CN106976544A - A kind of airship gondola structure - Google Patents
A kind of airship gondola structure Download PDFInfo
- Publication number
- CN106976544A CN106976544A CN201710124655.3A CN201710124655A CN106976544A CN 106976544 A CN106976544 A CN 106976544A CN 201710124655 A CN201710124655 A CN 201710124655A CN 106976544 A CN106976544 A CN 106976544A
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- CN
- China
- Prior art keywords
- gondola
- horizontal load
- load frame
- floor panel
- panel assembly
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- 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.)
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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
- B64B1/22—Arrangement of cabins or gondolas
-
- 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
- B64B1/24—Arrangement of propulsion plant
- B64B1/28—Arrangement of propulsion plant housed in nacelles
-
- 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
- B64B1/24—Arrangement of propulsion plant
- B64B1/30—Arrangement of propellers
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
Abstract
The present invention relates to a kind of airship gondola structure, including horizontal load frame, floor panel assembly, winglet, alien invasion and cabin top；The top of the horizontal load frame is connected with the overhanging structural member of air bag, and the height of bottom i shaped cross section is flushed with floor panel assembly, and horizontal load frame constitutes the power transmission skeleton of gondola with floor panel assembly；The winglet is arranged on gondola both sides, as the external-hanging structure of gondola, and motor mounts, cowling, propeller protection ring and engine system are installed on winglet；The alien invasion is arranged on horizontal load frame and floor panel assembly periphery, and support, fixation are played for the power transmission skeleton to horizontal load frame and floor panel assembly composition；The top profile on the cabin top is consistent with the cambered surface of air bag.Safety of the invention, comfortable, the width and height of the horizontal load frame of increase, you can produce spacious inner space；Taken photo by plane and in emergency circumstances military, civilian goods and materials of air transportation etc. available for the going sightseeing of aviation program, major holiday is managed.
Description
Technical field
The invention belongs to aircraft frame field of structural design, and in particular to a kind of airship gondola structure.
Background technology
Dirigible is the aerostatics with Powerpush Unit, with hovering ability, save the energy, cruising time length,
The advantages of voyage is remote, payload capacity is big, there is good the army and the people's application prospect.Gondola is the important component of dirigible, is winged
Ship completes the platform of functional task.The design requirement of gondola be proof strength, rigidity meet require under, weight try one's best gently, from
And effective mission payload can be increased or floatoblast volume is reduced.
Existing airship gondola uses simple steel welding construction hanging basket mostly, interior for taking photo by plane, imaging and delivering advertisement etc.
Portion's narrow space, comfortableness is poor, California bearing ratio inefficiency.
The content of the invention
The problem of it is an object of the invention to exist for prior art there is provided one kind collection comfortableness, security and efficiently
Load-carrying properties are in the airship gondola structure of one.
The technical scheme for realizing the object of the invention is：A kind of airship gondola structure, including horizontal load frame, floor panel assembly,
Winglet, alien invasion and cabin top；
The top of the horizontal load frame is connected with the overhanging structural member of air bag, height and the floor group of bottom i shaped cross section
Part is flushed, and horizontal load frame constitutes the power transmission skeleton of gondola with floor panel assembly；
The winglet is arranged on gondola both sides, as the external-hanging structure of gondola, motor mounts, cowling,
Propeller protection ring and engine system are installed on winglet；
The alien invasion is arranged on horizontal load frame and floor panel assembly periphery, for horizontal load frame and floor panel assembly group
Into power transmission skeleton play support and fixation；
The top profile on the cabin top is consistent with the cambered surface of air bag bottom.
Compared with prior art, remarkable advantage of the invention is：(1) efficient California bearing ratio, structure for pod weight is with effectively appointing
The ratio between business load reaches 1：4；(2) Modular Structure Design, can be achieved the longitudinal dilatation of gondola；(3) winglet is variable cross-section overhanging beam
Space truss structure；(4) spacious inner space；(5) safety, comfortableness are high.
Brief description of the drawings
Fig. 1 is the gondola power transmission skeleton structure diagram that 3 horizontal load frames and floor panel assembly are constituted.
