CN108482632A - A kind of rigid airship - Google Patents
A kind of rigid airship Download PDFInfo
- Publication number
- CN108482632A CN108482632A CN201810198509.XA CN201810198509A CN108482632A CN 108482632 A CN108482632 A CN 108482632A CN 201810198509 A CN201810198509 A CN 201810198509A CN 108482632 A CN108482632 A CN 108482632A
- Authority
- CN
- China
- Prior art keywords
- main body
- hull
- frame
- rigid airship
- lower main
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/08—Framework construction
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/20—Rigid airships; Semi-rigid airships provided with wings or stabilising surfaces
Abstract
The invention discloses a kind of rigid airships, including hull, tailplane, vertical tail, engine nacelle, cockpit, cargo hold and with the gondola on chassis, the hull be in the form of relative to the symmetrical solid in middle part made of and along the horizontal plane of upper main body and lower main body conjugation form, the cross section of lower main body is connected to the shape that main body forms isosceles trapezoid, the side outer inclination face of lower main body is main body sidewall, and main body wall is angled inwardly into the vertical direction of hull and is combined with upper main body；The upper main body and lower main body are made of frame and the longeron on frame respectively, and covering is coated on frame；The configuration of the present invention is simple, manufacturing cost is low, reduces drift and inclined intensity, the result obtained in test in crosswind and confirms expected design value, the aerodynamic coefficient of power and torque, which improves, so that dirigible is more stable under the influence of close to the beam wind on ground, will be enlarged by its use scope.
Description
Technical field
The present invention relates to vehicle technology field, specifically a kind of rigid airship.
Background technology
Technically rational project is neat in the 19th-century Russian scientist eighties to first of Large freight dirigible
The design of Ao Er Koffskies.Different from his coeval many people, it is vertical that Tsiolkovsky proposes to build up to 500,000
The dirigible of square rice, even if by being also huge from the point of view of the standard of today, this is a difficult task.At that time due to many accidents
Reason can not successfully build a dirigible, and not only in the former Soviet Union, in Britain, all dirigibles are all paralysed in the world.Famous DS-
H1 dirigibles, skeleton include frame and longeron and covering, horizontal and vertical empennage, enging cabin, crew module, cargo hold.Hard shell
It is made of lighter firmer composite material.
Existing rigid airship is complicated, and manufacturing cost is high, and dirigible is unstable under the influence of close to the beam wind on ground,
To limit the application of rigid airship.
Invention content
The purpose of the present invention is to provide a kind of rigid airships, to solve the problems mentioned in the above background technology.
To achieve the above object, the present invention provides the following technical solutions：
A kind of rigid airship, including hull, tailplane, vertical tail, engine nacelle, cockpit, cargo hold and with chassis
Gondola, the hull be in the form of relative to the symmetrical solid in middle part made of and along the level of upper main body and lower main body
The cross section of face conjugation composition, lower main body is connected to the shape that main body forms isosceles trapezoid, the side outer inclination of lower main body
Face is main body sidewall, and main body wall is angled inwardly into the vertical direction of hull and is combined with upper main body；The upper main body is under
Main body is made of frame and the longeron on frame respectively, and covering is coated on frame.
As a further solution of the present invention：The upper main body accounts for a semi-area of hull.
As further scheme of the invention：The chassis is wheeled.
As further scheme of the invention：The chassis is located at the end of gondola.
As further scheme of the invention：The cargo hold is installed on the longitudinal axis of hull equipped at least
One cargo hatch.
As further scheme of the invention：The vertical tail is mounted on the end of tailplane.
As further scheme of the invention：The vertical tail is covered by hull.
Compared with prior art, the beneficial effects of the invention are as follows：The configuration of the present invention is simple, manufacturing cost is low, reduces in side
Drift and inclined intensity, the result obtained in test confirm expected design value, the aerodynamics of power and torque in wind
Coefficient, which improves, so that dirigible is more stable under the influence of close to the beam wind on ground, will be enlarged by its use scope.
Description of the drawings
Fig. 1 is a kind of schematic front view of rigid airship；
Fig. 2 is the schematic top plan view of the rigid airship described in Fig. 1；
Fig. 3 is the left view schematic diagram of the rigid airship described in Fig. 1.
Specific implementation mode
The technical solution of this patent is described in more detail With reference to embodiment.
Please refer to Fig.1-3, a kind of rigid airship, including hull, tailplane 1, vertical tail 2, engine nacelle 3, seat
Cabin 4, cargo hold 5 and the gondola 6 with chassis 7, the hull be in the form of relative to the symmetrical solid in middle part made of simultaneously
And be conjugated and form along the horizontal plane of upper main body 8 and lower main body 11, the cross section of lower main body 11 is connected to main body 8 and forms isosceles ladder
The side outer inclination face of the shape of shape, lower main body 11 is main body sidewall 12, and main body wall 12 is angled inwardly into the vertical of hull
Direction is simultaneously combined with upper main body 8；The upper main body 8 and lower main body 11 the longeron group by frame 9 and installation on the frame 9 respectively
At being coated with covering 10 on frame 9.
The upper main body 8 accounts for a semi-area of hull.
The chassis 7 is wheeled.
The chassis 7 is located at the end of gondola 6.
The cargo hold 5 is installed on the longitudinal axis of hull equipped at least one cargo hatch 13.
