Sign In to Follow Application
View All Documents & Correspondence

Aircraft Tank Fuel Pick Up Valves In Fuel Transfer Lines

Abstract: This invented valve finds its applicability as fuel pick-ups coming in fuel transfer circuit in the civil aircrafts and military aircrafts which are having non pressurised fuel tanks. A new, economical, reliable and simple "Fuel Pick-up valve" has been invented using simple ball-gravity principle to allow fuel transfer in all aircraft attitudes including inverted flying without any discontinuity. Refueling does not need any electrical energizing of the valve. It performs satisfactorily even with contaminated fuel. Transfer line and refueling line uses common single line when this valve is used; results in less piping and system weight reduction.

Get Free WhatsApp Updates!
Notices, Deadlines & Correspondence

Patent Information

Application #
Filing Date
01 May 2013
Publication Number
32/2015
Publication Type
INA
Invention Field
ELECTRICAL
Status
Email
Parent Application
Patent Number
Legal Status
Grant Date
2024-01-30
Renewal Date

Applicants

HINDUSTAN AERONAUTICS LTD.
AIRCRAFT RESEARCH AND DESIGN CENTRE (ARDC), DESIGN COMPLEX, MARATHALLI POST, BANGALORE - 560 037

Inventors

1. P. RAMESH
POWER PLANT AND FUEL SYSTEM GROUP, HINDUSTAN AERONAUTICS LIMITED, AIRCRAFT RESEARCH AND DESIGN CENTRE (ARDC), DESIGN COMPLEX, MARATHALLI POST, BANGALORE - 560 037
2. N. SELVAKUMAR
POWER PLANT AND FUEL SYSTEM GROUP, HINDUSTAN AERONAUTICS LIMITED, AIRCRAFT RESEARCH AND DESIGN CENTRE (ARDC), DESIGN COMPLEX, MARATHALLI POST, BANGALORE - 560 037
3. AREKH SHARMA
POWER PLANT AND FUEL SYSTEM GROUP, HINDUSTAN AERONAUTICS LIMITED, AIRCRAFT RESEARCH AND DESIGN CENTRE (ARDC), DESIGN COMPLEX, MARATHALLI POST, BANGALORE - 560 037

Specification

1. Title of the invention

Aircraft Tank Fuel Pick-up Valves in Fuel transfer lines

2. Field of invention

It is a mechanical engineering design used for aircraft fuel system.

3. Use of invention

This invented valve finds its applicability in the civil aircrafts and military aircrafts which are having non pressurised fuel tanks.

4. Prior art

Presently in the world, in fuel system of an aircraft "Fuel No Air Valve" or "Refuel - Transfer -Stop Air - Valve" are used to pick up the fuel from the tanks at the transfer line tip which is kept near the bottom of the tank where fuel is expected all the time.

5. Draw backs of prior art

These valves has the limitations / draw backs as mentioned below

1) Complicated in nature and performance is getting affected due to contamination in the used fuel.

2) Number of parts involved is more and costly.

3) During inverted flying does not transfer the fuel and

4) Needs electrical energizing to refuel the tank.

6. Comparison between prior art and present invention

A new, economical, reliable and simple "Fuel Pick-up valve" has been invented using simple ball-gravity principle to allow fuel transfer in all aircraft attitudes including inverted flying without any discontinuity. Refueling does not need any electrical energizing of the valve. It performs satisfactorily even with contaminated fuel. Transfer line and refueling line uses common single line when this valve is used; results in less piping and system weight reduction.

7. Aim of the invention

Aim of the invention is to address the draw backs and limitations in the present valves mentioned prior art using a single simple valve.

8. Summary of the present invention

A new, economical, reliable and simple "Fuel Pick-up valve" has been invented using simple ball-gravity principle to allow fuel transfer in all aircraft attitudes including inverted flying without any discontinuity. Refueling does not need any electrical energizing of the valve. It performs satisfactorily even with contaminated fuel. It addresses the limitations / draw backs faced with present valves like "Fuel No Air Valve" or "Refuel - Transfer - Stop Air - Valve".

9. Brief description of drawings

Fig-l shows the default position of the fuel pick-up valve in which fuel is picked and transferred to the transfer line.

