FR2636523A1 - Mobile stretcher support for helicopter - Google Patents
Mobile stretcher support for helicopter Download PDFInfo
- Publication number
- FR2636523A1 FR2636523A1 FR8812326A FR8812326A FR2636523A1 FR 2636523 A1 FR2636523 A1 FR 2636523A1 FR 8812326 A FR8812326 A FR 8812326A FR 8812326 A FR8812326 A FR 8812326A FR 2636523 A1 FR2636523 A1 FR 2636523A1
- Authority
- FR
- France
- Prior art keywords
- stretcher
- helicopter
- support
- cabin
- stretcher support
- 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.)
- Withdrawn
Links
- 238000006073 displacement reaction Methods 0.000 claims description 3
- VJYFKVYYMZPMAB-UHFFFAOYSA-N ethoprophos Chemical compound CCCSP(=O)(OCC)SCCC VJYFKVYYMZPMAB-UHFFFAOYSA-N 0.000 description 2
- 101100045694 Caenorhabditis elegans art-1 gene Proteins 0.000 description 1
- 206010036590 Premature baby Diseases 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 108010066057 cabin-1 Proteins 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61G—TRANSPORT, PERSONAL CONVEYANCES, OR ACCOMMODATION SPECIALLY ADAPTED FOR PATIENTS OR DISABLED PERSONS; OPERATING TABLES OR CHAIRS; CHAIRS FOR DENTISTRY; FUNERAL DEVICES
- A61G3/00—Ambulance aspects of vehicles; Vehicles with special provisions for transporting patients or disabled persons, or their personal conveyances, e.g. for facilitating access of, or for loading, wheelchairs
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61G—TRANSPORT, PERSONAL CONVEYANCES, OR ACCOMMODATION SPECIALLY ADAPTED FOR PATIENTS OR DISABLED PERSONS; OPERATING TABLES OR CHAIRS; CHAIRS FOR DENTISTRY; FUNERAL DEVICES
- A61G1/00—Stretchers
- A61G1/06—Supports for stretchers, e.g. to be placed in or on vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61G—TRANSPORT, PERSONAL CONVEYANCES, OR ACCOMMODATION SPECIALLY ADAPTED FOR PATIENTS OR DISABLED PERSONS; OPERATING TABLES OR CHAIRS; CHAIRS FOR DENTISTRY; FUNERAL DEVICES
- A61G2220/00—Adaptations of particular transporting means
- A61G2220/10—Aircrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D2011/0069—Rest berths, beds or the like
- B64D2011/0092—Arrangements for mounting stretchers in aircraft cabins
Landscapes
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Animal Behavior & Ethology (AREA)
- General Health & Medical Sciences (AREA)
- Veterinary Medicine (AREA)
- Accommodation For Nursing Or Treatment Tables (AREA)
Abstract
Description
SUPPORT MOBILE bE CIVIERE POUR HELICOPTERE
La présente invention se rapporte â un
support de civière pour hélicoptere, elle se rapporte
pLus preciserent â un support mobiLe destiné à recevoir
dans ta cabine d'un hélicoptère une civière ou un
objet analogue tel que par exemple un incubateur
pour bébé prématuré. MOBILE HOLDER BE CIVIERE FOR HELICOPTER
The present invention relates to a
stretcher support for helicopter, it relates
MORE SPECIFIED TO A MOBILE MEDIUM FOR RECEIVING
in your helicopter cabin a stretcher or a
analogous object such as for example an incubator
for premature baby.
Les hélicopteres sont utilisés de pLus
en plus pour le transport des bLessés et des maLades
nécessitant des soins urgents. IL est bien envident
que ce transport doit se faire Le pLus rapidement
possible et dans Les meiLleures conditions.Helicopters are used more
in addition for the transport of wounded and sick
needing urgent care. HE is well envident
that this transport must be done ASAP
possible and under the best conditions.
