CN109131823A - A kind of gyroplane casing - Google Patents
A kind of gyroplane casing Download PDFInfo
- Publication number
- CN109131823A CN109131823A CN201811110856.9A CN201811110856A CN109131823A CN 109131823 A CN109131823 A CN 109131823A CN 201811110856 A CN201811110856 A CN 201811110856A CN 109131823 A CN109131823 A CN 109131823A
- Authority
- CN
- China
- Prior art keywords
- shell
- chair
- front stall
- gyroplane
- cockpit
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Special Chairs (AREA)
Abstract
A kind of gyroplane casing belongs to gyroplane technical field, including shell, windshield, front stall chair with back, back seat chair with back, handrail and cockpit reinforcing rib.Housing head has step, and windshield is mounted on stepped locations, and the arcwall face of windshield and the arcwall face of housing head fit closely；Housing central section is equipped with front stall chair with back and back seat chair with back, and the back side of front stall chair with back is equipped with handrail；Cockpit reinforcing rib is mounted in shell, and cockpit reinforcing rib surface is similar to slab construction.The front stall chair with back back side is equipped with instrument board；Shell has air inlet, and air inlet is equipped with the triangle flap of hollow out；Shell band organic oil inspection socket；Guardrail is installed, positioned at the two sides of back seat chair with back, one end is mounted on shell by hinge, and the other end is placed in front stall chair with back lock, when opening, is rotated using hinge plane normal as axis, goes to hull outside on shell.The configuration of the present invention is simple, multiple functional, safety coefficient is high, convenient for disassembly and assembly convenient for safeguarding.
Description
Technical field
A kind of gyroplane casing belongs to gyroplane technical field more particularly to a kind of gyroplane casing.
Background technique
With the continuous research and development of low flyer, more and more attention has been paid to so that more and more for gyroplane
People learns gyroplane flight, and there are also more clients to purchase gyroplane, and the casing of gyroplane is the important composition of gyroplane
Part, but also need to improve in existing casing structure and engine cool problem.The reinforcing rib of traditional rotor machine casing is
It is semicircle rod-shaped, it feels ill when passenger is stepped on foot.
Summary of the invention
The purpose of the present invention is overcoming the above-mentioned deficiency of traditional rotor machine casing structure, a kind of gyroplane casing is invented.
A kind of gyroplane casing, including shell, windshield, front stall chair with back, back seat chair with back, handrail and cockpit reinforcing rib.
The housing head has step, and windshield is mounted on stepped locations, the arcwall face and housing head of windshield
Arcwall face fit closely, contact area is big, and by the screw installation fix；The housing central section is equipped with front stall back
The back side of chair and back seat chair with back, the front stall chair with back is equipped with handrail；The cockpit reinforcing rib is mounted in shell, cockpit reinforcing rib
For arch, surfacing puts foot convenient for passenger.
Preferably, the front stall chair with back back side is equipped with instrument board, ginseng when convenient for positioned at passenger's observation flight of back seat
Number is convenient for training and teaching, and enhance passenger seizes the opportunity experience.
Preferably, the shell also has air inlet, and the air inlet positioned at back seat chair with back two sides behind is equipped with the three of hollow out
Angular flap improves the diversion effect of shell, accelerates engine cool；And be also convenient in the production process to shell into
Row demoulding.
Preferably, the shell also band organic oil inspection socket, facilitates inspection engine oil quantity.
Preferably, guardrail is installed on the shell, positioned at the two sides of back seat chair with back, one end is mounted on shell by hinge
On, the other end is placed in front stall chair with back lock, when needing to open, is rotated using hinge plane normal as axis, goes to shell
Outside.
A kind of gyroplane casing structure of the present invention is simple, multiple functional, safety coefficient is high, convenient for disassembly and assembly convenient for safeguarding.
Detailed description of the invention
Fig. 1 is a kind of schematic perspective view of gyroplane casing of the present invention；Fig. 2 is a kind of gyroplane casing of the present invention
Overlooking structure diagram；Fig. 3 is a kind of side structure schematic view of gyroplane casing of the present invention.
In figure, 1- shell, 2- windshield, 3- front stall chair with back, 4- back seat chair with back, 5- air inlet, 6- fuel oil inspection socket, 7-
Instrument board, 8- handrail, 9- guardrail, 10- cockpit reinforcing rib.
Specific embodiment
The present invention is illustrated referring now to attached drawing.
A kind of gyroplane casing, including shell 1, windshield 2, front stall chair with back 3, back seat chair with back 4, handrail 8 and cockpit add
Strengthening tendons 10.
