CN104906808A - Flying building block combination - Google Patents
Flying building block combination Download PDFInfo
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- CN104906808A CN104906808A CN201410086417.4A CN201410086417A CN104906808A CN 104906808 A CN104906808 A CN 104906808A CN 201410086417 A CN201410086417 A CN 201410086417A CN 104906808 A CN104906808 A CN 104906808A
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Abstract
The invention discloses a flying building block combination capable of allowing a user to combine and change at wills. The flying building block combination comprises a framework unit and a wing unit. The framework unit comprises a main frame building block, two wing frame building blocks, a cross connection building block and four wing connection building blocks. The cross connection building block can connect the main frame building block with the wing frame building blocks. Every two wing connection building blocks are connected to the two opposite end portions of each wing frame building block. The wing unit comprises two wing fans connected to the wing connection building blocks. The wing fans can provide buoyancy lift during gliding, in addition, the frame unit is driven via the wing connection building blocks, and the flying of the flying building block combination is supported.
Description
Technical field
The present invention relates to the combination of a kind of building blocks, particularly relate to a kind of fly able building blocks combination.
Background technology
Consult TaiWan, China Patent Case TW366296, disclose an existing building blocks combination, comprise multiple toy building element, described toy building element can be connected so that different angles are complementary in couples respectively, can shine model or the imagination according to this and construction goes out large scale structure.User can utilize described toy building element construction to go out structure as aircraft and human body, and interelement is because to be complementaryly in couples connected, and has an active ground free degree, can rotational deformation arbitrarily.
But although the combination of existing building blocks can assemble distortion arbitrarily, complete specific appearance, the structural design because of building blocks is only to form any shape easily, and the model therefore so as to assembling does not have any function.So although user uses described building blocks to combine make a model aircraft, this model aircraft does not have the ability of any flight completely.
Consult TaiWan, China Patent Case TWM392687U1, disclose a kind of existing flying toy, forming primarily of foaming Poly Foam, it includes an airframe, two reinforcement fuselage cradles, wing, a flat empennage.Two opposition sides of this airframe paste described reinforcement fuselage cradle respectively, form a fuselage.The central authorities of wing and this fuselage upper limb gluing, this flat empennage sticks in bottom the tail end of this fuselage.Because this plane toy is that the Poly Foam material that foams formed, have light-weighted characteristic, therefore when sliding, this wing can provide enough buoyancy lifts, and supports this flying toy, makes it fly.
But though existing flying toy has flight function, so its each interelement connects all in a fixed manner, only has single kind of outward appearance, user cannot adjust this existing flying toy according to its imagination.That is, existing flying toy cannot for user give free rein to one's imagination and complete its outward appearance for reaching.
So, though the combination of existing building blocks can be given free rein to one's imagination for user, complete desired aircraft kenel, not there is the function of flight.And though existing flying toy has the function of flight, user cannot according to its imagined the outward appearance for reaching.Cannot meet in existing toy simultaneously and be combined and have the needs of flight function concurrently.
Summary of the invention
The object of the present invention is to provide a kind of can any combination and have flight function flight building blocks combine.
The present invention flies building blocks combination, comprises a skeleton unit, and a wing element.This skeleton unit comprises dry bone building blocks, at least one ptergoid bone building blocks, connection building blocks, and at least two wings connect building blocks.These connection building blocks have one and linearly extend and supply the first jack that these dry bone building blocks removably plug, Ji Yige center and angled second jack of this first jack.This second jack is configure along the direction vertical with this first jack, and removably plugs for these ptergoid bone building blocks.The described wing connects building blocks and is removably plugged by two opposite ends of these ptergoid bone building blocks respectively, and has one in conjunction with group.
This wing element comprises a fin.This fin has two the engaging groups being positioned at two opposite ends, and each engaging group removably can fix in conjunction with group for each.This fin can provide a buoyancy lift in time gliding, and borrows the described wing to connect building blocks and drive this skeleton unit, supports that these flight building blocks combine flight.