Fig. 2 is the gondola power transmission skeleton structure diagram that 2 horizontal load frames and floor panel assembly are constituted.
Fig. 3 is horizontal load mount structure figure.
Fig. 4 is winglet structural representation.
Fig. 5 is alien invasion structural representation.
Fig. 6 is dirigible structure chart.
Fig. 7 is structure for pod figure.
Embodiment
A kind of airship gondola structure of the present invention, including horizontal load frame 1, floor panel assembly 2, winglet, alien invasion and cabin top；
The top of the horizontal load frame 1 is connected with the overhanging structural member of air bag, the height of bottom i shaped cross section and floor
Component 2 is flushed；Horizontal load frame 1 constitutes the power transmission skeleton of gondola with floor panel assembly 2；
The winglet is arranged on gondola both sides, is used as the external-hanging structure of gondola, motor mounts 3, cowling
4th, propeller protection ring 5 and engine system are installed on winglet；
The alien invasion is arranged on horizontal load frame and floor panel assembly periphery, for horizontal load frame and floor panel assembly group
Into power transmission skeleton play support and fixation；
The top profile on the cabin top is consistent with the cambered surface of air bag bottom.
Further, the floor panel assembly in latticed vertically and horizontally component by constituting, floor panel assembly longitudinal member and horizontal stroke
Connected to load frame.
Further, the alien invasion is made up of gondola wallboard, bulkhead and longitudinal reinforcer, and the bulkhead is arranged on transverse direction
Between load frame, the longitudinal reinforcer is arranged on gondola wallboard.
Further, the alien invasion is additionally provided with door and window.
The invention will be further described below in conjunction with the accompanying drawings.
With reference to Fig. 1-Fig. 5, structure for pod of the invention is mainly made up of following part：
(1) horizontal load frame.The closed loop configuration that horizontal load frame is made up of frame section according to gondola cross sectional shape；Laterally hold
The size of power frame is determined that the top slot milling of load frame is connected with the overhanging structural member of air bag, bottom work by gondola contour shape
The height in font section is flushed with floor panel assembly.
(2) floor panel assembly.Arbitrarily walked on floor for ease of pedestrian, bear the inertial loads such as seat, equipment and fuel tank,
And the load that engine is transmitted by winglet is born, underfloor supporting construction must have enough rigidity.Floor panel assembly by
Constituted in latticed vertically and horizontally component.
2 horizontal load frames and floor panel assembly are 1 complete structure function module.Gondola is external-hanging structure, passes through horizontal stroke
It is connected to the top 6 of load frame with the overhanging structural member of air bag, floor panel assembly longitudinal member is connected with the bottom of horizontal load frame.It is horizontal
The power transmission skeleton of gondola is constituted to load frame and floor panel assembly, is born caused by inertial load, and inertia and shock loading etc.
Moment of flexure, moment of torsion.
(3) winglet.Winglet is the external-hanging structure of gondola.Motor mounts, cowling, propeller protection ring and
Engine system is installed on winglet, carries the inertial load of all parts mounted thereon and pushing away for engine generation
Power.
(4) alien invasion.Alien invasion is made up of gondola wallboard, bulkhead and longitudinal reinforcer, to horizontal load frame and floor group
The power transmission skeleton of part composition plays support, fixation.According to stress needs, bulkhead, Yi Ji are arranged between horizontal load frame
Gondola wallboard arranges longitudinal reinforcer, increases the integral rigidity and local stiffness of gondola wallboard, prevents gondola wallboard from occurring local
Unstability.Carrying surface internal volume forms good masking environment, can door window as needed.
(5) cabin is pushed up.It is consistent with the cambered surface of air bag at the top of gondola to ensure, from rigidity at the top of technique manufacturing, increase gondola
Consider with aesthetic property angle, the bent top of increase by one in the design of gondola top of panels, it is ensured that the integrality of structure for pod.
(6) door and window.The position of horizontal load frame, common bulkhead and alien invasion longitudinal reinforcer is not influenceed in alien invasion,
The supplementary structures such as door, window are set, is easy to high-altitude tourism, takes photo by plane.And in driving cabin and main cabin, main cabin and equipment compartment, equipment compartment
Cut-off OR gate is set between fuel tank, increases sectoring function.