Parmi les nombreux supports de civière
utiLisés dans La technique antérieure1 on peut citer
celui qui est décrit dans te brevet français 2 366 010
déposé te 30 Septembre 1976. Dans ce brevet, on décrit
un support et une civière qui permettent de résoudre
plusieurs problèmes qui se présentent en cours d'utiLi
sation en vue d'améliorer Le confort des bLessés
ou des maLades.A savoir Le probLème de L'incLinaison
de L'héLicoptere de façon à stassurer que le bLessé
ou Le maLade puisse avoir Les pieds Légèrement suréLe
vés par rapport à la tete, Le problème de La diminution
des vibrations, de La recherche d'un meilleur confort
compte tenu de l'espace généralement réduit de L'habi
tac le et des instruments à transporter et enfin Le problème qui presente des anaLogies avec ce Lui que
parvient à résoudre La présente invention, à savoir
de celui du montage et du démontage de la civière
dans les meiLLeures conditions possibles de confort
et de rapidite.Among the many stretcher supports
used in the prior art1 we can cite
the one described in the French patent 2,366,010
filed on September 30, 1976. In this patent, we describe
a support and a stretcher which allow to solve
several problems that arise during use
to improve comfort for the injured
or patients. Namely the problem of tilting
of the helicopter so as to ensure that the injured
or the patient may have feet that are slightly safe
vés compared to the head, The problem of The decrease
vibrations, the search for better comfort
given the generally small space of L'habi
tackle and the instruments to be transported and finally The problem which presents analogies with this Him that
manages to solve the present invention, namely
the assembly and disassembly of the stretcher
in the best possible conditions of comfort
and speed.
La civière décrite dans ce brevet est munie
sur son fond de deux pièces profitées constituant
une gLissière évasée vers L'avant et dans laquelle peut coulisser une saiLLie servant de pivot montée sur Le support. L'équipement ainsi prévu est reLativement complexe et ne peut s'appLiquer qu'à une civière équipée sur son fond d'une glissière de forme spéciaLe.The stretcher described in this patent is provided
on its bottom two pieces made up constituting
a slide flared towards the front and in which a projection serving as a pivot mounted on the support can slide. The equipment thus provided is relatively complex and can only be applied to a stretcher fitted on its bottom with a special shaped slide.
D'autres supports utiLisés actueLLement sont montés sur Le pLancher de La cabine de piLotage entre d'une part de L'avant vers L'arrière La paroi avant de La carlingue et La paroi arrière de La cabine de pilotage et d'autre part entre Les sièges du pilote et du personneL hospitalier et La porte d'accès à
La cabine. La mise en pLace de La civière et son extraction sont maL commodes car même si Le support est agencé pour pouvoir tourner iL est Limité dans sa rotation comme on le verra plues en détaiL dans
La suite du présent exposé du fait qu'iL vient buter contre La console du tabLeau de bord.Other supports currently used are mounted on the deck of the cab between on the one hand from the front to the rear The front wall of the cabin and the rear wall of the cockpit and on the other hand between The pilot and hospital staff seats and the access door to
The cabin. The positioning of the stretcher and its extraction are very convenient because even if the support is arranged to be able to turn it is limited in its rotation as we will see more in detail in
The rest of this presentation of the fact that it comes up against the console of the dashboard.
La présente invention a pour but de fournir un support pour civière qui ne présente pas Les inconvénients indiqués ci-dessus en ce sens qu'iL s'oriente à voLonté et aisément, soit pour recevoir La civière, soit pour permettre son évacuation rapide. The object of the present invention is to provide a support for a stretcher which does not have the drawbacks indicated above in the sense that it is oriented at will and easily, either to receive the stretcher or to allow its rapid evacuation.
Le support mobiLe de civière ou d'incubateur pour hélicoptère conforme à L'invention est destiné à être installé de façon amovibLe sur Le plancher de La cabine de piLotage, essentieLLement entre d'une part Les parois avant et arrière de La cabine et d'autre part, au voisinage de La porte d'entrée de
La cabine dans La partie non occupée par Les sièges du piLote et du personnel hospitalier. Ce support est caractérisé en ce qu'il est équipé de moyens
Lui permettant d'être déplacé entre une position occupée notamment Lors du transport aérien, paraLLèLe à L'axe de L'hélicoptère et une position de réception ou d'évacuation de La civière à angLe droit par rapport à L'axe de L'hélicoptère. The movable stretcher or incubator support for a helicopter in accordance with the invention is intended to be removably installed on the floor of the cab, essentially between the front and rear walls of the cabin and on the other hand, near the front door of
The cabin in the part not occupied by the seats of the driver and the hospital staff. This support is characterized in that it is equipped with means
Allowing it to be moved between an occupied position, notably during air transport, parallel to the axis of the helicopter and a position for receiving or evacuating the stretcher at right angles to the axis of the helicopter. .
Grâce à cet agencement et comme on Le constatera mieux encore dans la suite de L'exposé, le support de civiere se manipule aisément en pouvant être orienté progressivement sans être gêné par la présence de
La consoLe du poste de piLotage.Thanks to this arrangement and as will be seen even better in the rest of the presentation, the stretcher support is easy to handle, being able to be oriented gradually without being hindered by the presence of
THE CONSOLE OF THE PLANTING POST.
