of 90 degrees and becomes almost horizontal, adjust the board 21 placed at the position corresponding to the upper end of the side board 6 to ensure that the weight of the side board 6 is reduced to the board 21. Let them receive it. Next, after pulling out the fixing pin 14 of the pin joint 13, the hangar top plate 5 is further pushed outward by hand, and the winches 16, 17 are extended to the unwinding side to extend the loosening cable 19.
When the top plate 5 becomes horizontal, it is supported by a board 21. When these deployment operations are completed, all the cables 19 are removed and the struts 8 are manually pulled out from the sockets 10, thereby turning the hangar 4 into a helipad free of obstacles. When configuring the hangar 4 again, the procedure described above is reversed.
なお、上記実施例においては、車輌に格納庫が
牽引される形式のものを示したが、車輌に格納庫
が塔載される形式のものでもよいことは明らか
で、この場合、車輌の荷台に一体的に組み込まれ
たものでも、車輌の荷台上に載置される形状のも
のでもよい。 In the above embodiment, the hangar is towed by a vehicle, but it is clear that the hangar may be mounted on the vehicle. It may be built into a vehicle, or it may be mounted on the loading platform of a vehicle.
以上本発明によれば、次に示す効果を得ること
ができる。 As described above, according to the present invention, the following effects can be obtained.
(1) 回転翼機の格納保管ができるとともにヘリポ
ートとしての働きもなすことができる。(1) It can store rotary-wing aircraft and also function as a helipad.
(2) 陸を移動することができるので、回転翼機を
陸送するのに用いることができ、また同時にヘ
リポートを陸送できることになる。(2) Since it can move over land, it can be used to transport rotary-wing aircraft over land, and at the same time it can transport helipads over land.
(3) 回転翼機の使用地近くまで進出させてヘリポ
ートとして用いれば、回転翼機の頻繁な離着陸
が可能となり、回転翼機の使用方法の拡大を図
ることができる。(3) If rotary-wing aircraft are advanced close to the area where they are used and used as a helipad, frequent take-off and landing of rotary-wing aircraft will be possible, and the ways in which rotary-wing aircraft can be used will be expanded.
(4) 非常の際に回転翼機が避難するのを、出向い
て行つて助けることができる。(4) Be able to go out and help rotorcraft evacuate in the event of an emergency.
(5) ウインチからの索を、側板に設けたガイドシ
ーブを介して頂板に連結したため、一本の索に
より側板と頂板とを同時に開閉することができ
る。(5) Since the cable from the winch is connected to the top plate via the guide sheave provided on the side plate, the side plate and the top plate can be opened and closed simultaneously with one cable.
(6) 台車に対して側板と端板とを回動自在に接続
するとともに、側板に対して頂板を回動自在に
接続したため、これら端板、側板および頂板を
水平に展開可能となつて水平なヘリポートを容
易に構成できるのみならず、これら端板、側板
および頂板を閉動させることにより簡単に格納
庫を組立てることができる。(6) Since the side plates and end plates are rotatably connected to the cart, and the top plate is rotatably connected to the side plates, these end plates, side plates, and top plate can be deployed horizontally. Not only can a heliport be easily constructed, but also a hangar can be easily assembled by closing the end plates, side plates, and top plate.
(7) ウインチを取付けた支柱を台車に対し挿脱可
能としたため、この支柱を取り去ることにより
支柱、ウインチなどの障害物が存在しないヘリ
ポートを構成できるとともに、この支柱を台車
に挿入することにより容易に格納庫の組立、展
開が可能で、しかも支柱により格納庫としての
直方体容器を補強できる。(7) The support with the winch attached can be inserted and removed from the trolley, so by removing this support it is possible to construct a helipad without obstacles such as supports and winches, and by inserting this support into the trolley, it is easy to construct a helipad. It is possible to assemble and deploy the hangar, and the pillars can reinforce the rectangular parallelepiped container as a hangar.
図面は本発明の一実施例を示し、第１図は本発
明に係る回転翼機の格納庫の側面図、第２図は第
１図の格納庫を展開してヘリポートを形成したと
ころの平面図、第３図は格納庫の横断面図、第４
図および第５図は具体的機構を説明するための図
を示し、第４図は格納庫端部の側面図、第５図は
格納庫の正面図である。
１…牽引車、３…ヘリコプター、４…格納庫、
５…頂板、６…側板、７…端板。
The drawings show one embodiment of the present invention, and FIG. 1 is a side view of a hangar for a rotary-wing aircraft according to the present invention, and FIG. 2 is a plan view of the hangar in FIG. 1 expanded to form a helipad. Figure 3 is a cross-sectional view of the hangar;
5 and 5 are diagrams for explaining the specific mechanism, FIG. 4 is a side view of the end of the hangar, and FIG. 5 is a front view of the hangar. 1... Towing vehicle, 3... Helicopter, 4... Hangar,
5... Top plate, 6... Side plate, 7... End plate.
