def createWingFuselageAttachment(parent,
parentUID,
targetUID='fuselage',
typeOfSeg='advDoubletrapezoid'):
if typeOfSeg == 'advDoubletrapezoid':
toFuselageUID = stringUIDBaseType(valueOf_=targetUID)
rib1 = ribIdentificationType(
ribDefinitionUID=stringUIDBaseType(valueOf_='wing_ribs_inner'),
ribNumber=integerBaseType(valueOf_=str(4)))
wingFuselageAttachment = wingFuselageAttachmentType(rib1=rib1)
if typeOfSeg == 'strut':
toFuselageUID = stringUIDBaseType(valueOf_=targetUID)
rib1 = ribIdentificationType(
ribDefinitionUID=stringUIDBaseType(valueOf_='strut_ribs'),
ribNumber=integerBaseType(valueOf_=str(1)))
wingFuselageAttachment = wingFuselageAttachmentType(rib1=rib1)
wingFuselageAttachments = wingFuselageAttachmentsType(
wingFuselageAttachment=[wingFuselageAttachment])
parent.set_wingFuselageAttachments(wingFuselageAttachments)
def createWingFuselageAttachment(parent, parentUID, targetUID='fuselage', typeOfSeg='advDoubletrapezoid'):
if typeOfSeg == 'advDoubletrapezoid':
toFuselageUID = stringUIDBaseType(valueOf_=targetUID)
rib1 = ribIdentificationType(ribDefinitionUID=stringUIDBaseType(valueOf_='wing_ribs_inner'), ribNumber=integerBaseType(valueOf_=str(4)))
wingFuselageAttachment = wingFuselageAttachmentType(rib1=rib1)
if typeOfSeg =='strut':
toFuselageUID = stringUIDBaseType(valueOf_=targetUID)
rib1 = ribIdentificationType(ribDefinitionUID=stringUIDBaseType(valueOf_='strut_ribs'), ribNumber=integerBaseType(valueOf_=str(1)))
wingFuselageAttachment = wingFuselageAttachmentType(rib1=rib1)
wingFuselageAttachments = wingFuselageAttachmentsType(wingFuselageAttachment=[wingFuselageAttachment])
parent.set_wingFuselageAttachments(wingFuselageAttachments)
def createTanks(parent, parentUID, targetUID='tank1', typeOfSeg='advDoubletrapezoid', nRib='2'):
'''
Used for generation of a wing tank
@param parent: ComponentSegment object, wing fuel tank will be added here.
@param typeOfSeg: either advDoubleTrapezoid or trapezoid
@param iRib: index of Rib in wing_ribs ribDefinition
'''
tanks = []
#===========================================================================
# Tanks
#===========================================================================
if typeOfSeg == 'advDoubletrapezoid':
# Innermost
myUID = parentUID + '_tank_inner'
myName = stringBaseType(valueOf_=myUID)
front = wingFuelTankBorderType(sparUID=stringUIDBaseType(valueOf_=parentUID + '_Spar_FS'))
outer = wingFuelTankBorderType(ribDefinitionUID=stringUIDBaseType(valueOf_='wing_ribs_inner'), ribNumber=integerBaseType(valueOf_=str(4)))
rear = wingFuelTankBorderType(sparUID=stringUIDBaseType(valueOf_=parentUID + '_Spar_RS'))
myGeometry = wingFuelTankGeometryType(border=[front, outer, rear])
tanks.append(wingFuelTankType(uID=myUID, name=myName, geometry=myGeometry))
# root to tw
myUID = parentUID + '_tank_middle'
myName = stringBaseType(valueOf_=myUID)
inner = outer
front = wingFuelTankBorderType(sparUID=stringUIDBaseType(valueOf_=parentUID + '_Spar_FS'))
