FR2929592A1 - Ultralight motorized small airplane i.e. tourism airplane, storing device for use with hanger, has transversal post provided with baseplates, wrench fixed to support and lifting airplane, and tie-rods assuring rigidity of assembly - Google Patents

Ultralight motorized small airplane i.e. tourism airplane, storing device for use with hanger, has transversal post provided with baseplates, wrench fixed to support and lifting airplane, and tie-rods assuring rigidity of assembly Download PDF

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Publication number
FR2929592A1
FR2929592A1 FR0801806A FR0801806A FR2929592A1 FR 2929592 A1 FR2929592 A1 FR 2929592A1 FR 0801806 A FR0801806 A FR 0801806A FR 0801806 A FR0801806 A FR 0801806A FR 2929592 A1 FR2929592 A1 FR 2929592A1
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France
Prior art keywords
airplane
baseplates
hanger
fixed
support
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Pending
Application number
FR0801806A
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French (fr)
Inventor
Antoine Torres
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Individual
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Individual
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Publication date
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Priority to FR0801806A priority Critical patent/FR2929592A1/en
Publication of FR2929592A1 publication Critical patent/FR2929592A1/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/22Ground or aircraft-carrier-deck installations for handling aircraft
    • B64F1/222Ground or aircraft-carrier-deck installations for handling aircraft for storing aircraft, e.g. in hangars

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)

Abstract

The device has a U-shaped iron carriage (1) arranged in a platform and provided with a U-shaped transversal post (9). A U-shaped central post (16) made of iron is fixed to the carriage. The transversal post is provided with maintaining baseplates (10), and supports the baseplates. Two tie-rods (17) assure the rigidity of an assembly, and an L-shaped support is fixed to a frame of a hanger (20). An electric wrench (19) is fixed to the support, and lifts an ultralight motorized small airplane i.e. tourism airplane, along an I-shaped pillar of the hanger till required height.

Description

La présente invention concerne un appareil servant à entreposer en hauteur des petits avions de tourisme du type U.L.M. dans les hangars à structure métallique. Ces petits avions sont garés au sol et leur grande envergure leur fait occuper beaucoup de place ce qui limite le nombre d'appareils que l'on peut mettre à l'intérieur 3e ces hangars. Le dispositif selon l'invention permet de gagner des places dans le hangar. On fait rouler l'avion sur l'appareil en positionnant la roue avant sur la poutre centrale et le;; deux roues arrière sur les semelles de maintien. Ensuite on soulève le tout en le faisant rouler le long du pilier du hangar à l'aide d'un treuil électrique fixé sur la charpente. Ce qui À0 libère totalement la place au dessous pour garer un autre avion. Il se présente sous la forme d'un kit de cinq éléments qui sont assemblés sur place avec des boulons et qui se compose de : Un chariot avec quatre roulements. Les roulements inférieurs viennent prendre appui sur la face avant du pilier.The present invention relates to an apparatus for storing high altitude small passenger aircraft type U.L.M. in steel structure hangars. These small planes are parked on the ground and their large size makes them occupy a lot of space which limits the number of devices that can put inside these hangars. The device according to the invention makes it possible to gain places in the shed. The airplane is rolled on the apparatus by positioning the front wheel on the central beam and the; two rear wheels on the insoles. Then we lift the whole by rolling it along the pier of the shed with the help of an electric winch fixed on the frame. Which À0 totally frees the place below to park another plane. It comes in the form of a kit of five elements that are assembled on site with bolts and which consists of: A carriage with four bearings. The lower bearings come to bear on the front of the pillar.