Beneficial effect of the present invention is: by providing different building blocks, allow user can piece together combination arbitrarily, and complete the outward appearance for reaching, and pass through this fin of energy Optional assembling, user can adjust the size and location of wing element whereby, and make to provide enough buoyancy lifts to make flight building blocks combine flight in time gliding.
Accompanying drawing explanation
Fig. 1 is a three-dimensional exploded view, illustrates that the present invention flies the element of a preferred embodiment of building blocks combination;
Fig. 2 is a partial enlargement exploded view, illustrates that a wing of this preferred embodiment connects the connected mode that first of building blocks implement aspect and two panels fin;
Fig. 3 is a stereogram, and first preferred embodiment of this preferred embodiment is described, is a medium-sized aircraft combination;
Fig. 4 is a stereogram, and second preferred embodiment of this preferred embodiment is described, is the aircraft combination of an aerofoil profile of inclining;
Fig. 5 is a stereogram, and the 3rd preferred embodiment of this preferred embodiment is described, is the aircraft combination of a spademan type;
Fig. 6 is a stereogram, and the 4th preferred embodiment of this preferred embodiment is described, is the aircraft combination of a multiple-fin;
Fig. 7 is a stereogram, and the 5th preferred embodiment of this preferred embodiment is described, is the aircraft combination of a folded aerofoil profile;
Fig. 8 is a stereogram, and the 6th preferred embodiment of this preferred embodiment is described, is the aircraft combination of a flap type;
Fig. 9 is a stereogram, illustrates that this wing of this preferred embodiment connects second of building blocks and implements aspect; And
Figure 10 is a stereogram, illustrates that this wing of this preferred embodiment connects the 3rd of building blocks and implements aspect.
Detailed description of the invention
Below in conjunction with drawings and Examples, the present invention is described in detail.
Before the present invention is described in detail, should be noted that in the following description content, similar element represents with identical numbering.
Need first it is noted that Fig. 1 is for illustrating that the present invention flies each element used in building blocks combination.The original paper structure of each preferred embodiment for convenience of description, each preferred embodiment all can with reference to the element listed by figure 1.
Consulting Fig. 1 to Fig. 3, is the first preferred embodiment of the present invention, is a medium-sized aircraft combination.It is that the dry bone building blocks of use one 11, two ptergoid bone building blocks 12, cross connects building blocks 13I, four wings connect building blocks 14, two panels fin 21, gravity unit 3, and two panels empennage 4 formed.Its material is the light material such as carbon fiber or plastic cement.
These dry bone building blocks 11 are the square column type linearly extended.Each ptergoid bone building blocks 12 can be identical with the shape of these dry bone building blocks 11, also can be different shapes, ought to not with the content disclosed in this preferred embodiment for restriction.
It is the first enforcement aspect that the present invention connects building blocks 13 that this cross connects building blocks 13I, has first jack 131 and second jack 132 that linearly extend.This second jack 132 is mutually vertical with this first jack 131, and the center of this second jack 132 is connected with this first jack 131.
Each wing connects building blocks 14 and has a body 141, three ptergoid bone jacks 142 be formed on this body 141, and two basic change group 143.This body 141 outer peripheral edge slightly in eye shape, and has the rib 144 of multiple connection outer peripheral edge and inner peripheral.Described rib 144 matches with this body 141 outer peripheral edge and defines multiple vacancy section 145.The shape of each ptergoid bone jack 142 is cross, plugs for each ptergoid bone building blocks 12.The quantity of described ptergoid bone jack 142 also can be one, two, or more than four.
Described two lateral margins being located at this body in conjunction with group 143 respectively, and each has three convex buttons 146 in conjunction with group 143.This also can be only one in conjunction with group 143.This also only can comprise one or two convex button 146 in conjunction with group 143, or is the convex button 146 of more than four.
Each convex button 146 has a head section 147, and the figure 148 of this section 147 of connection and this body 141.Match and define one and engage space 149 in the outer peripheral edge of this section 147 and this figure 148 and body 141.It is worth mentioning that, the outer peripheral edge of this body 141 can form the groove that multiple and described convex button 146 matches, and described convex button 146 is arranged in described groove respectively.
