CN202828097U - Rotorcraft engine compartment - Google Patents
Rotorcraft engine compartment Download PDFInfo
- Publication number
- CN202828097U CN202828097U CN 201220447840 CN201220447840U CN202828097U CN 202828097 U CN202828097 U CN 202828097U CN 201220447840 CN201220447840 CN 201220447840 CN 201220447840 U CN201220447840 U CN 201220447840U CN 202828097 U CN202828097 U CN 202828097U
- Authority
- CN
- China
- Prior art keywords
- engine compartment
- piggyback pod
- utility
- model
- protective cover
- 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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- Casings For Electric Apparatus (AREA)
Abstract
The utility model discloses a rotorcraft engine compartment. A protection cover is arranged on the upper portion of the engine compartment and fixed on the portion, on the tail portion of a body, of a housing. Due to the fact that the protection cover is arranged on the upper portion of the engine compartment, dust or rainwater or sundries can be prevented from falling into the engine compartment to damage equipment. The protection cover is fixed on the portion, on the tail portion of the body, of the housing to be combined with the housing into a whole, and therefore flow can be rectified in the process of flying, and the flying is more stable and safe.
Description
Technical field
The utility model relates to a kind of cyclogyro piggyback pod.
Background technology
Present small-sized cyclogyro, piggyback pod is at afterbody, and piggyback pod opens wide, and without any protective device, dust, rainwater or foreign material can fall to power plant is damaged; And, because piggyback pod opens wide, during cyclogyro flight air-flow resistance also large, air flow line is chaotic, affects flight safety.
The utility model content
The utility model purpose is to provide a kind of cyclogyro piggyback pod that can protect flight safety.
In order to solve the problems of the technologies described above, cyclogyro piggyback pod of the present utility model is provided with protective cover on the top of piggyback pod, and described protective cover is fixed in the afterbody casing.
Adopt structure of the present utility model, owing to be provided with protective cover on the top of piggyback pod, can prevent that dust, rainwater or foreign material from can fall to damage equipment in the piggyback pod; Protective cover is fixed in the afterbody casing, becomes whole with casing, can rectification in flight course, and the more stability and safety of flying.
Description of drawings
Fig. 1 is protective roof structure scheme drawing of the present utility model;
Fig. 2 is protective cover right elevation figure of the present utility model.
The specific embodiment
Below in conjunction with the drawings and specific embodiments the utility model is described in detail:
As shown in Figure 1 and Figure 2, cyclogyro piggyback pod of the present utility model is provided with protective cover 1 on the top of piggyback pod, and this protective cover is fixed in the afterbody casing.
Claims (1)
1. cyclogyro piggyback pod, it is characterized in that: be provided with protective cover (1) on the top of piggyback pod, described protective cover is fixed in the afterbody casing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220447840 CN202828097U (en) | 2012-09-05 | 2012-09-05 | Rotorcraft engine compartment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220447840 CN202828097U (en) | 2012-09-05 | 2012-09-05 | Rotorcraft engine compartment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202828097U true CN202828097U (en) | 2013-03-27 |
Family
ID=47939861
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220447840 Expired - Fee Related CN202828097U (en) | 2012-09-05 | 2012-09-05 | Rotorcraft engine compartment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202828097U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105314110A (en) * | 2015-10-30 | 2016-02-10 | 嘉兴亚欧光电科技有限公司 | Unmanned aerial vehicle with umbrella |
-
2012
- 2012-09-05 CN CN 201220447840 patent/CN202828097U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105314110A (en) * | 2015-10-30 | 2016-02-10 | 嘉兴亚欧光电科技有限公司 | Unmanned aerial vehicle with umbrella |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130327 Termination date: 20140905 |
|
| EXPY | Termination of patent right or utility model |