With reference to specific embodiment, the invention will be further described.
Embodiment
The present embodiment is a kind of 8 composite airship gondolas.
According to the load of 8 airship gondolas, agent structure is defined as 3 horizontal load frame+floor panel assemblies, as shown in Figure 1.
Fig. 3 is horizontal load frame, is made up of aviation laminate or fiberglass epoxy plate or paulownia timber.Floor panel assembly is by vertically and horizontally component groups
Into longitudinal member can use honeycomb sandwich construction using double honeycomb sandwich constructions or aviation laminate, cross member.
As shown in figure 4, the winglet of gondola both sides is the space truss structure of variable cross-section overhanging beam, welded using common iron
Form, be connected by 4 metal joints with the joint on gondola.Joint height is flushed with car floor component, with minimum knot
Structure deadweight realizes the transmission to the moment of flexure produced by engine inertia load and motor power, shearing and moment of torsion.Engine
Mounting bracket, cowling, propeller protection ring and engine system are installed on winglet.
Alien invasion is made up of gondola wallboard, bulkhead and longitudinal reinforcer, gondola wallboard is divided to or so two wallboards, such as Fig. 5 institutes
Show, production breakdown interface is in the centre position of nacelle, and wallboard cavity plate is that can be used as finishing die, also can as gondola assembly tooling.
Wallboard uses honeycomb sandwich construction, according to structure stress needs, is being longitudinally arranged foam reinforcement, and horizontal load frame it
Between arrange bulkhead.Cabin is pushed up pushes up according to the song of airbag shape, and cabin top forms overall structure by splicing with gondola flat-top.Outside
The suitable place of facade is provided with door, window, and cooperation is taken photo by plane using needs, and active window is arranged on alien invasion.Inside gondola, layout
Separate OR gate, carry out function division.Fig. 6 is dirigible structure chart, and Fig. 7 is the gondola overall structure figure of the present embodiment.
The foregoing is only a preferred embodiment of the present invention, protection scope of the present invention not limited to this, any ripe
Those skilled in the art is known in the technical scope of present disclosure, the letter for the technical scheme that can be become apparent to
Altered or equivalence replacement are each fallen within protection scope of the present invention as certain technical scheme portion of techniques.
Claims (4)
1. a kind of airship gondola structure, it is characterised in that including horizontal load frame (1), floor panel assembly (2), winglet, alien invasion and
Push up in cabin；
The top of the horizontal load frame (1) is connected with the overhanging structural member of air bag, height and the floor group of bottom i shaped cross section
Part (2) is flushed, and horizontal load frame (1) constitutes the power transmission skeleton of gondola with floor panel assembly (2)；
The winglet is arranged on gondola both sides, is used as the external-hanging structure of gondola, motor mounts (3), cowling
(4), propeller protection ring (5) and engine system are installed on winglet；
The alien invasion is arranged on horizontal load frame and floor panel assembly periphery, for what is constituted to horizontal load frame and floor panel assembly
Power transmission skeleton plays support and fixation；
The top profile on the cabin top is consistent with the cambered surface of air bag bottom.
2. airship gondola structure according to claim 1, it is characterised in that the floor panel assembly by it is latticed in length and breadth
Constituted to component, floor panel assembly longitudinal member is connected with horizontal load frame.
3. airship gondola structure according to claim 1, it is characterised in that the alien invasion by gondola wallboard, bulkhead and
Longitudinal reinforcer is constituted, and the bulkhead is arranged between horizontal load frame, and the longitudinal reinforcer is arranged on gondola wallboard.
