GB120701A – Improvements in Structural Elements and Parts for Aeroplanes.
– Google Patents
GB120701A – Improvements in Structural Elements and Parts for Aeroplanes.
– Google Patents
Improvements in Structural Elements and Parts for Aeroplanes.
Info
Publication number
GB120701A
GB120701A
GB8587/18A
GB858718A
GB120701A
GB 120701 A
GB120701 A
GB 120701A
GB 8587/18 A
GB8587/18 A
GB 8587/18A
GB 858718 A
GB858718 A
GB 858718A
GB 120701 A
GB120701 A
GB 120701A
Authority
GB
United Kingdom
Prior art keywords
rudder
elevators
planes
skids
braces
Prior art date
1918-05-23
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.)
Expired
Application number
GB8587/18A
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.)
Metropolitan Vickers Electrical Co Ltd
Original Assignee
British Westinghouse Electric and Manufacturing Co Ltd
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.)
1918-05-23
Filing date
1918-05-23
Publication date
1918-11-21
1918-05-23
Application filed by British Westinghouse Electric and Manufacturing Co Ltd
filed
Critical
British Westinghouse Electric and Manufacturing Co Ltd
1918-05-23
Priority to GB8587/18A
priority
Critical
patent/GB120701A/en
1918-11-21
Publication of GB120701A
publication
Critical
patent/GB120701A/en
Status
Expired
legal-status
Critical
Current
Links
Espacenet
Global Dossier
Discuss
239000000463
material
Substances
0.000
abstract
3
239000007859
condensation product
Substances
0.000
abstract
2
239000004744
fabric
Substances
0.000
abstract
2
239000006096
absorbing agent
Substances
0.000
abstract
1
239000010425
asbestos
Substances
0.000
abstract
1
239000011111
cardboard
Substances
0.000
abstract
1
238000010276
construction
Methods
0.000
abstract
1
239000002657
fibrous material
Substances
0.000
abstract
1
238000010438
heat treatment
Methods
0.000
abstract
1
239000002184
metal
Substances
0.000
abstract
1
239000003973
paint
Substances
0.000
abstract
1
239000000123
paper
Substances
0.000
abstract
1
150000002989
phenols
Chemical class
0.000
abstract
1
229910052895
riebeckite
Inorganic materials
0.000
abstract
1
125000006850
spacer group
Chemical group
0.000
abstract
1
238000004804
winding
Methods
0.000
abstract
1
239000002023
wood
Substances
0.000
abstract
1
Classifications
B—PERFORMING OPERATIONS; TRANSPORTING
B64—AIRCRAFT; AVIATION; COSMONAUTICS
B64C—AEROPLANES; HELICOPTERS
B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
B—PERFORMING OPERATIONS; TRANSPORTING
B64—AIRCRAFT; AVIATION; COSMONAUTICS
B64C—AEROPLANES; HELICOPTERS
B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
B64C2001/0054—Fuselage structures substantially made from particular materials
B64C2001/0063—Fuselage structures substantially made from particular materials from wood
B—PERFORMING OPERATIONS; TRANSPORTING
B64—AIRCRAFT; AVIATION; COSMONAUTICS
B64C—AEROPLANES; HELICOPTERS
B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
B64C2001/0054—Fuselage structures substantially made from particular materials
B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
B—PERFORMING OPERATIONS; TRANSPORTING
B64—AIRCRAFT; AVIATION; COSMONAUTICS
B64C—AEROPLANES; HELICOPTERS
B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
B64C2001/0054—Fuselage structures substantially made from particular materials
B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
Y02T50/00—Aeronautics or air transport
Y02T50/40—Weight reduction
Abstract
120,701. British Westinghouse Electric & Manufacturing Co., (Westing- house Electric & Manufacturing Co.). May 23, 1918. Cars; framework; planes, construction and arrangement of.-The various parts of aeroplanes are made of fibrous material, such as wood, asbestos, paper, cardboard, or cloth, impregnated with condensation products of phenols and formaldebydes as described in Specifications 1921/08 and 21566/08, [both in Class 95. Paints, &c.], or other similar condensation products, wrapped, pressed, or moulded into the required shape, and hardened by heat-treatment. Fig. 1 shows an aeroplane having the body 1 formed in one piece in the manner described above, the rear end being strengthened by crossbracing 12, Fig. 7, and having fins 15, 16 formed integrally therewith. The fins are provided with braces 25, Fig. 8, and are covered at the rear ends by a cruciform cap 19 to which the rudder 14 and elevators 17 are hinged. The rudder and elevators are composed of a front support 27, Figs. 9 and 10, of suitable material, to which and to a trailing edge 29 are secured the surfaces 28 formed of the above-mentioned materials and with inwardly projecting ribs 30, Figs. 9 and 12. The main planes are formed as described above of tubular or :-section spars 76, 77, Fig. 13, threaded through ribs 67 separated by tubular spacers 90, 91, Fig. 17, and connected to a leading edge 68 and trailing edge 70. The whole is covered with fabric 103. The interplane struts 96, Figs. 17, 19, and 21, are formed by winding layers upon a mandrel and are connected to the planes by screwing on to members 95 attached to metal brackets 93, Fig. 17, seated on the spars. The cables may be enclosed in streamline casings of similar form. Land wheels and skids.-Wheels 7 carried by braces 9, and a skid 22 are formed of the abovementioned materials. The skids are fitted with shock-absorbers 23, Fig. 7. Steering.-The operating-arms of the rudder and elevators are formed of hollow sections 31, Fig. 10, attached by bolts 33.
GB8587/18A
1918-05-23
1918-05-23
Improvements in Structural Elements and Parts for Aeroplanes.
Expired
GB120701A
(en)
Priority Applications (1)
Application Number
Priority Date
Filing Date
Title
GB8587/18A
GB120701A
(en)
1918-05-23
1918-05-23
Improvements in Structural Elements and Parts for Aeroplanes.
Applications Claiming Priority (1)
Application Number
Priority Date
Filing Date
Title
GB8587/18A
GB120701A
(en)
1918-05-23
1918-05-23
Improvements in Structural Elements and Parts for Aeroplanes.
Publications (1)
Publication Number
Publication Date
GB120701A
true
GB120701A
(en)
1918-11-21
Family
ID=32343387
Family Applications (1)
Application Number
Title
Priority Date
Filing Date
GB8587/18A
Expired
GB120701A
(en)
1918-05-23
1918-05-23
Improvements in Structural Elements and Parts for Aeroplanes.
Country Status (1)
Country
Link
GB
(1)
GB120701A
(en)
1918
1918-05-23
GB
GB8587/18A
patent/GB120701A/en
not_active
Expired
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