outer = wingFuelTankBorderType(ribDefinitionUID=stringUIDBaseType(valueOf_='wing_ribs_engine2'), ribNumber=integerBaseType(valueOf_=str(1)))
rear = wingFuelTankBorderType(sparUID=stringUIDBaseType(valueOf_=parentUID + '_Spar_RS'))
myGeometry = wingFuelTankGeometryType(border=[inner, front, outer, rear])
tanks.append(wingFuelTankType(uID=myUID, name=myName, geometry=myGeometry))
# tw to outer
myUID = parentUID + '_tank_outer'
myName = stringBaseType(valueOf_=myUID)
inner = outer
front = wingFuelTankBorderType(sparUID=stringUIDBaseType(valueOf_=parentUID + '_Spar_FS'))
outer = wingFuelTankBorderType(ribDefinitionUID=stringUIDBaseType(valueOf_=parentUID + '_ribs_outer'), ribNumber=integerBaseType(valueOf_=str(nRib)))
rear = wingFuelTankBorderType(sparUID=stringUIDBaseType(valueOf_=parentUID + '_Spar_RS'))
myGeometry = wingFuelTankGeometryType(border=[inner, front, outer, rear])
tanks.append(wingFuelTankType(uID=myUID, name=myName, geometry=myGeometry))
if typeOfSeg == "strutBracedWing":
# Innermost
myUID = parentUID + '_tank_inner'
myName = stringBaseType(valueOf_=myUID)
front = wingFuelTankBorderType(sparUID=stringUIDBaseType(valueOf_=parentUID + '_Spar_FS'))
outer = wingFuelTankBorderType(ribDefinitionUID=stringUIDBaseType(valueOf_='wing_ribs_inner'), ribNumber=integerBaseType(valueOf_=str(4)))
rear = wingFuelTankBorderType(sparUID=stringUIDBaseType(valueOf_=parentUID + '_Spar_RS'))
myGeometry = wingFuelTankGeometryType(border=[front, outer, rear])
tanks.append(wingFuelTankType(uID=myUID, name=myName, geometry=myGeometry))
# root to strut
myUID = parentUID + '_tank_middle'
myName = stringBaseType(valueOf_=myUID)
inner = outer
front = wingFuelTankBorderType(sparUID=stringUIDBaseType(valueOf_=parentUID + '_Spar_FS'))
outer = wingFuelTankBorderType(ribDefinitionUID=stringUIDBaseType(valueOf_='wing_ribs_outer'), ribNumber=integerBaseType(valueOf_=str(1)))
rear = wingFuelTankBorderType(sparUID=stringUIDBaseType(valueOf_=parentUID + '_Spar_RS'))
myGeometry = wingFuelTankGeometryType(border=[inner, front, outer, rear])
tanks.append(wingFuelTankType(uID=myUID, name=myName, geometry=myGeometry))
# strut to outer
myUID = parentUID + '_tank_outer'
myName = stringBaseType(valueOf_=myUID)
inner = outer
front = wingFuelTankBorderType(sparUID=stringUIDBaseType(valueOf_=parentUID + '_Spar_FS'))
outer = wingFuelTankBorderType(ribDefinitionUID=stringUIDBaseType(valueOf_=parentUID + '_ribs_outer'), ribNumber=integerBaseType(valueOf_=str(nRib)))
rear = wingFuelTankBorderType(sparUID=stringUIDBaseType(valueOf_=parentUID + '_Spar_RS'))
myGeometry = wingFuelTankGeometryType(border=[inner, front, outer, rear])
tanks.append(wingFuelTankType(uID=myUID, name=myName, geometry=myGeometry))
myTanks = wingFuelTanksType(wingFuelTank=tanks)
parent.set_wingFuelTanks(myTanks)
def createTanks(parent,
parentUID,
targetUID='tank1',
typeOfSeg='advDoubletrapezoid',
nRib='2'):
'''
Used for generation of a wing tank
@param parent: ComponentSegment object, wing fuel tank will be added here.