D'autres avantages et caractéristiques de L'invention ressortiront d'ailleurs de La description qui suit de queLques modes de réaLisation donnés en référence aux dessins annexés : - La figure 1 représente L'intérieur d'une cabine
de pilotage dans LaqueLle est monté un support
mobile pour civière de type courant de L'art anté
rieur.Other advantages and characteristics of the invention will appear moreover from the following description of that certain embodiments given with reference to the appended drawings: - Figure 1 represents the interior of a cabin
in LaqueLle is mounted a support
mobile for stretcher of the current type of art anté
laughing.
- La figure 2 est également une vue de L'intérieur
d'une cabine d'hélicoptère, celte-ci étant toutefois
équipée d'un support mobile pour civière conforme
à L'invention.- Figure 2 is also a view of the interior
a helicopter cabin, this being however
equipped with a movable support for compliant stretcher
to the invention.
- La figure 3 est une vue de dessus du support de
civiere conforme à L'invention en position verrouil
Lée sur le pLancher de La cabine d'un héLicoptère. - Figure 3 is a top view of the support
stretcher according to the invention in the locked position
Lée on the plLetter of the cabin of a helicopter.
- La figure 4 représente Le support de civière conforme
à L'invention en vue Latérale.- Figure 4 shows The stretcher support conform
to the invention in side view.
- La figure 5 est une vue agrandie d'un élément de
verrouiLlage d'une béquille du support de civière.- Figure 5 is an enlarged view of an element of
latching a stretcher support strut.
- La figure 6 est une représentation schématique
de différentes positions occupées par Le support
de civiere au cours de son dépLacement.- Figure 6 is a schematic representation
different positions occupied by the support
of stretcher during its displacement.
- La figure 7 est une représentation LatéraLe en
coupe du bras articuLé sur Lequel repose en partie
Le support de civière.- Figure 7 is a lateral representation in
section of the articulated arm on which partly rests
The stretcher support.
Comme on peut Le voir sur La figure 1, ta cabine 1 d'un héLicoptère qui repose sur deux patins 3 est équipée d'un support mobile 5 de L'art anterieur qui peut tourner d'un certain angLe autour d'un axe de rotation 6 au-dessus d'un cadre de renfor cement 7 fixé sur Le pLancher de La cabine. La civière 9 représentée en pointilLé se pose sur Le support mobiLe sur lequel elle peut rouler en se dirigeant vers l'avant Lors de sa réception ou en se dirigeant vers L'arrière Lors de son évacuation. Dans son mouvement de rotation vers l'extérieur, le support est
Limité du fait qu'iL vient buter contre La consoLe 11 du tableau de bord.En conséquence, L'entrée ou
La sortie de La civiere ne peut se faire que de biais et entre Le côté droit de La civiere et Le montant de L'embrasure du battant droit de ta porte 13 de l'héLicoptère iL nly a pas d'espace suffisant permettant à un homme de se placer entre le support de civière et Le battant droit de La porte afin d'intervenir et de faciliter les manoeuvres.As can be seen in Figure 1, your cabin 1 of a helicopter which rests on two skids 3 is equipped with a movable support 5 of the prior art which can rotate at a certain angle around an axis of rotation 6 above a reinforcing frame 7 fixed to the cabin plank. The stretcher 9 shown in dotted lines is placed on the movable support on which it can roll, moving forwards during its reception or by moving towards the rear during its evacuation. In its outward rotation, the support is
Limited by the fact that it comes into contact with the console 11 on the dashboard.
The exit from La Civiere can only be done at an angle and between the right side of La Civiere and the amount of the embrasure of the right wing of your door 13 of the helicopter. There is not enough space allowing a man to be placed between the stretcher support and the right leaf of the door in order to intervene and facilitate the maneuvers.
Le support de civière 15 conforme à L'invention tel qu'il apparat sur La figure 2 est prêt à recevoir une civiere. IL est monté à angle droit par rapport à L'axe de l'hélicoptère. IL repose à sa partie arrière sur une première extrémité 17 d'un premier bras articulé 19 comme on peut le voir sur
La figure 7, alors que sa partie avant repose sur un guide 21 par L'intermédiaire d'un élément de guidage cylindrique 23. Le premier bras articulé 19 a son autre extrémité 25 qui peut tourner autour d'un axe 27 maintenu entre Les deux joues d'une chape 29.The stretcher support 15 according to the invention as it appears in Figure 2 is ready to receive a stretcher. It is mounted at right angles to the axis of the helicopter. It rests at its rear part on a first end 17 of a first articulated arm 19 as can be seen on
FIG. 7, while its front part rests on a guide 21 by means of a cylindrical guide element 23. The first articulated arm 19 has its other end 25 which can rotate around an axis 27 held between the two cheeks of a clevis 29.
