CN203111519U - Rocker booster - Google Patents
Rocker booster Download PDFInfo
- Publication number
- CN203111519U CN203111519U CN 201320013068 CN201320013068U CN203111519U CN 203111519 U CN203111519 U CN 203111519U CN 201320013068 CN201320013068 CN 201320013068 CN 201320013068 U CN201320013068 U CN 201320013068U CN 203111519 U CN203111519 U CN 203111519U
- Authority
- CN
- China
- Prior art keywords
- rocket booster
- aircraft
- plane
- booster
- rocket
- 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 - Fee Related
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Abstract
The utility model discloses a rocket booster, and belongs to aircraft boosting devices. The rocket booster comprises rocket booster bodies, the rocket booster bodies are mounted on the lower surfaces of two wings of a plane at the inside of motors, and the rocket booster is designed to be detachable at the position close to a plane body. A control switch of the rocket booster bodies is mounted inside a pilot compartment of the plane. When the plane breaks down and needs landing, the rocket booster is turned on, and thus the plane can land stably.
Description
Technical field
The utility model relates to a kind of booster, specifically a kind of rocket booster.
Background technology
Aircraft all is equipped with driving engine on two wings, when one of them driving engine breaks down shutdown, only depend on the another one engine operation, and aircraft also can fly reluctantly.But when landing time, because a side wing lacks power, can be to steadily the exerting an influence of aircraft, the landing difficulty is very big.
The utility model content
The purpose of this utility model is to provide a kind of rocket booster, and this rocket booster can help to occur the aircraft stable landing of engine breakdown.
The technical scheme in the invention for solving the technical problem is: a kind of rocket booster, it is characterized in that, comprise the rocket booster body, described rocket booster body is installed in below the both wings of aircraft, inboard at aero-engine, near the body place, be detachable design, the master cock of rocket booster body is installed in the aircraft cockpit.
The beneficial effects of the utility model are: when driving engine breaks down, when aircraft need land, open this rocket booster, can help the landing of aircraft pulsation-free.
Description of drawings
Fig. 1 is structural representation of the present utility model.
Among the figure: 1 rocket booster body, 2 driving engines, 3 bodies, 4 driving compartments.
The specific embodiment
As shown in Figure 1.A kind of rocket booster, comprise rocket booster body 1, described rocket booster body 1 is installed in below the both wings of aircraft, inboard at aero-engine 2, near body 3 places, be detachable design, the master cock of rocket booster body 1 is installed in the aircraft cockpit 4, can be at driving compartment 4 inner control rocket booster bodies 1.
Working as driving engine 2 when aircraft breaks down, aircraft still can rely on the driving engine 2 of a side to continue flight, when aircraft need land, open this rocket booster body 1, kill engine 2 again, the steady power that aircraft relies on both sides rocket booster body 1 to produce can help the landing of aircraft pulsation-free.
Claims (1)
1. a rocket booster is characterized in that, comprises the rocket booster body, described rocket booster body is installed in below the both wings of aircraft, in the inboard of aero-engine, near the body place, be detachable design, the master cock of rocket booster body is installed in the aircraft cockpit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320013068 CN203111519U (en) | 2013-01-10 | 2013-01-10 | Rocker booster |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320013068 CN203111519U (en) | 2013-01-10 | 2013-01-10 | Rocker booster |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203111519U true CN203111519U (en) | 2013-08-07 |
Family
ID=48891889
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320013068 Expired - Fee Related CN203111519U (en) | 2013-01-10 | 2013-01-10 | Rocker booster |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203111519U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108168380A (en) * | 2017-12-18 | 2018-06-15 | 合肥凯石投资咨询有限公司 | A kind of reusable rocket boost motor of Bionic Design |
| CN108180794A (en) * | 2017-12-18 | 2018-06-19 | 合肥凯石投资咨询有限公司 | A kind of reusable rocket boost motor with rotor blade |
-
2013
- 2013-01-10 CN CN 201320013068 patent/CN203111519U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108168380A (en) * | 2017-12-18 | 2018-06-15 | 合肥凯石投资咨询有限公司 | A kind of reusable rocket boost motor of Bionic Design |
| CN108180794A (en) * | 2017-12-18 | 2018-06-19 | 合肥凯石投资咨询有限公司 | A kind of reusable rocket boost motor with rotor blade |
| CN108168380B (en) * | 2017-12-18 | 2019-11-08 | 合肥凯石投资咨询有限公司 | A kind of reusable rocket boost motor of Bionic Design |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130807 Termination date: 20140110 |