[go: up one dir, main page]

ES2571061B1 - Propeller protection system for unmanned aerial vehicles - Google Patents

Propeller protection system for unmanned aerial vehicles Download PDF

Info

Publication number
ES2571061B1
ES2571061B1 ES201400927A ES201400927A ES2571061B1 ES 2571061 B1 ES2571061 B1 ES 2571061B1 ES 201400927 A ES201400927 A ES 201400927A ES 201400927 A ES201400927 A ES 201400927A ES 2571061 B1 ES2571061 B1 ES 2571061B1
Authority
ES
Spain
Prior art keywords
protection
unmanned aerial
aerial vehicles
plates
protection system
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.)
Active
Application number
ES201400927A
Other languages
Spanish (es)
Other versions
ES2571061A1 (en
Inventor
Pablo NEIRA LÓPEZ
David ROCA BERNÁRDEZ
Borja CONDE CARNERO
Belén Riveiro Rodríguez
Higinio González Jorge
Pedro ARIAS SÁNCHEZ
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Universidade de Vigo
Original Assignee
Universidade de Vigo
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Universidade de Vigo filed Critical Universidade de Vigo
Priority to ES201400927A priority Critical patent/ES2571061B1/en
Publication of ES2571061A1 publication Critical patent/ES2571061A1/en
Application granted granted Critical
Publication of ES2571061B1 publication Critical patent/ES2571061B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • B64C39/024Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • B64U10/13Flying platforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/13Propulsion using external fans or propellers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Lighting Device Outwards From Vehicle And Optical Signal (AREA)
  • Road Signs Or Road Markings (AREA)

Abstract

La presente invención ofrece un sistema de protección para las hélices de vehículos aéreos no tripulados compuesto por una pieza principal (protección) y dos pletinas que actúan como sujeción a los brazos del vehículo. Para tener en cuenta distintas disposiciones, se incluyen dos montajes diferentes que tienen en cuenta la presencia o no de un sistema de iluminación, por lo que las pletinas a utilizar en cada caso serán diferentes. Así mismo, la parte del encastre de la protección posee una geometría diseñada para facilitar la integración con el vehículo.The present invention offers a protection system for the propellers of unmanned aerial vehicles consisting of a main part (protection) and two plates that act as fastening to the arms of the vehicle. To take into account different arrangements, two different assemblies are included that take into account the presence or not of a lighting system, so the plates to be used in each case will be different. Likewise, the protection insert has a geometry designed to facilitate integration with the vehicle.

Description

55

1010

15fifteen

20twenty

2525

3030

3535

4040

45Four. Five

50fifty

DESCRIPCIONDESCRIPTION

Sistema de protection de helices para vehteulo aereo no tripulado.Propeller protection system for unmanned aerial vehicles.

La presente invention se refiere a la conception de una pieza protectora en polietileno para las helices de un vehiculo aereo no tripulado.The present invention relates to the conception of a protective piece in polyethylene for the propellers of an unmanned aerial vehicle.

Antecedentes de la invencionBackground of the invention

En muchas ocasiones los vehiculos aereos no tripulados tipo multi-rotor se emplean para la toma de imagenes aereas e inspection de infraestructuras utilizando camaras termograficas y RGB. Dichos vehiculos disponen, entre otros elementos, de un sistema de posicionamiento por GPS, un sensor barometrico y un controlador de vuelo que le permiten mantener una position y altura prefijadas sin aumentar excesivamente la carga de trabajo del piloto.In many cases, multi-rotor unmanned aerial vehicles are used for aerial imaging and infrastructure inspection using thermographic and RGB cameras. These vehicles have, among other elements, a GPS positioning system, a barometric sensor and a flight controller that allow you to maintain a preset position and height without excessively increasing the pilot's workload.

