SU105402A1 - The mechanism of the suspension flap on the swept wing of the aircraft - Google Patents
The mechanism of the suspension flap on the swept wing of the aircraftInfo
- Publication number
- SU105402A1 SU105402A1 SU550972A SU550972A SU105402A1 SU 105402 A1 SU105402 A1 SU 105402A1 SU 550972 A SU550972 A SU 550972A SU 550972 A SU550972 A SU 550972A SU 105402 A1 SU105402 A1 SU 105402A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- flap
- aircraft
- swept wing
- suspension flap
- wing
- Prior art date
Links
Landscapes
- Platform Screen Doors And Railroad Systems (AREA)
Description
На стреловидных крыль х выдвижение и отклонение закрылка по потоку происходит по сложной пространственной кривой. В известных конструкци х закрылки соединены с каретками, перемещающимис по направл ющим рельсам. Последние имеют сложную форму. Объ сн етс это тем, что направление выдвижени неперпендпкул рио мгновенной оси вращени закрылка .On the swept wings, the extension and deflection of the flap downstream occurs along a complex spatial curve. In known constructions, the flaps are connected to carriages moving along guide rails. The latter have a complex shape. This is explained by the fact that the direction of the non-pendulum advancement of the instantaneous axis of rotation of the flap.
Предлагаемый свободен от этого недостатка.The proposed is free from this disadvantage.
Сущность изобретени заключаетс в том, что закрылок соединен с каретками при помощи карданного механизма .The essence of the invention is that the flap is connected to the carriages using a gimbal mechanism.
На фиг. 1 изображена схема крыла с указанием оси вращени закрылка в убранном и отклоненном положении закрылка; на фиг. 2-разрез крыла по АЛ на фиг. 1 (в увеличенном масштабе); на фиг. 3 приведены в качестве примера формы направл ющих дл кареток рельсов.FIG. 1 shows a wing diagram showing the axis of rotation of the flap in the retracted and rejected position of the flap; in fig. 2-section of the wing along the AL in FIG. 1 (on an enlarged scale); in fig. 3 shows as an example the shape of the guides for rail carriages.
В убранном положении ось закрылка 1 расположена по линиии /а-1а, а Б отклоненном положении она переместитс в положение 2а-2а, оси рельсов размещены по линии За-За. Механизм подвески закрылка состоит изIn the retracted position, the flap axis 1 is located along the line / a-1a, and in the B deflected position it moves to position 2a-2a, the rail axes are placed along the line Za-Za. The flap suspension mechanism consists of
кардана 2 с горизонтальной 3 и вертикальной 4 ос ми вращени , передней 5 п задней 6 кареток, перемещающихс по направл ющим рельсам 7.cardan 2 with horizontal 3 and vertical 4 axes of rotation, front 5 n rear 6 carriages moving along guide rails 7.
Предлагаемый карданный механизм подвески закрылка дает возмои ность осуществить сложное пространственное движение закрылка при помощи простых плоскостных кареток п плоских рельсов различной формы. Применение различных форм рельсов позвол ет получать разные зависимости между ходом закрылка и его углами отклонени без конструктивных и технологических усложнений механизма.The proposed cardan flap suspension mechanism makes it possible to carry out a complex spatial movement of the flap using simple planar carriages and flat rails of various shapes. The use of different rail shapes allows different dependencies to be obtained between the flap stroke and its deflection angles without structural and technological complications of the mechanism.
Предмет изобретени Subject invention
L Механизм подвески закрылка на стреловидно.м крыле самолета со значительной толщиной крыла, с каретками , движущимис по направл ющим рельсам, отличающийс тем, что, с целью осуществлени сложного пространственного движени закрылка при помощи плоских элементов, закрылок соединен с каретками карда1юм, а направл ющий рельс выполнен плоским .L The flap suspension mechanism on an arrow-shaped wing of an aircraft with a considerable wing thickness, with carriages moving along guide rails, characterized in that, in order to accomplish a complex spatial movement of the flap using flat elements, the flap is connected to the carriage carriage, rail is made flat.
2. Форма выполнени маханизма по п. 1, отличающа с тем, что, с целью обеспечени заданны.х отношеРазрез по ДЙ2. The form of accomplishment of the makhanizm according to claim 1, characterized in that, in order to ensure the predetermined relationship.
Фиг. 2FIG. 2
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU550972A SU105402A1 (en) | 1956-04-13 | 1956-04-13 | The mechanism of the suspension flap on the swept wing of the aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU550972A SU105402A1 (en) | 1956-04-13 | 1956-04-13 | The mechanism of the suspension flap on the swept wing of the aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU105402A1 true SU105402A1 (en) | 1956-11-30 |
Family
ID=48378805
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU550972A SU105402A1 (en) | 1956-04-13 | 1956-04-13 | The mechanism of the suspension flap on the swept wing of the aircraft |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU105402A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2024091205A1 (en) * | 2022-10-25 | 2024-05-02 | Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi | A control surface movement mechanism |
-
1956
- 1956-04-13 SU SU550972A patent/SU105402A1/en active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2024091205A1 (en) * | 2022-10-25 | 2024-05-02 | Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi | A control surface movement mechanism |
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