By by these dry bone building blocks 11, described ptergoid bone building blocks 12, and the described wing connects building blocks 14 and connects, and forms a skeleton unit 1.Connected mode is these dry bone building blocks 11 are inserted in this cross to connect in first jack 131 of building blocks 13I, and described ptergoid bone building blocks 12 are inserted in respectively in second jack 132 of this cross connection building blocks 13I, finally every two wings are connect building blocks 14 and be located in two opposite ends of each ptergoid bone building blocks 12.
Every a slice fin 21 has two the engaging groups 211 being positioned at two opposite ends.Each engaging group 211 for can the described wing of confession connect building blocks 14 each removably fix in conjunction with group 143, and there are three of matching with described convex button 146 bore a hole 212.The quantity of described perforation 212 is closed with the cooperating number of described convex button 146, and therefore when the quantity of described convex button 146 is one, the quantity of described perforation 212 is also one.The change of this kind of quantity can be selected arbitrarily, ought to not with the content disclosed in this preferred embodiment for restriction.
Described in conjunction with in group 143 by described engaging group 211 being fastened in respectively, two wings that every a slice fin 21 is located on each ptergoid bone building blocks 12 connect on building blocks 14, complete a wing element 2.
It is worth mentioning that, this wing element 2 can comprise four fins 21 (as shown in Figure 1).Every a slice fin 21 is connect building blocks 14 by two wings and fixes and be obedient to the outer peripheral edge that this wing connects the body 141 of building blocks 14, makes each wing connect building blocks 14 and connects two panels fin 21.The mode that this kind connects can be selected arbitrarily.
This gravity unit 3 is located on these dry bone building blocks 11, and this cross contiguous connects an end of building blocks 13I.This gravity unit 3 is by rectangle building blocks 31, and a square building block 32 is formed.A terminal part side of this rectangle building blocks 31 length direction is connected with these dry bone building blocks 11.This square building block 32 is connected to another opposite ends of these rectangle building blocks 31.
Mutually vertical between described empennage 4, and be located in two end opposite of these dry bone building blocks 11, and comprise at least one empennage jack 41 for being plugged by these dry bone building blocks 11 or this ptergoid bone building blocks 12.
By adjusting this gravity unit 3, the position of described empennage 4 and assembled state, this plain edition aircraft is combined in have when sliding preferably to balance, and this wing element 2 can provide buoyancy lift in time sliding, this plain edition aircraft is combined can firmly free coast.
Consulting Fig. 1, Fig. 2 and Fig. 4, is the second preferred embodiment of the present invention, is the aircraft combination of an aerofoil profile of inclining.The wing connects building blocks 13II, four wings connect building blocks 14, two panels fin 21, gravity unit 3 to use 12, one, dry bone building blocks 11, two ptergoid bone building blocks to incline, and two panels empennage 4 formed.
It is the second enforcement aspect that the present invention connects building blocks 13 that this wing that inclines connects building blocks 13II, has the second jack 132 that first jack 131, a Ji Yige center linearly extended is connected with this first jack 131.This second jack 132 is configure along the direction vertical with this first jack 131, and profile is V-shaped.Because this second jack 132 presents V-arrangement, therefore can present praise form after the described ptergoid bone building blocks 12 of insertion, make this wing element 2 present symmetrical V-arrangement.
This gravity unit 3 is by rectangle building blocks 31, two square building blocks 32, and arc building blocks 33 are stacking forms.An end of the length direction of these rectangle building blocks 31 is connected to one end of these dry bone building blocks 11, and another end connects this arc building blocks 33.The downside of these rectangle building blocks 31 and these arc building blocks 33 connects two connected square building blocks 32.This gravity unit 3 forms a head shape.