Un second bras 31 a sa premiere extrémité 33 fixée entre Les deux joues de La chape 29 et sa seconde extrémité 35 qui peut tourner autour d'un axe 37 dont l'assise 39 est fixée sur Le plancher 41 de L'héLicoptère. A second arm 31 has its first end 33 fixed between the two cheeks of the yoke 29 and its second end 35 which can rotate about an axis 37 whose seat 39 is fixed on the floor 41 of the helicopter.
Comme on peut Le voir sur La figure 2,
Le bras 31 est doubLe pour être renforcé, il est en outre équipe à sa partie inférieure d'une roulette d'allégement 40. As can be seen in Figure 2,
The arm 31 is doubLe to be reinforced, it is further equipped at its lower part with a lightening wheel 40.
Comme on peut Le voir sur la figure 3,
Le mouvement de rotation du bras 31 est limité vers
L'intérieur de la cabine par une butée 43 et vers
L'extérieur par une butée 45. Un élément de verrouil Lage 44 assure Le maintien en position du support de civière pendant Le transport. Le support 15 est doté à sa partie avant et dessous d'un éLément de guidage 21 porteur de L'élément cylindrique 23 comportant un alésage 49 qui peut se déplacer Le long du guide rectiligne 21 porté par deux flasques 51 et 52 fixes au plancher.As can be seen in Figure 3,
The rotational movement of the arm 31 is limited towards
The interior of the cabin by a stop 43 and towards
The exterior by a stop 45. A Lage 44 locking element ensures the maintenance in position of the stretcher support during transport. The support 15 is provided at its front and bottom part with a guide element 21 carrying the cylindrical element 23 comprising a bore 49 which can move along the rectilinear guide 21 carried by two flanges 51 and 52 fixed to the floor.
Le support 15 est équipe d'une béquilLe 54 qui peut être maintenue au repos par un élément de verrouiLlage 56 ou être amenée en position d'appui sur Le patin 3 de L'hélicoptère. The support 15 is equipped with a stand 54 which can be kept at rest by a locking element 56 or be brought into the support position on the pad 3 of the helicopter.
Sur la figure 6, on peut distinguer schématiquement quatre positions occupées par le support de civière lors des manoeuvres :
- une première position en trait plein dans Laquelle Le support est parallèle à L'axe de L'hélicoptère, L'élément cylindrique 23 se trouve en bout de course au voisinage du flasque 51, les bras 31 et 19 se trouvent aLors rapprochés t'un de
L'autre.In FIG. 6, we can schematically distinguish four positions occupied by the stretcher support during the maneuvers:
- A first position in solid line in which the support is parallel to the axis of the helicopter, the cylindrical element 23 is located at the end of travel in the vicinity of the flange 51, the arms 31 and 19 are then brought together. a die
The other.
- Une seconde position en trait mixte dans laquelte L'élément de cylindre 23 s'éLoigne du fLasque 51 pour se diriger vers Le fLasque 52. - A second position in phantom in which the cylinder element 23 moves away from the plate 51 to go towards the plate 52.
- Une troisième position en pointillé. On note ta position de l'élément cylindrique 23 qui se rapproche du fLasque 51. - A third dotted position. We note your position of the cylindrical element 23 which approaches the plate 51.
- Une quatrième position en trait plein fin, L'élément cylindrique 23 est arrivé en fin de course au voisinage du flasque 52. - A fourth position in full solid line, the cylindrical element 23 has reached the end of the race in the vicinity of the flange 52.
On peut observer qu'au cours du déplacement du support de civière à partir de La premiere position
Le bras 31 tourne Légèrement vers la gauche alors que le bras 19 tourne en s'ouvrant vers te bas de
La figure jusqu'à former un angLe droit avec La position qu'iL occupait au départ dans sa première position.We can observe that during the movement of the stretcher support from the first position
The arm 31 turns slightly to the left while the arm 19 turns while opening downwards
The figure up to form a right angle with the position it occupied at the start in its first position.