@param typeOfSeg: either advDoubleTrapezoid or trapezoid
@param iRib: index of Rib in wing_ribs ribDefinition
'''
tanks = []
#===========================================================================
# Tanks
#===========================================================================
if typeOfSeg == 'advDoubletrapezoid':
# Innermost
myUID = parentUID + '_tank_inner'
myName = stringBaseType(None, None, None, myUID)
front = wingFuelTankBorderType(
None, None, None,
stringUIDBaseType(None, None, 'True', None,
parentUID + '_Spar_FS'))
outer = wingFuelTankBorderType(
ribDefinitionUID=stringUIDBaseType(valueOf_='wing_ribs_inner'),
ribNumber=integerBaseType(valueOf_=str(4)))
rear = wingFuelTankBorderType(
None, None, None,
stringUIDBaseType(None, None, 'True', None,
parentUID + '_Spar_RS'))
myGeometry = wingFuelTankGeometryType(None, None, None,
[front, outer, rear])
tanks.append(
wingFuelTankType(None, None, None, myUID, myName, None, myGeometry,
None))
# root to tw
myUID = parentUID + '_tank_middle'
myName = stringBaseType(None, None, None, myUID)
inner = outer
front = wingFuelTankBorderType(
None, None, None,
stringUIDBaseType(None, None, 'True', None,
parentUID + '_Spar_FS'))
outer = wingFuelTankBorderType(
ribDefinitionUID=stringUIDBaseType(valueOf_='wing_ribs_engine2'),
ribNumber=integerBaseType(valueOf_=str(1)))
rear = wingFuelTankBorderType(
None, None, None,
stringUIDBaseType(None, None, 'True', None,
parentUID + '_Spar_RS'))
myGeometry = wingFuelTankGeometryType(None, None, None,
[inner, front, outer, rear])
tanks.append(
wingFuelTankType(None, None, None, myUID, myName, None, myGeometry,
None))
# tw to outer
myUID = parentUID + '_tank_outer'
myName = stringBaseType(None, None, None, myUID)
inner = outer
front = wingFuelTankBorderType(
None, None, None,
stringUIDBaseType(None, None, 'True', None,
parentUID + '_Spar_FS'))
outer = wingFuelTankBorderType(
ribDefinitionUID=stringUIDBaseType(valueOf_=parentUID +
'_ribs_outer'),
ribNumber=integerBaseType(valueOf_=str(nRib)))
rear = wingFuelTankBorderType(
None, None, None,
stringUIDBaseType(None, None, 'True', None,
parentUID + '_Spar_RS'))
myGeometry = wingFuelTankGeometryType(None, None, None,
[inner, front, outer, rear])
tanks.append(
wingFuelTankType(None, None, None, myUID, myName, None, myGeometry,
None))
if typeOfSeg == "strutBracedWing":
# Innermost
myUID = parentUID + '_tank_inner'
myName = stringBaseType(None, None, None, myUID)
front = wingFuelTankBorderType(
None, None, None,
stringUIDBaseType(None, None, 'True', None,
parentUID + '_Spar_FS'))
outer = wingFuelTankBorderType(
ribDefinitionUID=stringUIDBaseType(valueOf_='wing_ribs_inner'),
ribNumber=integerBaseType(valueOf_=str(4)))
rear = wingFuelTankBorderType(
None, None, None,
stringUIDBaseType(None, None, 'True', None,
parentUID + '_Spar_RS'))
myGeometry = wingFuelTankGeometryType(None, None, None,
[front, outer, rear])
tanks.append(
wingFuelTankType(None, None, None, myUID, myName, None, myGeometry,
None))
# root to strut
myUID = parentUID + '_tank_middle'
myName = stringBaseType(None, None, None, myUID)
inner = outer
front = wingFuelTankBorderType(
None, None, None,
stringUIDBaseType(None, None, 'True', None,
parentUID + '_Spar_FS'))
outer = wingFuelTankBorderType(
ribDefinitionUID=stringUIDBaseType(valueOf_='wing_ribs_outer'),
ribNumber=integerBaseType(valueOf_=str(1)))
rear = wingFuelTankBorderType(
None, None, None,
stringUIDBaseType(None, None, 'True', None,
parentUID + '_Spar_RS'))
myGeometry = wingFuelTankGeometryType(None, None, None,
[inner, front, outer, rear])
tanks.append(
wingFuelTankType(None, None, None, myUID, myName, None, myGeometry,
None))
# strut to outer
myUID = parentUID + '_tank_outer'
myName = stringBaseType(None, None, None, myUID)
inner = outer
front = wingFuelTankBorderType(
None, None, None,
stringUIDBaseType(None, None, 'True', None,
parentUID + '_Spar_FS'))
outer = wingFuelTankBorderType(
ribDefinitionUID=stringUIDBaseType(valueOf_=parentUID +
'_ribs_outer'),
ribNumber=integerBaseType(valueOf_=str(nRib)))
rear = wingFuelTankBorderType(
None, None, None,
stringUIDBaseType(None, None, 'True', None,
parentUID + '_Spar_RS'))
myGeometry = wingFuelTankGeometryType(None, None, None,
[inner, front, outer, rear])
tanks.append(
wingFuelTankType(None, None, None, myUID, myName, None, myGeometry,
None))
myTanks = wingFuelTanksType(None, None, None, tanks)
parent.set_wingFuelTanks(myTanks)