Described empennage 4 connects in orthogonal mode, and be located at these dry bone building blocks 11 away from an end of this gravity unit 3.By adjusting position and the assembled state of this gravity unit 3 and described empennage 4, this aerofoil profile aircraft that inclines is combined in have when sliding preferably to balance, and this wing element 2 can provide buoyancy lift in time sliding, making this incline the combination of aerofoil profile aircraft can firmly free coast.
This preferred embodiment be utilize this wing that inclines with inclination angle to connect building blocks 13II and make this wing element 2 described fin 21 shapes at an angle, different from medium-sized aircraft form.The aspect and completing that user can convert these connection building blocks 13 arbitrarily has angle or not tool this wing element 2 angled.
Consulting Fig. 1, Fig. 2 and Fig. 5, is the 3rd preferred embodiment of the present invention, is the aircraft combination of a spademan type.This preferred embodiment is the change of this first preferred embodiment, and for many increases by two 12, two, ptergoid bone building blocks incline, the wing connects building blocks 13II, four wings connect building blocks 14 for it, and two panels fin 21.
Second jack 132 of building blocks 13II is connected by the wing that inclines described in newly-increased, the newly-increased described wing is connect building blocks 12 and be linked to this first end comparatively adding the described ptergoid bone building blocks 12 of embodiment respectively, again every two newly-increased wings being connect building blocks 14 is located in two opposite ends of each newly-increased ptergoid bone building blocks 12, forms the skeleton unit 1 extended.
By two wings be fastened on each newly-increased ptergoid bone building blocks 12 connect building blocks 14 by each newly-increased fin 21, form a wing element 2 extended.
By adjusting this gravity unit 3, described empennage 4 and described wing element 2, and this spademan type aircraft is combined in when sliding can obtain buoyancy lift from this wing element 2, and borrow this gravity unit 3 to adjust the center of gravity of overall aircraft and described empennage 4 balance airplane is overall, this spademan type aircraft is combined can firmly free coast.
This enforcement aspect is the skeleton utilizing described connection building blocks 13I, 13II of two different shapes to extend wing, and then increases the length of this wing element 2.User can adjust the length of this wing element 2 arbitrarily by using described connection building blocks 13I, 13II, be not subject to the restriction of described ptergoid bone building blocks 12 length.
Consulting Fig. 1, Fig. 2 and Fig. 6, is the 4th preferred embodiment of the present invention, is the aircraft combination of a multiple-fin.This preferred embodiment is the change of this second preferred embodiment, and characteristic is to give up empennage 4 and uses another wing element 2 instead and replaces, and simplifies this gravity unit 3.
For many increases by two 12, one, ptergoid bone building blocks incline, the wing connects building blocks 13II to the present embodiment, four wings connect building blocks 14, two panels fin 21.It is for remove this empennage 4 of this second preferred embodiment, and these dry bone building blocks 11 of this second preferred embodiment is plugged this newly-increased wing that inclines and connect on first jack 131 of building blocks 13II, and this skeleton unit 1 is increased wing element 2.
For convenience of description, the connected mode of newly-increased element is below only described: described ptergoid bone building blocks 12 insert this wing that inclines respectively and connect on second jack 132 of building blocks 13II, again every two wings are connect building blocks 14 to be located in two opposite ends of each ptergoid bone building blocks 12, complete this skeleton unit 1.Two wings be fastened in by every a slice fin 21 on each ptergoid bone building blocks 12 connect building blocks 14, form two wing element 2.
This gravity unit 3 only comprises rectangle building blocks 31, and a terminal part side of this rectangle building blocks 31 length direction is connected with these dry bone building blocks 11.
By adjusting this gravity unit 3 and described wing element 2, and this multiple-fin aircraft is combined in when sliding can obtain buoyancy lift from described wing element 2, and borrow this gravity unit 3 to adjust the center of gravity of overall aircraft, this multiple-fin aircraft is combined can firmly free coast.
This preferred embodiment is located on these dry bone building blocks 11 by multiple wing connection building blocks 13II that inclines by using, and increase the quantity of described wing element 2.User can utilize the mode increasing and connect building blocks 13, and simply reaches its desired described wing element 2 quantity.