On voit donc, et c'est important, que Le support de civière contrairement à ce qui se produit dans Le cas de la figure 1 de L'art antérieur, peut tourner sans que sa partie avant ne vienne se heuter à La console du tabLeau de bord. Ce résultat est obtenu grâce à L'action conjuguee d'une part du guide 21 qui impose un dépLacement rectiligne de L'élément cylindrique 23 et d'autre part des bras articules 19 et 31 qui assure La rotation simultanée du support de civière. It is therefore seen, and this is important, that the stretcher support, unlike what occurs in the case of FIG. 1 of the prior art, can rotate without its front part coming to crash into the console of the table. of edge. This result is obtained thanks to the combined action on the one hand of the guide 21 which requires a rectilinear displacement of the cylindrical element 23 and on the other hand of the articulated arms 19 and 31 which ensures the simultaneous rotation of the stretcher support.
Ainsi, Le support de civière ne . se trouve jamais entravé dans son mouvement de rotation puisque sa partie avant ne se heurte plus à la console de
La cabine. En outre, iL peut se déplacer pour former un angLe droit avec La position qu 'iL occupe tors de son installation dans La cabine de l'hélicoptère. Thus, the stretcher support does. is never hampered in its rotational movement since its front part no longer collides with the console
The cabin. In addition, iL can move to form a right angle with the position iL occupies when it is installed in the helicopter cabin.
C'est Là une position idéale qui facilite l'accès du personnel hospitalier tant à L'entrée qu'à la sortie de La civière.This is an ideal position which facilitates the access of hospital staff both at the entrance and at the exit of La Civière.
Il est bien entendu que Le mode de reaLisation du support de civière conforme à L'invention teL qu'il a été décrit ci-dessus à titre préférentiel n'est nullement limitatif et que de nombreuses modifications et variations pourront y être apportees par
Les spécialistes sans se departir pour autant ni du cadre ni de l'esprit de L'invention. It is understood that the method of carrying out the stretcher support in accordance with the invention, as it has been described above on a preferential basis, is in no way limiting and that numerous modifications and variations may be made thereto by
The specialists without departing from the framework or the spirit of the invention.
Claims (6)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR8812326A FR2636523A1 (en) | 1988-09-21 | 1988-09-21 | Mobile stretcher support for helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR8812326A FR2636523A1 (en) | 1988-09-21 | 1988-09-21 | Mobile stretcher support for helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR2636523A1 true FR2636523A1 (en) | 1990-03-23 |
Family
ID=9370224
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR8812326A Withdrawn FR2636523A1 (en) | 1988-09-21 | 1988-09-21 | Mobile stretcher support for helicopter |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR2636523A1 (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2682930A1 (en) * | 1991-10-28 | 1993-04-30 | Heli Rhone Alpes | Medical installation, especially for a helicopter |
| EP1247738A3 (en) * | 2001-04-04 | 2003-02-26 | Agusta S.p.A. | Rescue vehicle |
| DE10116096C2 (en) * | 2001-03-30 | 2003-12-18 | Wietmarscher Ambulanz Und Sond | Palanquin locking |
| WO2010034967A1 (en) * | 2008-09-23 | 2010-04-01 | Boyd Maunsell Michael Francis | Support |
| FR2989574A1 (en) * | 2012-04-23 | 2013-10-25 | Nexter Systems | Device for assisting loading and unloading of stretcher in and out of e.g. military vehicle for transporting injured persons in stretcher, has arms articulated to move support between loading/unloading position and transfer position |
| EP3590481A1 (en) | 2018-07-05 | 2020-01-08 | AEREA S.p.A. | A device for handling a helicopter stretcher |
| CN111150562A (en) * | 2019-11-15 | 2020-05-15 | 陕西飞机工业（集团）有限公司 | Stretcher rescue equipment used on airplane |
| CN114903700A (en) * | 2021-12-22 | 2022-08-16 | 三河科达实业有限公司 | High-mobility field-operation emergency ambulance capable of being rapidly loaded and unloaded by stretcher |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2309735A (en) * | 1940-04-26 | 1943-02-02 | Arthur L Koch | Vehicle construction |