The vertical tail 2 is mounted on the end of tailplane.
The vertical tail 2 is covered by hull.
Operation principle：The configuration of the present invention is simple, manufacturing cost is low, reduces drift and inclined intensity in crosswind, test
The result of middle acquisition confirms that expected design value, the aerodynamic coefficient improvement of power and torque make dirigible close to ground
Beam wind under the influence of it is more stable, will be enlarged by its use scope.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " setting ", " phase
Even " and " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；
It can be directly connected, can also can be indirectly connected through an intermediary the connection inside two elements.For this field
Those of ordinary skill for, the concrete meaning of above-mentioned term in the present invention can be understood with concrete condition.
It is obvious to a person skilled in the art that invention is not limited to the details of the above exemplary embodiments, Er Qie
In the case of without departing substantially from spirit or essential attributes of the invention, the present invention can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the present invention is by appended power
Profit requires rather than above description limits, it is intended that all by what is fallen within the meaning and scope of the equivalent requirements of the claims
Variation is included within the present invention.Any reference signs in the claims should not be construed as limiting the involved claims.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiment being appreciated that.
Claims (7)
1. a kind of rigid airship, including hull, tailplane (1), vertical tail (2), engine nacelle (3), cockpit (4), goods
Cabin (5) and the gondola (6) for carrying chassis (7), which is characterized in that the hull is with the shape relative to the symmetrical solid in middle part
It is conjugated made of formula and along the horizontal plane of upper main body (8) and lower main body (11) and forms, the cross section of lower main body (11) is connected to
Upper main body (8) forms the shape of isosceles trapezoid, and the side outer inclination face of lower main body (11) is main body sidewall (12), main body wall
(12) it is angled inwardly into the vertical direction of hull and is combined with upper main body (8)；The upper main body (8) and lower main body (11) are respectively
It is made of frame (9) and the longeron on frame (9), covering (10) is coated on frame (9).
2. rigid airship according to claim 1, which is characterized in that the upper main body (8) accounts for a semi-area of hull.
3. rigid airship according to claim 1, which is characterized in that the chassis (7) is wheeled.
4. rigid airship according to claim 1, which is characterized in that the chassis (7) is located at the end of gondola (6).
5. rigid airship according to claim 1, which is characterized in that longitudinal axis of the cargo hold (5) perpendicular to hull
Upper installation is equipped at least one cargo hatch (13).
6. rigid airship according to claim 1, which is characterized in that the vertical tail (2) is mounted on tailplane
End.
7. rigid airship according to claim 6, which is characterized in that the vertical tail (2) is covered by hull.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810198509.XA CN108482632A (en) | 2018-03-12 | 2018-03-12 | A kind of rigid airship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810198509.XA CN108482632A (en) | 2018-03-12 | 2018-03-12 | A kind of rigid airship |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108482632A true CN108482632A (en) | 2018-09-04 |
Family
ID=63338314
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810198509.XA Pending CN108482632A (en) | 2018-03-12 | 2018-03-12 | A kind of rigid airship |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108482632A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109131820A (en) * | 2018-10-15 | 2019-01-04 | 金陵科技学院 | Composite material is without the double-deck wall panel structure airship gondola of mechanical connection large scale low cost |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2165098Y (en) * | 1993-04-21 | 1994-05-18 | 辽宁八达高校科技开发集团 | Aircraft |
| US6290176B1 (en) * | 1998-10-09 | 2001-09-18 | Airship Management Services, Inc. | Airship gondola suspension system and method of making same |
| US20030141410A1 (en) * | 2000-05-12 | 2003-07-31 | Marc Senepart | Dirigible balloon rigidified by helium tanks |
| WO2014120041A1 (en) * | 2013-02-01 | 2014-08-07 | Общество с ограниченной ответственностью ОКБ "АТЛАНТ" | Rigid airship |
| CN105059524A (en) * | 2015-07-29 | 2015-11-18 | 骆银成 | Micropower hovering recreational vehicle |
| CN106976544A (en) * | 2017-03-03 | 2017-07-25 | 南京航空航天大学 | A kind of airship gondola structure |
-
2018
- 2018-03-12 CN CN201810198509.XA patent/CN108482632A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2165098Y (en) * | 1993-04-21 | 1994-05-18 | 辽宁八达高校科技开发集团 | Aircraft |
| US6290176B1 (en) * | 1998-10-09 | 2001-09-18 | Airship Management Services, Inc. | Airship gondola suspension system and method of making same |
| US20030141410A1 (en) * | 2000-05-12 | 2003-07-31 | Marc Senepart | Dirigible balloon rigidified by helium tanks |
| WO2014120041A1 (en) * | 2013-02-01 | 2014-08-07 | Общество с ограниченной ответственностью ОКБ "АТЛАНТ" | Rigid airship |
| CN105059524A (en) * | 2015-07-29 | 2015-11-18 | 骆银成 | Micropower hovering recreational vehicle |
| CN106976544A (en) * | 2017-03-03 | 2017-07-25 | 南京航空航天大学 | A kind of airship gondola structure |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109131820A (en) * | 2018-10-15 | 2019-01-04 | 金陵科技学院 | Composite material is without the double-deck wall panel structure airship gondola of mechanical connection large scale low cost |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180904 |
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| RJ01 | Rejection of invention patent application after publication |