GB859057A - Improvements relating to the insulation and ventilation of aircraft - Google Patents

Improvements relating to the insulation and ventilation of aircraft

Info

Publication number
GB859057A
GB859057A GB38944/57A GB3894457A GB859057A GB 859057 A GB859057 A GB 859057A GB 38944/57 A GB38944/57 A GB 38944/57A GB 3894457 A GB3894457 A GB 3894457A GB 859057 A GB859057 A GB 859057A
Authority
GB
United Kingdom
Prior art keywords
ducts
duct
units
fuselage
panel
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.)
Expired
Application number
GB38944/57A
Inventor
William Fothergill Taylor
Arthur Dudley
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.)
Baxter Woodhouse and Taylor Ltd
Original Assignee
Baxter Woodhouse and Taylor 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.)
Filing date
Publication date
Application filed by Baxter Woodhouse and Taylor Ltd filed Critical Baxter Woodhouse and Taylor Ltd
Priority to GB38944/57A priority Critical patent/GB859057A/en
Publication of GB859057A publication Critical patent/GB859057A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • 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

Landscapes

  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Duct Arrangements (AREA)

Abstract

859,057. Insulating aircraft. BAXTER, WOODHOUSE & TAYLOR Ltd. Dec. 15, 1958 [Dec. 14, 1957], No. 38944/57. Class 4. An aircraft fuselage comprising frames 1 and stringers 2 is provided with composite insulating and ventilating units constructed individually and arranged; in vertically adjoining relationship against the structure to which they are secured by cords 19. The units are arranged in vertically adjoining pairs arranged side-by-side along the length of the fuselage and the upper unit of each pair, as shown in section in Fig. 3, comprises an outer layer of glass fibre 7 encased in a P.V.C. coated fabric skin 8 which is attached to a panel 10 of similar coated fabric which, with pillars 11 of encased foamed plastic and a panel 12 secured to panel 10 by fabric strips 6, form a duct 5 which connects at its upper end with a longitudinal air trunk (not shown). The lower unit of each pair, Fig. 6, comprises a part 21 of sound insulating material, e.g. glass fibre, and three laterally spaced ducts 23, 24 formed by pillars 27 of encased foamed plastic and a closing panel 28, the central pillars 27 stopping short of the base of the unit so that the three ducts are in communication. The upper end of the central duct 23 telescopes on to or into the duct 5 of the upper unit and at its lower end it has a tubular extension to an under-floor compartment of the fueslage. The lateral extremities of the upper and lower units are provided respectively with lacing eyelets 17 and 29 by means of which the units are secured by the cords 19 to strips 18 attached to frames 1. Air from the longitudinal air trunk is fed to each duct 5 and thence down through duct 23 and up through ducts 24 to emerge into the fuselage through outlet nozzles 25. It is stated that the ducts may be adjacent the fuselage wall with the sound insulating panels forming the interior faces of the units or the ducts may be formed integrally within the insulating panels. The sound insulating panels 7 and 21 may be formed with shaped recesses to accommodate structural members 1 and 2.
GB38944/57A 1957-12-14 1957-12-14 Improvements relating to the insulation and ventilation of aircraft Expired GB859057A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB38944/57A GB859057A (en) 1957-12-14 1957-12-14 Improvements relating to the insulation and ventilation of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB38944/57A GB859057A (en) 1957-12-14 1957-12-14 Improvements relating to the insulation and ventilation of aircraft

Publications (1)

Publication Number Publication Date
GB859057A true GB859057A (en) 1961-01-18

Family

ID=10406651

Family Applications (1)

Application Number Title Priority Date Filing Date
GB38944/57A Expired GB859057A (en) 1957-12-14 1957-12-14 Improvements relating to the insulation and ventilation of aircraft

Country Status (1)

Country Link
GB (1) GB859057A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3116613A (en) * 1961-05-31 1964-01-07 Boeing Co Air conditioning and heat intercept system for high speed vehicles
US4739823A (en) * 1984-11-09 1988-04-26 Mcdonnell Douglas Heat exchanger structure
US4819720A (en) * 1984-11-09 1989-04-11 Mcdonnell Douglas Corporation Skin heat exchanger
JP2010501390A (en) * 2006-08-22 2010-01-21 エアバス ドイチェランド ゲゼルシャフト ミット ベシュレンクテル ハフツング Frame element, aircraft air conditioning system, and method of attaching frame element to aircraft
EP2407379A1 (en) * 2010-07-13 2012-01-18 Airbus Operations Ventilation system for an aircraft
CN107021203A (en) * 2015-11-30 2017-08-08 波音公司 Using stack Carbon Fiber Reinforced Plastics fill out part the plastic stringers terminal softening

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3116613A (en) * 1961-05-31 1964-01-07 Boeing Co Air conditioning and heat intercept system for high speed vehicles
US4739823A (en) * 1984-11-09 1988-04-26 Mcdonnell Douglas Heat exchanger structure
US4819720A (en) * 1984-11-09 1989-04-11 Mcdonnell Douglas Corporation Skin heat exchanger
JP2010501390A (en) * 2006-08-22 2010-01-21 エアバス ドイチェランド ゲゼルシャフト ミット ベシュレンクテル ハフツング Frame element, aircraft air conditioning system, and method of attaching frame element to aircraft
EP2407379A1 (en) * 2010-07-13 2012-01-18 Airbus Operations Ventilation system for an aircraft
US20120015595A1 (en) * 2010-07-13 2012-01-19 Airbus Operations (S.A.S.) Aircraft ventilation system
FR2962715A1 (en) * 2010-07-13 2012-01-20 Airbus Operations Sas AERATION SYSTEM FOR AIRCRAFT.
US9494266B2 (en) 2010-07-13 2016-11-15 Airbus Operations S.A.S. Aircraft ventilation system
CN107021203A (en) * 2015-11-30 2017-08-08 波音公司 Using stack Carbon Fiber Reinforced Plastics fill out part the plastic stringers terminal softening
CN107021203B (en) * 2015-11-30 2021-10-29 波音公司 Stringer and method of controlling delamination and separation between composite stringer and composite structure

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