15 Les roulements supérieurs sont ensuite boulonnés sur le chariot et prennent place sur la face intérieure du pilier. Les roulements répartissent les charges le long du pilier et permettent à l'appareil de monter et descendre le long de ce dernier. Une poutre centrale qui est fixée sur le bas du chariot, à l'extrémité de cette 2d dernière se fixe la poutre transversale qui maintient les deux semelles. Deux tirants sont fixés d'une part sur le haut du chariot et d'autre part sur l'extrémité extérieure des deux semelles. - On se sert d'un treuil électrique fixé à la charpente au-dessus de l'appareil pour faire monter et descendre ce dernier le long du pilier du hangar. Le sommet du 25 chariot est pourvu d'un anneau pour recevoir le crochet du treuil. Une fois en place , on goupille le chariot au pilier par sécurité. Les dessins annexés illustrent l'invention : Les figures 1 û 2 û 3 représentent le chariot de profil, face et coupe. La figure 4 représente en coupe la figure 10.The upper bearings are then bolted to the carriage and sit on the inner side of the pillar. The bearings distribute the loads along the pillar and allow the unit to move up and down along the pillar. A central beam which is fixed on the bottom of the carriage, at the end of this last 2d is fixed transverse beam which maintains the two soles. Two tie rods are fixed on the one hand on the top of the carriage and on the other hand on the outer end of the two soles. - An electric winch attached to the frame above the unit is used to raise and lower the unit along the pier pillar. The top of the carriage is provided with a ring for receiving the winch hook. Once in place, the carriage is pinned to the pillar for safety. The accompanying drawings illustrate the invention: FIGS. 1 to 2 show the profile carriage, face and section. FIG. 4 is a sectional view of FIG.

30 La figure 5 représente le support du treuil et la figure 6 sa coupe. Les figures 7 et 8 représentent la poutre centrale face et coupe. La figure 9 représente les deux tirants. La figure 10 représente la poutre transversale avec ses deux semelles. La figure 1 l représente l'appareil monté en entier.Figure 5 shows the support of the winch and Figure 6 shows its section. Figures 7 and 8 show the central beam face and cut. Figure 9 shows the two tie rods. Figure 10 shows the transverse beam with its two soles. Figure 11 represents the entire mounted apparatus.

85 En référence à ces dessins le kit comporte : un chariot en fer U de 160 (1) sur lequel sont soudés quatre supports (7) où sont fixés les roulements ( deux supérieurs (6) et deux inférieurs (5), au sommet un anneau de traction (2) où s'accroche le treuil électrique (19), sur les côtés deux oreilles (4) où se fixent les tirants (17), sur l'arrière deux plaques guide (3) et sur le bas deux forages (8) de diamètre 14 pour fixer la poutre centrale.85 with reference to these drawings the kit comprises: a trolley in iron U of 160 (1) on which are welded four supports (7) where are fixed the bearings (two upper (6) and two lower (5), at the top a traction ring (2) where the electric winch (19) is hooked, on the sides two ears (4) where the tie-rods (17) are fixed, on the rear two guide plates (3) and on the bottom two boreholes (8) of diameter 14 for fixing the central beam.

2 Une poutre centrale en U de 160 qui reçoit la roue avant de l'avion( 16) dont une extrémité possède deux forages de diamètre 14 pour la fixer au chariot, à l'autre extrémité est soudée une plaque de fer plat avec deux forages (15 ) pour y boulonner la poutre transversale (9) à l'aide du fer en U soudé sur celle-ci par les forages (18 ). Une poutre transversale en U de 160 (9 ) sur laquelle sont soudées les deux semelles (10 ) qui possèdent deux oreilles (11) sur les côtés extérieurs. Chaque semelle comporte trois renforts (12) soudés également sur la poutre (9 ). Sur ces semelles viennent prendre place les deux roues centrales de l'avion. Les deux tirants (17) sont boulonnés aux oreilles du chariot ( 4 ) et aux oreilles )0 des semelles (11 ), ils donnent la rigidité à l'ensemble. Un support en L (13 ) qui se boulonne sur la charpente métallique du toit qui permet de fixer un treuil électrique (19) pour élever l'ensemble de l'appareil. Une fois l'appareil entièrement monté, lorsqu'il est au sol l'avion vient se positionner la roue avant sur la poutre centrale (16 ) et les deux roues arrière sur les J 5 semelles (10 ). L'avion est maintenu à l'arrêt par une sangle, ensuite à l'aide du treuil électrique (19) on élève le tout le long du pilier du hangar (20) jusqu'à la hauteur voulue. Deux clavetages viennent sécuriser l'ensemble sur le pilier. La place au-dessous est entièrement libérée pour mettre un autre avion. Ce dispositif permet aux petits aérodromes d'augmenter leur capacité d'acceu.l 2 A central U-beam of 160 which receives the front wheel of the aircraft (16), one end of which has two boreholes with a diameter of 14 to attach it to the carriage, at the other end is welded a flat iron plate with two drillings (15) for bolting the transverse beam (9) with the U-iron welded thereon by the boreholes (18). A transverse U-beam 160 (9) on which are welded the two flanges (10) which have two lugs (11) on the outer sides. Each sole comprises three reinforcements (12) also welded to the beam (9). On these soles come to take place the two central wheels of the plane. The two tie rods (17) are bolted to the ears of the carriage (4) and the ears) 0 soles (11), they give rigidity to all. An L-bracket (13) that bolts to the roof metal frame that secures an electric winch (19) to elevate the entire apparatus. Once the aircraft is fully assembled, when it is on the ground the aircraft is positioned the front wheel on the central beam (16) and the two rear wheels on J 5 soles (10). The aircraft is held at a stop by a strap, then using the electric winch (19) is raised all along the pillar of the shed (20) to the desired height. Two keyways secure the whole on the pillar. The place below is fully vacated to put another plane. This device allows small airfields to increase their capacity of acceu.l