There is step on 1 head of shell, and windshield 2 is mounted on stepped locations, the arcwall face and shell 1 of windshield 2
The arcwall face on head fits closely, and contact area is big, and is fixed by screw installation；It is equipped in the middle part of the shell 1
The back side of front stall chair with back 3 and back seat chair with back 4, the front stall chair with back 3 is equipped with handrail 8；The cockpit reinforcing rib 10 is mounted on shell 1
Interior, cockpit reinforcing rib 10 is arch, and surfacing puts foot convenient for passenger.3 back side of front stall chair with back is equipped with instrument board 7,
Positioned at back seat passenger can observation flight when parameter, be convenient for training and teaching, enhance passenger seizes the opportunity experience.The shell 1
Air inlet 5 is also had, 4 two sides behind of back seat chair with back is located at, air inlet 5 is equipped with the triangle flap of hollow out, improves shell 1
Diversion effect, accelerate engine cool；And it is also convenient for demoulding shell 1 in the production process.The shell 1 goes back band
Organic oil inspection socket 6 facilitates inspection engine oil quantity.Guardrail 9 is installed on the shell 1, positioned at the two sides of back seat chair with back 4, one
End is mounted on shell 1 by hinge, and the other end is placed in the lock of front stall chair with back 3, when needing to open, is with hinge plane normal
Axis is rotated, and 1 outside of shell is gone to.
Claims (5)
1. a kind of gyroplane casing, it is characterised in that: including shell (1), windshield (2), front stall chair with back (3), back seat chair with back
(4), handrail (8) and cockpit reinforcing rib (10)；There is step on shell (1) head, and windshield (2) is mounted on stepped locations, keeps out the wind
The arcwall face of glass (2) and the arcwall face on shell (1) head fit closely；Be equipped in the middle part of shell (1) front stall chair with back (3) and after
The back side of seat chair with back (4), the front stall chair with back (3) is equipped with handrail (8)；The cockpit reinforcing rib (10) is mounted in shell (1),
Cockpit reinforcing rib (10) is arch, surfacing.
2. a kind of gyroplane casing according to claim 1, it is characterised in that: front stall chair with back (3) back side is equipped with instrument
Disk (7).
3. a kind of gyroplane casing according to claim 1, it is characterised in that: shell (1) also has air inlet (5), position
In back seat chair with back (4) two sides behind, air inlet (5) is equipped with the triangle flap of hollow out.
4. a kind of gyroplane casing according to claim 1 or 2 or 3, it is characterised in that: shell (1) is also examined with organic oil
Look into mouth (6).
5. a kind of gyroplane casing according to claim 1 or 2 or 3, it is characterised in that: shell is equipped with guardrail on (1)
(9), it is located at the two sides of back seat chair with back (4), one end is mounted on shell (1) by hinge, and the other end is placed in front stall chair with back (3) lock
In button.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811110856.9A CN109131823A (en) | 2018-09-21 | 2018-09-21 | A kind of gyroplane casing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811110856.9A CN109131823A (en) | 2018-09-21 | 2018-09-21 | A kind of gyroplane casing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109131823A true CN109131823A (en) | 2019-01-04 |
Family
ID=64823118
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811110856.9A Withdrawn CN109131823A (en) | 2018-09-21 | 2018-09-21 | A kind of gyroplane casing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109131823A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN119408691A (en) * | 2024-10-16 | 2025-02-11 | 中国直升机设计研究所 | A tandem helicopter cockpit with variable configuration |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040099766A1 (en) * | 2002-11-27 | 2004-05-27 | Pratt John H. | Aircraft passenger seat with seat back control array |
| DE102009038509A1 (en) * | 2009-08-25 | 2011-03-03 | Modular Flying Concepts Gmbh | Base body for aircraft, has fixing unit and controlling unit for controlling of rowing elements, where base body is provided with aerodynamic form and openings |
| CN204210731U (en) * | 2014-01-03 | 2015-03-18 | 苏桂滨 | Autogyro |
| CN204750472U (en) * | 2015-07-03 | 2015-11-11 | 湖北工业大学 | Frame formula boat tractor hull |
| CN107792356A (en) * | 2017-09-28 | 2018-03-13 | 宝鸡欧亚化工设备制造厂 | One kind takes off vertically type gyroplane |
| CN209037832U (en) * | 2018-09-21 | 2019-06-28 | 湖南湘晨飞机工业有限公司 | A kind of gyroplane casing |
-
2018
- 2018-09-21 CN CN201811110856.9A patent/CN109131823A/en not_active Withdrawn
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040099766A1 (en) * | 2002-11-27 | 2004-05-27 | Pratt John H. | Aircraft passenger seat with seat back control array |
| DE102009038509A1 (en) * | 2009-08-25 | 2011-03-03 | Modular Flying Concepts Gmbh | Base body for aircraft, has fixing unit and controlling unit for controlling of rowing elements, where base body is provided with aerodynamic form and openings |
| CN204210731U (en) * | 2014-01-03 | 2015-03-18 | 苏桂滨 | Autogyro |
| CN204750472U (en) * | 2015-07-03 | 2015-11-11 | 湖北工业大学 | Frame formula boat tractor hull |
| CN107792356A (en) * | 2017-09-28 | 2018-03-13 | 宝鸡欧亚化工设备制造厂 | One kind takes off vertically type gyroplane |
| CN209037832U (en) * | 2018-09-21 | 2019-06-28 | 湖南湘晨飞机工业有限公司 | A kind of gyroplane casing |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN119408691A (en) * | 2024-10-16 | 2025-02-11 | 中国直升机设计研究所 | A tandem helicopter cockpit with variable configuration |
| CN119408691B (en) * | 2024-10-16 | 2025-12-30 | 中国直升机设计研究所 | A tandem helicopter cockpit with variable configuration |
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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 | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190104 |
|
| WW01 | Invention patent application withdrawn after publication |