CN205135374U - Curtain hangar door structure is rolled up in combination - Google Patents
Curtain hangar door structure is rolled up in combination Download PDFInfo
- Publication number
- CN205135374U CN205135374U CN201520920899.9U CN201520920899U CN205135374U CN 205135374 U CN205135374 U CN 205135374U CN 201520920899 U CN201520920899 U CN 201520920899U CN 205135374 U CN205135374 U CN 205135374U
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- hangar
- door
- track
- model
- horizontal rail
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Abstract
The utility model relates to a hangar, specifically speaking are curtain hangar door structure is rolled up in combination, including the hangar frame, the access & exit equipartition of hangar frame is equipped with the first door body, the third door body, the second door body, and hangar frame top is equipped with first horizontal track corresponding to first door body department, and hangar frame top is equipped with the horizontal track of second corresponding to second door body department, sliding on the first horizontal track and setting up a shiftable track, it sets up the 2nd shiftable track to slide on the horizontal track of second, AND gate body matched with slotted guide track has all been offered along vertical orientation in a shiftable track, the 2nd shiftable track's side. The product of the utility model is simple in structure, rationally, in use can carry out corresponding regulation to hangar door opening size according to the size of model to make the hangar can be applicable to more specification model's aircraft, the utility model discloses hangar door opening size's regulation convenient and fast in the product.
Description
Technical field
The utility model relates to hangar, specifically a kind of combination roller shutter hangar door structure.
Background technology
The hangar door of helicopter, fighter plane generally adopts the opening ways of lateral rotating type, plug-type, upper-turn-type, after opening completely, takies peripheral space large, comparatively complicated in the hangar door structure of this several mode; You Yu takes up room comparatively large, brings the interior layout of hangar and fabricating cost also large.Also there is a larger problem in existing hangar, because the width of hangar door access is fixed, can only hold the aircraft of specific model, and the larger aircraft of some width is then because the restriction of hangar door cannot enter in hangar.
Summary of the invention
The utility model is for the problems referred to above, and provide a kind of combination roller shutter hangar door structure, the size of this hangar access can carry out corresponding adjustment according to type size.
According to the technical solution of the utility model: a kind of combination roller shutter hangar door structure, it is characterized in that: comprise hangar framework, the access of hangar framework is laid with first body, 3rd body, second body, hangar frame roof corresponds to first body place and is provided with the first horizontal rail, hangar frame roof corresponds to second body place and is provided with the second horizontal rail, described first horizontal rail is slided the first shiftable track is set, second horizontal rail is slided the second shiftable track is set, described first shiftable track, the side of the second shiftable track all vertically offers the chute track with door mates.
As further improvement of the utility model, described hangar frame roof installs the first door lifter, the second door lifter, three open-door machine, wherein the first door lifter is for first body that reel, and the second door lifter is for second body that reel, and three open-door machine is for the 3rd body that reel.
As further improvement of the utility model, bottom described first body, second body, the 3rd body three, be fixed with seal head respectively.
As further improvement of the utility model, described hangar base of frame position, corresponding to the first horizontal rail, both the second horizontal rail below be respectively equipped with a stopper slot, first shiftable track, both the second shiftable tracks lower end are fixed with fastening screw respectively, and two fastening screw correspondences are arranged in corresponding stopper slot.
Technique effect of the present utility model is: the utility model product structure is simple, reasonable, in use can carry out corresponding adjustment according to the size of type to hangar door openings of sizes, with the aircraft making hangar can be applicable to more specifications and models; In the utility model product, hangar door openings of sizes is fast easy to adjust.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the left view of Fig. 1.
Fig. 3 is the top view of Fig. 1.
Fig. 4 is I place's partial enlarged drawing in Fig. 2.
Fig. 5 is II place's partial enlarged drawing in Fig. 3.
Fig. 6 is III place's partial enlarged drawing in Fig. 2.
Detailed description of the invention
Below in conjunction with accompanying drawing, detailed description of the invention of the present utility model is further described.
In Fig. 1 ~ 6, comprise hangar framework 1, first door lifter 2, three open-door machine 3, second door lifter 4, second horizontal rail 5, first horizontal rail 6, first body 7, the 3rd body 8, second body 9, first shiftable track 10, second shiftable track 11, seal head 12, fastening screw 13, curtain plate 14, wind resistance wheel 15 etc.
As shown in Fig. 1 ~ 6, the utility model is a kind of combination roller shutter hangar door structure, comprise hangar framework 1, the access of hangar framework 1 is laid with first body 7, 3rd body 8, second body 9, hangar framework 1 top corresponds to first body 7 place and is provided with the first horizontal rail 6, hangar framework 1 top corresponds to second body 9 place and is provided with the second horizontal rail 5, described first horizontal rail 6 is slided the first shiftable track 10 is set, second horizontal rail 5 is slided the second shiftable track 11 is set, described first shiftable track 10, the side of the second shiftable track 11 all vertically offers the chute track with door mates.