4. airship gondola structure according to claim 3, it is characterised in that the alien invasion is additionally provided with door and window.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710124655.3A CN106976544A (en) | 2017-03-03 | 2017-03-03 | A kind of airship gondola structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710124655.3A CN106976544A (en) | 2017-03-03 | 2017-03-03 | A kind of airship gondola structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106976544A true CN106976544A (en) | 2017-07-25 |
Family
ID=59338682
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710124655.3A Pending CN106976544A (en) | 2017-03-03 | 2017-03-03 | A kind of airship gondola structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106976544A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108482632A (en) * | 2018-03-12 | 2018-09-04 | 山东东晟飞艇科技有限公司 | A kind of rigid airship |
| 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 |
| CN109552590A (en) * | 2018-12-26 | 2019-04-02 | 广州拓浪智能应急科技有限公司 | A kind of dirigible |
| CN114148501A (en) * | 2021-12-03 | 2022-03-08 | 中国特种飞行器研究所 | Solar electric airship |
| CN114313205A (en) * | 2021-12-30 | 2022-04-12 | 中国特种飞行器研究所 | Manned airship nacelle made of composite materials and having non-mechanically-connected single-layer wall plate structure |
| CN116534266A (en) * | 2023-07-06 | 2023-08-04 | 中国电子科技集团公司第二十九研究所 | Airborne high-rigidity and lightweight electronic nacelle body and assembly method |
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| CN2895243Y (en) * | 2006-05-16 | 2007-05-02 | 河南送变电建设公司 | Remote control boat seaplane |
| KR20100100106A (en) * | 2009-03-05 | 2010-09-15 | 이청주 | Airline for advertisements using a hot-air balloon |
| CN102241274A (en) * | 2011-04-08 | 2011-11-16 | 祝永刚 | Multifunctional interlayer air sac airship |
| CN104652853A (en) * | 2015-01-12 | 2015-05-27 | 南京航空航天大学 | Quick lifting installation building structure |
| CN204507243U (en) * | 2014-10-21 | 2015-07-29 | 深圳光启空间技术有限公司 | Gondola and there is its aircraft |
| CN205239885U (en) * | 2015-12-25 | 2016-05-18 | 深圳光启空间技术有限公司 | Airship |
| RU2604914C2 (en) * | 2015-05-06 | 2016-12-20 | Федеральное государственное казенное военное образовательное учреждение высшего профессионального образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации | Airborne early warning airship |
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Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2895243Y (en) * | 2006-05-16 | 2007-05-02 | 河南送变电建设公司 | Remote control boat seaplane |
| KR20100100106A (en) * | 2009-03-05 | 2010-09-15 | 이청주 | Airline for advertisements using a hot-air balloon |
| CN102241274A (en) * | 2011-04-08 | 2011-11-16 | 祝永刚 | Multifunctional interlayer air sac airship |
| CN204507243U (en) * | 2014-10-21 | 2015-07-29 | 深圳光启空间技术有限公司 | Gondola and there is its aircraft |
| CN104652853A (en) * | 2015-01-12 | 2015-05-27 | 南京航空航天大学 | Quick lifting installation building structure |
| RU2604914C2 (en) * | 2015-05-06 | 2016-12-20 | Федеральное государственное казенное военное образовательное учреждение высшего профессионального образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации | Airborne early warning airship |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108482632A (en) * | 2018-03-12 | 2018-09-04 | 山东东晟飞艇科技有限公司 | A kind of rigid airship |
| 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 |
| CN109552590A (en) * | 2018-12-26 | 2019-04-02 | 广州拓浪智能应急科技有限公司 | A kind of dirigible |
| CN114148501A (en) * | 2021-12-03 | 2022-03-08 | 中国特种飞行器研究所 | Solar electric airship |
| CN114313205A (en) * | 2021-12-30 | 2022-04-12 | 中国特种飞行器研究所 | Manned airship nacelle made of composite materials and having non-mechanically-connected single-layer wall plate structure |
| CN114313205B (en) * | 2021-12-30 | 2024-04-09 | 中国特种飞行器研究所 | Manned airship nacelle made of composite material and free of mechanical connection and having single-layer wallboard structure |
| CN116534266A (en) * | 2023-07-06 | 2023-08-04 | 中国电子科技集团公司第二十九研究所 | Airborne high-rigidity and lightweight electronic nacelle body and assembly method |
| CN116534266B (en) * | 2023-07-06 | 2024-01-05 | 中国电子科技集团公司第二十九研究所 | Airborne high-rigidity and lightweight electronic nacelle body and assembly method |
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| 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: 20170725 |
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| RJ01 | Rejection of invention patent application after publication |