Consulting Fig. 1, Fig. 2 and Fig. 7, is the 5th preferred embodiment of the present invention, is the aircraft combination of a folded aerofoil profile, is connection building blocks 13I, 13III of utilizing two different shapes, assembles the aircraft of multiple wing element 2.Use two dry bone building blocks, 11, four ptergoid bone building blocks 12, cross connection building blocks 13I, orthogonal connection building blocks 13III, eight wings to connect building blocks 14, four fins 21, gravity unit 3, and a sheet empennage 4 formed.
This orthogonal connection building blocks 13III is the 3rd enforcement aspect that the present invention connects building blocks 13, has and linearly extends and mutually orthogonal first jack 131, second jack 132, and the 3rd jack 133.It is worth mentioning that, this orthogonal connection building blocks 13III can use two crosses to connect building blocks 13I to intersect stacking forming, and its stack manner is that the axis direction of described second jack 132 is mutually vertical, and makes described first jack 131 mutually aim at and communicate.
By by described dry bone building blocks 11, described ptergoid bone building blocks 12, and the described wing connects building blocks 14 and connects, and forms a skeleton unit 1.Connected mode is that one of them is inserted in first jack 131 of this orthogonal connection building blocks 13III by described dry bone building blocks 11, and another dry bone building blocks 11 are inserted in the 3rd jack 133.This dry another end of bone building blocks 11 inserted in the 3rd jack 133 plugs this cross and connects in first jack 131 of building blocks 13I.Described ptergoid bone building blocks 12 are inserted in respectively in second jack 132 of this orthogonal connection building blocks 13III and this cross connection building blocks 13I.Every two wings are connect building blocks 14 be located in two opposite ends of each ptergoid bone building blocks 12.
By two wings be fastened on each ptergoid bone building blocks 12 connect on building blocks 14 by each fin 21, form two wing element 2.
This gravity unit 3 is by rectangle building blocks 31, square building block 32, and arc building blocks 33 are stacking forms.An end of the length direction of these rectangle building blocks 31 is connected to the one end of this orthogonal connection building blocks 13III contiguous in these dry bone building blocks 11.Another end of the length direction of these rectangle building blocks 31 connects this arc building blocks 33.The downside of these rectangle building blocks 31 connects this square building block 32.This gravity unit 3 forms a head shape.
This empennage 4 is located at these dry bone building blocks 11 away from an end of this gravity unit 3.By adjusting this gravity unit 3, this empennage 4 and described wing element 2, and this folded aerofoil profile aircraft is combined in when sliding can obtain buoyancy lift from described wing element 2, and borrow this gravity unit 3 to adjust the center of gravity of overall aircraft and described empennage 4 balance airplane is overall, make this folded aerofoil profile aircraft combination can firmly free coast.
This enforcement aspect is the maincenter using this orthogonal connection building blocks 13III to connect as skeleton.Because this orthogonal connection building blocks 13III has the closure of three axles, therefore compare medium-sized aircraft aspect, use this orthogonal connection building blocks 13III can increase a link position more, be accomplished the aircraft combination of folded aerofoil profile state.User can use this orthogonal connection building blocks 13III easily and increase the free degree of connection.
Consulting Fig. 1, Fig. 2 and Fig. 8, is the 6th preferred embodiment of the present invention, is the aircraft combination of a flap type.Use two dry bone building blocks, 11, five ptergoid bone building blocks, 12, three crosses to connect building blocks 13I, two wing connection building blocks 13II that incline, eight wings connect building blocks 14, four fins 21, and a slice empennage 4 formed.
Below for convenience of description, described ptergoid bone building blocks 12 are divided into ptergoid bone building blocks 12 ' according to connected mode, and four ptergoid bone building blocks 12 ' '.Described cross is connected building blocks 13I and divide into a cross connection building blocks 13I ' according to connected mode, and two crosses connect building blocks 13I ' '.