The first door lifter 2, second door lifter 4, three open-door machine 3 are installed in hangar framework 1 top, and wherein the first door lifter 2 is for first body 7, second door lifter 4 that reels for second body 9 that reel, and three open-door machine 3 is for the 3rd body 8 that reel.
As shown in Figure 6, seal head 12 is fixed with respectively bottom first body, 7, second body 9, the 3rd body 8 three.
As shown in Figure 2, hangar framework 1 bottom position, corresponding to both the first horizontal rail 6, second horizontal rail 5 below be respectively equipped with a stopper slot, both first shiftable track 10, second shiftable tracks 11 lower end is fixed with fastening screw 13 respectively, and two fastening screw 13 correspondences are arranged in corresponding stopper slot.
As shown in Figure 4, the door body in the utility model adopts polylith curtain plate 14 to be mutually spliced, and the crotch by being connected with curtain plate one between curtain plate with curtain plate is engaged mutually, and this kind of door body structure has good wind resistance effect.
As shown in Figure 5, be provided with the chute track same with on the first shiftable track 10, second shiftable track 11 inside hangar framework 1, the width both sides of three door bodies are equipped with wind resistance wheel 15, and wind resistance wheel 15 is equipped with in corresponding chute track.
The course of work of the present utility model is as follows: the utility model product is after arranging, the flivver of general model can enter in storehouse smoothly after door body is opened, when there being large aircraft to enter in storehouse, large aircraft due to width dimensions larger, be difficult to enter in storehouse, now, by the first door lifter 2, second door lifter 4, three open-door machine 3 is respectively by first body 7, second body 9, 3rd body 8 is opened respectively, after three door bodies are opened respectively, first shiftable track 10 is moved along the first horizontal rail 6 to hangar framework 1 frame, second shiftable track 11 is moved along the second horizontal rail 5 to hangar framework 1 frame, treat the first shiftable track 10, after second shiftable track 11 moves into place, three door body accesss form a large access, the turnover of relatively large aircraft can be met.
Be provided with three door bodies in the utility model product, in practice, door body quantity can be arranged according to specific needs.
Claims (4)
1. a combination roller shutter hangar door structure, it is characterized in that: comprise hangar framework (1), the access of hangar framework (1) is laid with first body (7), 3rd body (8), second body (9), hangar framework (1) top corresponds to first body (7) place and is provided with the first horizontal rail (6), hangar framework (1) top corresponds to second body (9) place and is provided with the second horizontal rail (5), the upper slip of described first horizontal rail (6) arranges the first shiftable track (10), the upper slip of second horizontal rail (5) arranges the second shiftable track (11), described first shiftable track (10), the side of the second shiftable track (11) all vertically offers the chute track with door mates.
2. according to combination roller shutter hangar door structure according to claim 1, it is characterized in that: the first door lifter (2), the second door lifter (4), three open-door machine (3) are installed in described hangar framework (1) top, wherein the first door lifter (2) is for first body (7) that reel, second door lifter (4) is for second body (9) that reel, and three open-door machine (3) is for the 3rd body (8) that reel.
3. according to combination roller shutter hangar door structure according to claim 1, it is characterized in that: bottom described first body (7), second body (9), the 3rd body (8) three, be fixed with seal head (12) respectively.
4. according to combination roller shutter hangar door structure according to claim 1, it is characterized in that: described hangar framework (1) bottom position, corresponding to the first horizontal rail (6), the second horizontal rail (5) both below be respectively equipped with a stopper slot, both lower ends of first shiftable track (10), the second shiftable track (11) are fixed with fastening screw (13) respectively, and two fastening screw (13) correspondences are arranged in corresponding stopper slot.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520920899.9U CN205135374U (en) | 2015-11-18 | 2015-11-18 | Curtain hangar door structure is rolled up in combination |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520920899.9U CN205135374U (en) | 2015-11-18 | 2015-11-18 | Curtain hangar door structure is rolled up in combination |
Publications (1)
Publication Number | Publication Date |
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CN205135374U true CN205135374U (en) | 2016-04-06 |
Family
ID=55621181
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201520920899.9U Expired - Fee Related CN205135374U (en) | 2015-11-18 | 2015-11-18 | Curtain hangar door structure is rolled up in combination |
Country Status (1)
Country | Link |
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CN (1) | CN205135374U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105298373A (en) * | 2015-11-18 | 2016-02-03 | 无锡旭峰门业制造有限公司 | Combined roller blind hangar door structure |
-
2015
- 2015-11-18 CN CN201520920899.9U patent/CN205135374U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105298373A (en) * | 2015-11-18 | 2016-02-03 | 无锡旭峰门业制造有限公司 | Combined roller blind hangar door structure |
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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 | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160406 Termination date: 20201118 |