| FR1004309A (en) * | 1947-04-03 | 1952-03-28 | Christian Miesen | Device allowing the installation of stretchers in vehicles of all types and, in particular, in tourist motor cars |
| DE1161386B (en) * | 1961-09-12 | 1964-01-16 | Lorcher Karosseriefabrik Binz | Laterally swiveling stretcher platform for ambulances |
| CH415954A (en) * | 1961-08-02 | 1966-06-30 | Binz & Co | Stretcher platform with guide, by means of which the platform can be moved in an at least approximately horizontal plane, in particular for stretchers in ambulances |
| FR2332003A2 (en) * | 1975-11-24 | 1977-06-17 | Piguillem Sauveur | Sledge type rescue stretcher - is placed horizontally opposite helicopter cabin and hauled in up ramp by flexible sling on guide rope |
| FR2366010A1 (en) * | 1976-09-30 | 1978-04-28 | Paris Direction Serv Tech Vill | Rescue stretcher system for helicopter use - can be loaded onto support from side and has foot end higher than head and fitted with vibration dampers |
| EP0005424A2 (en) * | 1978-05-01 | 1979-11-14 | United Technologies Corporation | Apparatus for synchronously elevating and lowering air-ambulance litter with crash attenuation |
| FR2480206A1 (en) * | 1980-04-10 | 1981-10-16 | Okey | Vehicle seat for handicapped people - pivots from one locked position inside to another position outside vehicle |
-
1988
- 1988-09-21 FR FR8812326A patent/FR2636523A1/en not_active Withdrawn
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2309735A (en) * | 1940-04-26 | 1943-02-02 | Arthur L Koch | Vehicle construction |
| FR1004309A (en) * | 1947-04-03 | 1952-03-28 | Christian Miesen | Device allowing the installation of stretchers in vehicles of all types and, in particular, in tourist motor cars |
| CH415954A (en) * | 1961-08-02 | 1966-06-30 | Binz & Co | Stretcher platform with guide, by means of which the platform can be moved in an at least approximately horizontal plane, in particular for stretchers in ambulances |
| DE1161386B (en) * | 1961-09-12 | 1964-01-16 | Lorcher Karosseriefabrik Binz | Laterally swiveling stretcher platform for ambulances |
| FR2332003A2 (en) * | 1975-11-24 | 1977-06-17 | Piguillem Sauveur | Sledge type rescue stretcher - is placed horizontally opposite helicopter cabin and hauled in up ramp by flexible sling on guide rope |
| FR2366010A1 (en) * | 1976-09-30 | 1978-04-28 | Paris Direction Serv Tech Vill | Rescue stretcher system for helicopter use - can be loaded onto support from side and has foot end higher than head and fitted with vibration dampers |
| EP0005424A2 (en) * | 1978-05-01 | 1979-11-14 | United Technologies Corporation | Apparatus for synchronously elevating and lowering air-ambulance litter with crash attenuation |
| FR2480206A1 (en) * | 1980-04-10 | 1981-10-16 | Okey | Vehicle seat for handicapped people - pivots from one locked position inside to another position outside vehicle |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2682930A1 (en) * | 1991-10-28 | 1993-04-30 | Heli Rhone Alpes | Medical installation, especially for a helicopter |
| DE10116096C2 (en) * | 2001-03-30 | 2003-12-18 | Wietmarscher Ambulanz Und Sond | Palanquin locking |
| EP1247738A3 (en) * | 2001-04-04 | 2003-02-26 | Agusta S.p.A. | Rescue vehicle |
| US6585188B2 (en) | 2001-04-04 | 2003-07-01 | Agusta S.P.A. | Rescue vehicle |
| WO2010034967A1 (en) * | 2008-09-23 | 2010-04-01 | Boyd Maunsell Michael Francis | Support |
| FR2989574A1 (en) * | 2012-04-23 | 2013-10-25 | Nexter Systems | Device for assisting loading and unloading of stretcher in and out of e.g. military vehicle for transporting injured persons in stretcher, has arms articulated to move support between loading/unloading position and transfer position |
| EP3590481A1 (en) | 2018-07-05 | 2020-01-08 | AEREA S.p.A. | A device for handling a helicopter stretcher |
| CN111150562A (en) * | 2019-11-15 | 2020-05-15 | 陕西飞机工业（集团）有限公司 | Stretcher rescue equipment used on airplane |
| CN111150562B (en) * | 2019-11-15 | 2022-03-15 | 陕西飞机工业（集团）有限公司 | Stretcher rescue equipment used on airplane |
| CN114903700A (en) * | 2021-12-22 | 2022-08-16 | 三河科达实业有限公司 | High-mobility field-operation emergency ambulance capable of being rapidly loaded and unloaded by stretcher |
| CN114903700B (en) * | 2021-12-22 | 2022-12-13 | 三河科达实业有限公司 | High maneuvering type field emergency ambulance capable of rapidly loading and unloading stretcher |
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Legal Events
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| ST | Notification of lapse |