By by described dry bone building blocks 11, described ptergoid bone building blocks 12, and the described wing connects building blocks 14 and connects, and forms a skeleton unit 1.Connected mode connects in second jack 132 of building blocks 13I ' for these ptergoid bone building blocks 12 ' being arranged in this cross, then is inserted in respectively by described dry bone building blocks 11 in first jack 131 of this cross connection building blocks 13I '.Two end opposite of these ptergoid bone building blocks 12 ' connect second jack 132 of building blocks 13II and described ptergoid bone building blocks 12 ' respectively by the described wing that inclines ' one end of two is wherein connected.Remaining two of described ptergoid bone building blocks 12 ' ' the other end connect second jack 132 of building blocks 13I ' ' and described ptergoid bone building blocks 12 ' by described cross ' are connected.Finally, every two wings are connect building blocks 14 and is located in two opposite ends of each ptergoid bone building blocks 12, complete this skeleton unit 1.
By two wings be fastened on each ptergoid bone building blocks 12 connect on building blocks 14 by each fin 21, form a wing element 2.
This empennage 4 connects on an end of building blocks 13I ' away from this cross for being located at these dry bone building blocks 11.By adjusting this empennage 4 and this wing element 2, and this flap type aircraft is combined in when sliding can obtain buoyancy lift from this empennage 4 and this wing element 2, this flap type aircraft is combined can free coast.
This enforcement aspect connection building blocks 13I ', the 13I ' ' and 13II of multiple aspect is interconnected between described ptergoid bone building blocks 12 by use, and the wing element 2 of formation and modification form.User can utilize this mode and simply change its this wing element 2 form desired.
Should be noted, flight building blocks of the present invention combination, only can connect building blocks 14 by dry bone building blocks 11, ptergoid bone building blocks 12, orthogonal connection building blocks 13III (or being that a cross connects building blocks 13I), two wings, a slice fin 21 is formed.On the first jack 131 that these dry bone building blocks 11 and this ptergoid bone building blocks 12 are located in this orthogonal connection building blocks 13III respectively and the second jack 132, form symmetrical cross, this wing being connect building blocks 14 is located in two opposite ends of these ptergoid bone building blocks 12 again, finally this fin 21 is connect building blocks 14 with this wing to fix, and then define two symmetrical tab portion (not shown), complete an aircraft.
It is worth mentioning that, the described wing connects building blocks 14 and also has two kinds to implement aspect, and for connecing building blocks 14 as difference with the described wing, distinguishing the second enforcement aspect is that the wing connects building blocks 15, and the 3rd enforcement aspect is that the wing connects building blocks 16.
Consulting Fig. 9, is that the wing of the second enforcement aspect connects building blocks 15.This wing connects building blocks 15 and has a body 151, three ptergoid bone jacks 152 be formed on this body 151, and one in conjunction with group 153.It is similar haply that the described wing that this body 151 structure and first implements aspect connects building blocks 14 (see Fig. 2), and it is only another change of described rib 144 and outer peripheral edge.Described ptergoid bone jack 152 is M shape, and quantity also can be one, two, or more than four.
This has in conjunction with group 153 projection 154 that three are located at this body 151 1 lateral margin, and two cards 155 being located at this body 151 two end opposite.Each projection 154 has a head section 156, and the figure 157 of this section 156 of connection and this body 151.This section 156 matches with the outer peripheral edge of this figure 157, described card 155 and this body 151 and defines one and engage space 158.
Consult Fig. 2 and Fig. 9 to replace this wing connect building blocks 14 when using this wing to connect building blocks 15, and during for connecting a slice fin 21, each perforation 212 can be penetrated by the head section 156 of each projection 154 and make this fin 21 be placed in this engaging space 158, and the card 155 being located at this body 151 two end opposite removably clamps.
Consult Figure 10, be that the 3rd wing implementing aspect connects building blocks 16, present a hair clip shape.This wing connects building blocks 16 and has a body 161, three ptergoid bone jacks 162 be formed on this body 161, and one in conjunction with group 163.The structure and second of this body 161 implements the wing described in aspect, and to connect building blocks 15 identical.This ptergoid bone jack 162 is M shape, and quantity also can be one, two, or more than four.
