公开(公告)号：US20150225073A1

公开(公告)日：2015-08-13

申请号：US14426955

申请日：2013-09-09

Applicant: AIRBUS GROUP SAS

Inventor： Michel Bermudez ,  Didier Mesnage ,  Hichem Smaoui ,  Benoit Fleury

IPC: B64C7/00 ,  B64D41/00 ,  B64C1/40 ,  H01G11/58 ,  H01G11/78

CPC classification number: B64C7/00 ,  B64C1/12 ,  B64C1/40 ,  B64C2001/0072 ,  B64D41/00 ,  H01G11/58 ,  H01G11/78 ,  Y02T50/43 ,  Y10T29/435 ,  Y10T29/49622

Abstract: A method of manufacturing a stiffened panel having a skin and at least one substantially elongate stiffener having a longitudinal groove forming a cavity. At least one storage device for storing and releasing electrical energy. The longitudinal groove is filled with at least one storage device for storing and releasing electrical energy. The storage device is covered with a skin which forms the cavity together with the longitudinal groove of the stiffener. A stiffened ring can be derived from the method.

Abstract translation: 一种制造具有皮肤的加强板的方法和具有形成空腔的纵向槽的至少一个基本上细长的加强件。 用于存储和释放电能的至少一个存储装置。 纵向凹槽填充有用于存储和释放电能的至少一个存储装置。 存储装置被覆盖有与加强件的纵向槽一起形成空腔的皮肤。 可以从该方法得到加强环。

公开(公告)号：US09677466B2

公开(公告)日：2017-06-13

申请号：US14966180

申请日：2015-12-11

Applicant: AIRBUS GROUP SAS

Inventor： Hichem Smaoui ,  Bruno Rechain ,  Fabien Retho

IPC: F02B65/00 ,  B64C39/02 ,  F02B37/00 ,  F02B33/40 ,  F01D15/10 ,  F02C6/12 ,  F02C6/14 ,  F02C6/20 ,  B60K6/24 ,  B60K6/38 ,  B60K6/40 ,  B60K6/44 ,  B60K6/387 ,  B60K6/442 ,  B64D27/02

CPC classification number: F02B65/00 ,  B60K6/24 ,  B60K6/387 ,  B60K6/40 ,  B60K6/442 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/042 ,  B64C2201/048 ,  B64D2027/026 ,  F01D15/10 ,  F02B33/40 ,  F02B37/00 ,  F02C6/12 ,  F02C6/14 ,  F02C6/206 ,  F05D2220/329 ,  F05D2220/40 ,  F05D2220/62 ,  F05D2220/76 ,  F05D2220/90 ,  F05D2260/42 ,  Y02T10/144 ,  Y02T10/6234 ,  Y02T10/6295 ,  Y02T50/64 ,  Y02T50/671

Abstract: A method of managing a power demand to assure the operation of a pilotless aircraft. The aircraft includes an internal combustion engine supplying a maximum principal power which can vary. The management method is particularly suitable for a rotary wing pilotless aircraft. It guarantees the storage of an amount of electrical energy at least equal to a recovery energy of the aircraft in the event of failure of the internal combustion engine. This recovery energy enables the control of autorotation and landing of the aircraft.

公开(公告)号：US09643713B2

公开(公告)日：2017-05-09

申请号：US14426955

申请日：2013-09-09

Applicant: AIRBUS GROUP SAS

Inventor： Michel Bermudez ,  Didier Mesnage ,  Hichem Smaoui ,  Benoit Fleury

IPC: H01G9/155 ,  B64C7/00 ,  B64D41/00 ,  B64C1/12 ,  B64C1/40 ,  H01G11/58 ,  H01G11/78 ,  B64C1/00

CPC classification number: B64C7/00 ,  B64C1/12 ,  B64C1/40 ,  B64C2001/0072 ,  B64D41/00 ,  H01G11/58 ,  H01G11/78 ,  Y02T50/43 ,  Y10T29/435 ,  Y10T29/49622

Abstract: A method of manufacturing a stiffened panel having a skin and at least one substantially elongate stiffener having a longitudinal groove forming a cavity. At least one storage device for storing and releasing electrical energy. The longitudinal groove is filled with at least one storage device for storing and releasing electrical energy. The storage device is covered with a skin which forms the cavity together with the longitudinal groove of the stiffener. A stiffened ring can be derived from the method.