Sin embargo, muchos de los trabajos a realizar implican volar en una zona con atenuacion o apantallamiento de la senal GPS (por ejemplo debajo del tablero de un puente). En este caso se hace necesario el control manual por parte del piloto, corrigiendo las posibles perturbaciones externas debidas a rafagas de viento, etc. Se concluye que la necesidad de aproximarse al objeto a analizar para la toma de imagenes, unida a las condiciones del entorno, pueden poner en peligro la integridad estructural del aparato implicando el fracaso de la mision, siendo las helices las partes mas expuestas a sufrir danos severos por impactos.However, many of the work to be done involves flying in an area with attenuation or shielding of the GPS signal (for example under the bridge deck). In this case, manual control by the pilot is necessary, correcting possible external disturbances due to wind gusts, etc. It is concluded that the need to approach the object to be analyzed for the taking of images, together with the surrounding conditions, can jeopardize the structural integrity of the apparatus implying the failure of the mission, the propellers being the most exposed parts to suffer damage. severe by impacts.

Se hace necesaria entonces la concepcion, fabricacion e integracion de unas protecciones capaces de amortiguar los sucesivos contactos que haya entre el vehiculo y la estructura a analizar.It is necessary then the conception, manufacture and integration of protections capable of cushioning the successive contacts between the vehicle and the structure to be analyzed.

Description de la invencionDescription of the invention

Se ha creado una proteccion que fuese facilmente instalable y desmontable ya que existen aplicaciones en las que dichas protecciones no son necesarias. El conjunto se compone de 3 piezas:A protection has been created that is easily installable and removable since there are applications where such protections are not necessary. The set consists of 3 pieces:

- Proteccion: parte principal que desempena la funcion protectora.- Protection: main part that performs the protective function.

- Pletinas #1 y #2: elementos que sirven para unir los brazos del vehiculo a la proteccion por medio de una union atornillada.- Plates # 1 and # 2: elements that serve to join the arms of the vehicle to the protection by means of a bolted joint.

Se pretende que el conjunto resultante aproveche la geometria de los brazos como restricciones a su propio movimiento, reduciendo asi el numero de piezas y por lo tanto el peso.The resulting set is intended to take advantage of the geometry of the arms as restrictions on its own movement, thus reducing the number of pieces and therefore the weight.

Breve descripcion de los dibujosBrief description of the drawings

En este apartado se explican las distintas piezas que conforman la proteccion.This section explains the different pieces that make up the protection.

En la figura 1 se muestra la geometria de la proteccion propiamente dicha. Esta pieza tiene un espesor maximo de 10 mm y forma un abanico protector de 70°. La parteFigure 1 shows the geometry of the protection itself. This piece has a maximum thickness of 10 mm and forms a protective fan of 70 °. The part

55

1010

15fifteen

20twenty

2525

3030

3535

4040

designada como (1) corresponde a la zona del encastre con el brazo que une el motor al cuerpo del dron.designated as (1) corresponds to the area of the insert with the arm that joins the engine to the drone body.

En las figuras 2 y 3 se puede apreciar un detalle de la parte superior e inferior de esta region respectivamente. Se ha eliminado material en (2) para aliviar el peso en una zona no solicitada estructuralmente. En (3) se realiza la union atornillada a las dos pletinas restantes por medio de sendos tornillos de 3 mm de diametro. Las superficies (4) y (6) constituyen topes fisicos para mantener la protection inmovilizada. Cada motor se sujeta a cada brazo mediante dos tornillos cuyas cabezas sobresalen en el interior del brazo 2 mm. Para alojar dichas cabezas se ha creado la region (5). Los brazos que soportan cada motor poseen unos orificios en la parte inferior que son utilizados para fijar la proteccion al brazo. Los dos salientes marcados como (7) cumplen con esta funcion.Figures 2 and 3 show a detail of the upper and lower part of this region respectively. Material has been removed in (2) to relieve weight in an area not structurally requested. In (3) the union is made screwed to the two remaining plates by means of two screws of 3 mm in diameter. The surfaces (4) and (6) constitute physical stops to keep the protection immobilized. Each motor is fastened to each arm by two screws whose heads protrude inside the arm 2 mm. To accommodate these heads, the region (5) has been created. The arms that support each motor have holes in the bottom that are used to fix the protection to the arm. The two projections marked as (7) fulfill this function.