This has three in conjunction with group 163 and is located at the projection 164 of this body 161 1 lateral margin, a slice intermediate plate 165 being located at two end opposite of this body 161 and a draw-in groove 166.The profile of this intermediate plate 165 presents the radian matched with the outer peripheral edge of this body 161, and there are three perforation 168 matched with described projection 164 respectively, be positioned at a bonding pad 167 of two end opposite and one fix district 169.This intermediate plate is connected on one end of this body 161 by this bonding pad 167, and can be arranged in this in conjunction with on the draw-in groove 166 of group 163 by this fixing district 169.An accommodation space 160 is defined between the outer peripheral edge of this intermediate plate 165 and this body 161.
Consult Fig. 2 and Figure 10, replace this wing connect building blocks 14 when the described wing of use connects building blocks 16, and during for connecting a slice fin 21, each perforation 212 can be penetrated by each projection 164, and by pulling this intermediate plate 165, this fin 21 is located in this accommodation space 160, and the fixing district 169 of this intermediate plate 165 can be fastened on this draw-in groove 166 and not come off, make this fin 21 sandwiched fixing.
It is noted that the described wing connects building blocks 14,15 and 16 can select a kind of use in time combining this skeleton unit 1, or at random used in combination.Each preferred embodiment of the present invention for convenience of description, only discloses the described wing and connects the element of building blocks 14 as this skeleton unit 1.
In sum, user can use different building blocks to piece together combination arbitrarily, complete the outward appearance for reaching, and the size and location of wing element 2 are adjusted by the assembling mode adjusting this skeleton unit 1 and fin 21, make during glide, to provide enough buoyancy lifts to make flight building blocks combine flight, so really object of the present invention can be reached.
Only as described above, be only preferred embodiment of the present invention, when not limiting scope of the invention process with this, the simple equivalence namely generally done according to the claims in the present invention scope and patent specification content changes and modifies, and all still remains within the scope of the patent.
Claims (11)
1. flight building blocks combination, is characterized in that:
Comprise a skeleton unit, and a wing element,
This skeleton unit comprises dry bone building blocks, at least one ptergoid bone building blocks, connection building blocks, and at least two wings connect building blocks, these connection building blocks have one and linearly extend and supply the first jack that these dry bone building blocks removably plug, the second jack that Ji Yige center is connected with this first jack, this second jack is configure along the direction vertical with this first jack, and removably plug for these ptergoid bone building blocks, the described wing connects building blocks and is removably plugged by two opposite ends of these ptergoid bone building blocks respectively, and each wing connects building blocks has one in conjunction with group; And
This wing element comprises a fin, this fin has two the engaging groups laying respectively at two opposite ends, each engaging group removably can fix in conjunction with group for each, this fin can provide a buoyancy lift in time gliding, and borrow the described wing to connect building blocks and drive this skeleton unit, support that these flight building blocks combine flight.
2. flight building blocks as claimed in claim 1 combination, is characterized in that: the second jack of these connection building blocks is for extend along straight line.
3. flight building blocks as claimed in claim 1 combination, is characterized in that: this skeleton unit is for comprising two ptergoid bone building blocks, and the second jack profile of these connection building blocks is V-shaped, this second jack is for plugging respectively for described ptergoid bone building blocks.
4. flight building blocks as claimed in claim 2 combination, is characterized in that: these connection building blocks also comprise one and linearly extend, and with this first jack and mutually orthogonal the 3rd jack of this second jack.
5. the flight building blocks combination as described in claim arbitrary in claim 2 to 4, it is characterized in that: this skeleton unit comprises the ptergoid bone building blocks that two are plugged in this second jack respectively, and four wings connect building blocks, every two wings connect building blocks and are removably arranged in respectively in one of them two opposite ends of described ptergoid bone building blocks.
6. flight building blocks as claimed in claim 5 combination, is characterized in that: this wing element comprises two panels fin, and every a slice fin is that two wings be located on each ptergoid bone building blocks connect building blocks fixing.