Claims (1)
回転翼機格納可能に構成し、前記直方体容器の頂
板を長手方向の分割線に沿つて２つに分割し、そ
れぞれの頂板の基端側を直方体容器の両側板上端
に、回動自在に接続し、一方、直方体容器の両側
板および両端板の下端を台車に回動自在に接続
し、上記接続された側板と頂板および上記端板を
展開させるためのウインチをそれぞれ有するとと
もに、その上端面で両頂板を支持可能でかつ上端
側部で端板を支持して位置決めする支柱を台車の
両側端部に挿脱可能に立設し、上記側板と頂板を
展開するためのウインチに巻回され両側板内中央
部に配設されたガイドシーブを介して両頂板の先
端側内面に連結された索と、上記端板を展開する
ためのウインチに巻回され、端板の上端部内面に
連結されている索とにより直方体容器の前記側
板、頂板および端板を外方に、水平に展開可能に
構成したことを特徴とする回転翼機の格納庫。1. A rectangular parallelepiped container mounted on or towed by a vehicle is configured to be capable of storing a rotary-wing aircraft, the top plate of the rectangular parallelepiped container is divided into two along a longitudinal dividing line, and the base end side of each top plate is formed into a rectangular parallelepiped. The upper ends of both side plates of the container are rotatably connected, while the lower ends of both side plates and both end plates of the rectangular parallelepiped container are rotatably connected to the cart, and the connected side plates, top plate, and end plate are unfolded. In addition to each having a winch for the purpose of the truck, columns capable of supporting both top plates on their upper end faces and supporting and positioning the end plates on the upper end sides are removably installed at both ends of the trolley, and A cable is wound around a winch for deploying the top plate and is connected to the inner surface of the tip side of both top plates via a guide sheave placed in the center of each side plate, and a cable is wound around a winch for deploying the end plate. A hangar for a rotary-wing aircraft, characterized in that the side plates, top plate, and end plates of the rectangular parallelepiped container are configured to be able to be deployed outward and horizontally by means of cables that are rotated and connected to the inner surface of the upper end of the end plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8846382A JPS58206434A (en) | 1982-05-24 | 1982-05-24 | Hangar for rotor craft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8846382A JPS58206434A (en) | 1982-05-24 | 1982-05-24 | Hangar for rotor craft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS58206434A JPS58206434A (en) | 1983-12-01 |
| JPS6257560B2 true JPS6257560B2 (en) | 1987-12-01 |
Family
ID=13943462
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP8846382A Granted JPS58206434A (en) | 1982-05-24 | 1982-05-24 | Hangar for rotor craft |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS58206434A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| 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 |
| 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 |
| WO2019042262A1 (en) * | 2017-08-31 | 2019-03-07 | Zhejiang Geely Holding Group Co., Ltd. | Modular flying car and flying car system and flying car sharing method |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2264593B1 (en) * | 2003-12-26 | 2008-02-01 | Tecnove, S.L. | ROAD TRANSPORTATION UNIT, OF VARIABLE VOLUMETRY. |
| ES2417280B1 (en) * | 2011-12-30 | 2014-06-09 | Eleuterio SANSALONI REIG | TOWING APPLICABLE TO LANDING; TAKEOFF; STORAGE AND TRANSPORTATION OF HELICOPTERS |
| CN106476672B (en) * | 2016-11-11 | 2019-02-12 | 成都创奇汽车制造有限公司 | A kind of semitrailer with hoistable platform |
| CN112644359B (en) * | 2021-02-20 | 2023-07-14 | 湖北博利特种汽车装备股份有限公司 | Be used for unmanned aerial vehicle's crane on fire engine |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4082240A (en) * | 1976-08-23 | 1978-04-04 | General Dynamics Corporation | Continuous integrated clamping hoop space vehicle support system |
| US4171114A (en) * | 1976-09-02 | 1979-10-16 | Marden Jay W | Mobile aerial support system |
-
1982
- 1982-05-24 JP JP8846382A patent/JPS58206434A/en active Granted
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4082240A (en) * | 1976-08-23 | 1978-04-04 | General Dynamics Corporation | Continuous integrated clamping hoop space vehicle support system |
| US4171114A (en) * | 1976-09-02 | 1979-10-16 | Marden Jay W | Mobile aerial support system |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| 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 |
| 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 |
| WO2019042262A1 (en) * | 2017-08-31 | 2019-03-07 | Zhejiang Geely Holding Group Co., Ltd. | Modular flying car and flying car system and flying car sharing method |
| US11661127B2 (en) | 2017-08-31 | 2023-05-30 | Zhejiang Geely Holding Group Co., Ltd. | Modular ground vehicle and flight vehicle sharing system |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS58206434A (en) | 1983-12-01 |
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