Finalmente las figuras 4 y 5 muestran las pletinas #1 y #2 respectivamente. Ambas atrapan a la proteccion y la fijan verticalmente por medio de dos tornillos.Finally, figures 4 and 5 show plates # 1 and # 2 respectively. Both catch the protection and fix it vertically by means of two screws.

Description de una realization preferidaDescription of a preferred realization

El dron existente posee 8 brazos formados por tubos huecos de aluminio de 10x10 mm de section externa y un espesor de 1 mm. Se encuentran dispuestos en forma cruciforme 4 a 4, con longitudes de 381 mm y 276 mm desde el cuerpo del dron hasta el extremo. Estos brazos son los encargados de alojar a cada uno de los motores. En la figura 6 se muestra la configuration inicial del veticulo.The existing drone has 8 arms formed by hollow aluminum tubes of 10x10 mm of external section and a thickness of 1 mm. They are arranged in a cruciform shape 4 to 4, with lengths of 381 mm and 276 mm from the body of the drone to the end. These arms are responsible for housing each of the engines. Figure 6 shows the initial configuration of the vehicle.

En la parte inferior de los brazos marcados como (8) se encuentran unos dispositivos luminosos para facilitar la orientation del aparato al piloto en condiciones de baja visibilidad. Esto hace que el montaje de las protecciones difiera ligeramente de los brazos restantes:At the bottom of the arms marked as (8) are luminous devices to facilitate the orientation of the apparatus to the pilot in low visibility conditions. This makes the mounting of the protections differ slightly from the remaining arms:

En la figura 7 se muestra una seccion del tubo que usa leds. Solo se emplearan pletinas #1. En la figura 8 se muestra el caso de los 5 brazos restantes, combinando pletinas #1 y #2. Por lo tanto, el numero de pletinas necesarias es de 11 tipo #1 y 5 tipo #2.Figure 7 shows a section of the tube using LEDs. Only # 1 plates will be used. Figure 8 shows the case of the remaining 5 arms, combining plates # 1 and # 2. Therefore, the number of plates required is 11 type # 1 and 5 type # 2.

Para su montaje, inicialmente se introduce la region marcada como (1) de la proteccion en el extremo de un brazo, teniendo en cuenta la correcta position de la parte superior e inferior. Las protuberancias (7) deben quedar encajadas en los respectivos orificios existentes en la parte inferior del brazo de aluminio. El plano inferior de la proteccion debera quedar alineado con la cara inferior del brazo. Finalmente se atornillan dos pletinas #1 a la parte superior e inferior (figura 7) o se realiza el montaje de la figura 8 segun estemos en un brazo con iluminacion o sin ella.For assembly, initially the region marked as (1) of the protection is introduced at the end of an arm, taking into account the correct position of the upper and lower part. The protrusions (7) must fit into the respective holes in the lower part of the aluminum arm. The lower plane of the protection should be aligned with the lower face of the arm. Finally, two # 1 plates are screwed to the upper and lower part (figure 7) or the assembly of figure 8 is carried out according to whether we are on an arm with or without lighting.

En la figura 9 puede verse la parte superior e inferior de una proteccion instalada.Figure 9 shows the upper and lower part of an installed protection.

Claims (1)

ES 2 571 061 A1ES 2 571 061 A1 REIVINDICACIONES 1. El sistema de proteccion de helices para vehteulo aereo no tripulado, consistente en una proteccion en forma de abanico y dos pletinas que permiten la sujecion del conjunto 5 a los brazos del vehiculo por medio de tornillos. La proteccion emplea protuberancias (7) como ayuda a la sujecion.1. The propeller protection system for unmanned aerial vehicles, consisting of a fan-shaped protection and two plates that allow the assembly of the assembly 5 to the arms of the vehicle by means of screws. The protection uses protuberances (7) as an aid to the support.
ES201400927A 2014-11-20 2014-11-20 Propeller protection system for unmanned aerial vehicles Active ES2571061B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES201400927A ES2571061B1 (en) 2014-11-20 2014-11-20 Propeller protection system for unmanned aerial vehicles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES201400927A ES2571061B1 (en) 2014-11-20 2014-11-20 Propeller protection system for unmanned aerial vehicles