7. flight building blocks as claimed in claim 1 combination, it is characterized in that: each wing connects building blocks and also has a body, and a ptergoid bone jack be formed on this body, this body outer peripheral edge is slightly eye shape and is connected in conjunction with group with this, this ptergoid bone jack is plugged by these ptergoid bone building blocks, this has a convex button in conjunction with group, and each engaging group of this fin has the perforation that button convex in this matches.
8. flight building blocks as claimed in claim 7 combination, is characterized in that: the body that each wing connects building blocks has the rib of multiple connection outer peripheral edge and inner peripheral, and described rib matches with this outer peripheral edge and defines multiple vacancy section.
9. flight building blocks as claimed in claim 7 combination, it is characterized in that: the convex fastener that each wing connects building blocks has a head section, and the figure of this section of connection and this body, match and define one and engage space in the outer peripheral edge of this section and this figure and this body, this section can penetrate the perforation of this fin and this fin is placed in this engaging space.
10. flight building blocks as claimed in claim 7 combination, is characterized in that: this also has in conjunction with group the card that two panels lays respectively at this body two end opposite, and described card can clamp this fin.
11. flight building blocks combinations as claimed in claim 7, it is characterized in that: this also has a slice intermediate plate and a draw-in groove in conjunction with group, one end of this intermediate plate is connected with this body, and the other end can be fastened on this draw-in groove, form a hairpin, make to be fastened in this and can be clamped by this intermediate plate in conjunction with this fin in group and fix.
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| CN201410086417.4A CN104906808B (en) | 2014-03-10 | 2014-03-10 | Flying building block combination |
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| CN201410086417.4A CN104906808B (en) | 2014-03-10 | 2014-03-10 | Flying building block combination |
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| CN104906808A true CN104906808A (en) | 2015-09-16 |
| CN104906808B CN104906808B (en) | 2017-04-26 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105771269B (en) * | 2016-02-29 | 2018-10-09 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of toy building set formula unmanned plane and its control method |
| CN113682470A (en) * | 2021-10-08 | 2021-11-23 | 中国民航大学 | Vector power aircraft based on front and back symmetrical wing profiles |
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| CN2437379Y (en) * | 2000-08-11 | 2001-07-04 | 谢孟达 | Toy aircraft capable of replacing elements |
| TWM392687U (en) * | 2010-06-14 | 2010-11-21 | Zheng-Li Cai | light-weight toy aircraft |
| TWM457572U (en) * | 2013-02-08 | 2013-07-21 | Chin Tang Paperware Co Ltd | Building block unit, building block assembling structure using the building block unit, and base material of the building block unit |
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2014
- 2014-03-10 CN CN201410086417.4A patent/CN104906808B/en not_active Expired - Fee Related
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2166863Y (en) * | 1993-08-11 | 1994-06-01 | 龚藤达 | Toy air-plane |
| CN2396857Y (en) * | 1999-09-15 | 2000-09-20 | 廖运焕 | Toy aircraft |
| GB2355672A (en) * | 1999-10-29 | 2001-05-02 | Huang Te Li | Multipurpose modular article |
| CN2405630Y (en) * | 1999-11-24 | 2000-11-15 | 杨明堂 | Ejection-type toy plane |
| CN2437379Y (en) * | 2000-08-11 | 2001-07-04 | 谢孟达 | Toy aircraft capable of replacing elements |
| TWM392687U (en) * | 2010-06-14 | 2010-11-21 | Zheng-Li Cai | light-weight toy aircraft |
| TWM457572U (en) * | 2013-02-08 | 2013-07-21 | Chin Tang Paperware Co Ltd | Building block unit, building block assembling structure using the building block unit, and base material of the building block unit |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105771269B (en) * | 2016-02-29 | 2018-10-09 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of toy building set formula unmanned plane and its control method |
| CN113682470A (en) * | 2021-10-08 | 2021-11-23 | 中国民航大学 | Vector power aircraft based on front and back symmetrical wing profiles |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104906808B (en) | 2017-04-26 |
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