Claims (4)

REVENDICATIONS1) Dispositif servant à entreposer en hauteur des petits avions de type U.L.M. dans les hangars à structure métallique caractérisé en ce qu'il est constitué d'un kit de cinq éléments dont un chariot (1) où est fixé la partie centrale (16), d'une plateforme pourvue d'une poutre transversale (9) avec ses deux semelles (10), deux tirants (17) qui assurent la rigidité de l'ensemble et un support de treuil (13). CLAIMS1) Device for storing high level U.L.M. in hangars with a metal structure characterized in that it consists of a kit of five elements including a carriage (1) where is fixed the central portion (16), a platform provided with a transverse beam (9) with its two soles (10), two tie rods (17) which ensure the rigidity of the assembly and a winch support (13). 2) Dispositif selon la revendication 1 caractérisé en ce que le chariot (1) roule long du pilier en I du hangar (20) à l'aide de ses quatre roulements ( 5 et 6 ). 2) Device according to claim 1 characterized in that the carriage (1) rolls along the I-pillar of the shed (20) with its four bearings (5 and 6). 3) Dispositif selon la revendication 1 en ce que la poutre centrale (16) est un fer en U de 160 mm. JO 3) Device according to claim 1 in that the central beam (16) is a U-shaped iron 160 mm. OJ 4) Dispositif selon la revendication 1 en ce que la poutre transversale (9) supporte les deux semelles (10) qui sont fixées sur elle. 4) Device according to claim 1 in that the transverse beam (9) supports the two flanges (10) which are fixed on it.
FR0801806A 2008-04-02 2008-04-02 Ultralight motorized small airplane i.e. tourism airplane, storing device for use with hanger, has transversal post provided with baseplates, wrench fixed to support and lifting airplane, and tie-rods assuring rigidity of assembly Pending FR2929592A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0801806A FR2929592A1 (en) 2008-04-02 2008-04-02 Ultralight motorized small airplane i.e. tourism airplane, storing device for use with hanger, has transversal post provided with baseplates, wrench fixed to support and lifting airplane, and tie-rods assuring rigidity of assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0801806A FR2929592A1 (en) 2008-04-02 2008-04-02 Ultralight motorized small airplane i.e. tourism airplane, storing device for use with hanger, has transversal post provided with baseplates, wrench fixed to support and lifting airplane, and tie-rods assuring rigidity of assembly

Publications (1)

Publication Number Publication Date
FR2929592A1 true FR2929592A1 (en) 2009-10-09

Family

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FR0801806A Pending FR2929592A1 (en) 2008-04-02 2008-04-02 Ultralight motorized small airplane i.e. tourism airplane, storing device for use with hanger, has transversal post provided with baseplates, wrench fixed to support and lifting airplane, and tie-rods assuring rigidity of assembly

Country Status (1)

Country Link
FR (1) FR2929592A1 (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3954197A (en) * 1971-08-27 1976-05-04 Dean Charles W Method of storing aircraft
US5141371A (en) * 1990-07-12 1992-08-25 Pish Paul J Apparatus for lifting and storing aircraft
US5645388A (en) * 1995-09-27 1997-07-08 Lacasse; Maurice Cantilever lift assembly for stationary small aircraft

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3954197A (en) * 1971-08-27 1976-05-04 Dean Charles W Method of storing aircraft
US5141371A (en) * 1990-07-12 1992-08-25 Pish Paul J Apparatus for lifting and storing aircraft
US5645388A (en) * 1995-09-27 1997-07-08 Lacasse; Maurice Cantilever lift assembly for stationary small aircraft

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