Publications (2)

Publication Number Publication Date
ES2571061A1 ES2571061A1 (en) 2016-05-23
ES2571061B1 true ES2571061B1 (en) 2016-12-01

Family

ID=55970565

Family Applications (1)

Application Number Title Priority Date Filing Date
ES201400927A Active ES2571061B1 (en) 2014-11-20 2014-11-20 Propeller protection system for unmanned aerial vehicles

Country Status (1)

Country Link
ES (1) ES2571061B1 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007003458A1 (en) * 2007-01-24 2008-07-31 Diehl Bgt Defence Gmbh & Co. Kg Power supply device for battery-operated small air-craft, has charging device provided for recharging rechargeable battery after implementing flight mission of small air-craft, and landing and loading platform attached to battery magazine
US8322648B2 (en) * 2008-05-15 2012-12-04 Aeryon Labs Inc. Hovering aerial vehicle with removable rotor arm assemblies
GB2483881B (en) * 2010-09-22 2017-04-26 Irps Thomas A dual-function landing gear and rotor protector for a UAV

Also Published As

Publication number Publication date
ES2571061A1 (en) 2016-05-23

Similar Documents

Publication Publication Date Title
ES2754229T3 (en) Unmanned aircraft and procedure for performing a lightning protection measurement in a wind power installation
BR112013007255A8 (en) system, air unit and method for controlling an air unit
SG11201910744WA (en) Vertical take-off and landing unmanned aerial vehicle having foldable fixed wing and based on twin-ducted fan power system
ES2544638T3 (en) Procedure and device for thermal verification of the structural state of wind plants
MX2011011247A (en) SYSTEMS AND METHODS TO RECOVER AND CONTROL THE POST-RECOVERY MOVEMENT OF AN UNTRIPULATED AIRCRAFT.
US20160069299A1 (en) Orientable rocket-motor system
JPWO2017154551A1 (en) Flying object
BR112017026357A2 (en) ?airplane?.
MX2018010786A (en) ASSEMBLY ASSEMBLIES AND METHODS.
RU2017130844A (en) AERODYNAMIC BRAKING SYSTEM FOR DEPARTMENT OF A SATELLITE FROM ORBIT
WO2017058507A3 (en) Portable, controlled environment system
ES2571061B1 (en) Propeller protection system for unmanned aerial vehicles
WO2015114625A8 (en) Methods for operating an air vehicle
ES2549464A1 (en) SALVAMENT SYSTEM
DK3635234T3 (en) AIRCRAFT AIR CONSUMING PROPULSION SYSTEM WITH ISOLATOR WITH OBSTACLE
US10006597B2 (en) Bubble lamp structure for qusai air bubble flow
EA200800855A1 (en) PLANE WITH A UNIVERSAL INTEGRATED RADIO ELECTRONIC COMPLEX
ES1140161U (en) Remote aerial device for measuring environmental variables in closed spaces (Machine-translation by Google Translate, not legally binding)
WO2015136139A1 (en) Viewing system for in-flight refuelling
ES2864215T3 (en) Stratospheric Drone Payload Module Structure
CN106898187A (en) A kind of rotor wing unmanned aerial vehicle landing training platform that takes off
KR20200092022A (en) Drone-mounted lighting system with heat shield in the gimbal and lighting areas
ES2689408T3 (en) Airplane fuselage structure
KR102086655B1 (en) Safety cover for drone
IN2014CH05037A (en)

Legal Events

Date Code Title Description
FG2A Definitive protection

Ref document number: 2571061

Country of ref document: ES

Kind code of ref document: B1

Effective date: 20161201