Fig-2 shows the operated position of the fuel pick-up valve in which the ball blocks the transfer as the air is expected to be exposed near the pick-up zone; the blocked passage will not allow fuel as well as air to the transfer line.

10. Statement of invention

A new, economical, reliable and simple "Fuel Pick-up valve" has been invented using simple ball-gravity principle to allow fuel transfer in ail aircraft attitudes including inverted flying without any discontinuity and in addition, during refueling, it does not need any electrical energizing.

11. Detailed description of invention

Refer Fig-l. Fuel pick-up valve is made of a tube (1) with increasing diameter and with eccentric cross section to form ajapered inner surface. Bigger opening works as inlet with screen (3) to filter any foreign body / contamination. Ball (2) is housed inside the tube (1) and which will be at default position as shown in Fig-1 due to gravity and slope of the tube (1). This pick-up valve is positioned on the bottom skin (5) of the tank (which are not air pressurized) so that it could pick-up more fuel from the tank. Installation orientation is to be ensured that a designed inclination (4) is maintained to keep the ball at default position. When the valve is given tilt more than the designed inclination, ball will roll over to throat area of the transfer line (6). It helps the air not to enter into transfer line if pick-up is exposed to air because of fuel movement during maneouver. A tank may be equipped with minimum 3 or many pick-up valves in different zones connected to common transfer line. These Pick-up valves are installed in such a way that each valve will help stopping air entering transfer line due to fuel movement to other sides during maneouver.The same valve pick-up mounted in upside down orientation and in such a way that during normal flying ball is at throat position (passage blocked) and during inverted flying, ball will roll down to default position so that fuel is continuously being picked and available at transfer line.

Claims

1. A new, economical, reliable and simple "Fuel Pick-up valve" has been invented using simple ball-gravity principle to allow fuel transfer in all aircraft attitudes including inverted flying without any discontinuity.

2. Refueling does not need any electrical energizing of the valve.

3. It performs satisfactorily even with contaminated fuel.

4. Transfer line and refueling line uses common single line when this valve is used; results in less piping and system weight reduction.

Documents

Orders

Section Controller Decision Date

Application Documents

# Name Date
1 1955-CHE-2013 FORM-5 01-05-2013.pdf 2013-05-01
1 1955-CHE-2013-IntimationOfGrant30-01-2024.pdf 2024-01-30
2 1955-CHE-2013 FORM-3 01-05-2013.pdf 2013-05-01
2 1955-CHE-2013-PatentCertificate30-01-2024.pdf 2024-01-30
3 1955-CHE-2013-Amended Pages Of Specification-270123.pdf 2023-02-10
3 1955-CHE-2013 FORM-2 01-05-2013.pdf 2013-05-01
4 1955-CHE-2013-Abstract_Hearing Reply_27-01-2023.pdf 2023-01-27
4 1955-CHE-2013 FORM-1 01-05-2013.pdf 2013-05-01
5 1955-CHE-2013-Claims_Hearing Reply_27-01-2023.pdf 2023-01-27
5 1955-CHE-2013 DRAWINGS 01-05-2013.pdf 2013-05-01
6 1955-CHE-2013-Correspondence_Amended Pages Of Specification And Hearing Reply_27-01-2023.pdf 2023-01-27
6 1955-CHE-2013 DESCRIPTION (COMPLETE) 01-05-2013.pdf 2013-05-01
7 1955-CHE-2013-Drawing_Hearing Reply_27-01-2023.pdf 2023-01-27
7 1955-CHE-2013 CLAIMS 01-05-2013.pdf 2013-05-01
8 1955-CHE-2013-Marked Up Copy_Authorization Certificate And Hearing Reply_27-01-2023.pdf 2023-01-27
8 1955-CHE-2013 ABSTRACT 01-05-2013.pdf 2013-05-01
9 1955-CHE-2013-US(14)-HearingNotice-(HearingDate-20-01-2023).pdf 2022-12-18
9 1955CHE2013 FORM-18 28-03-2014.pdf 2014-03-28
10 1955-CHE-2013-FER.pdf 2019-02-12
10 Abstract_FER Reply_09-08-2019.pdf 2019-08-09
11 Amended Pages Of Specification_FER Reply_09-08-2019.pdf 2019-08-09
11 Marked up Copy of Specification_FER Reply_09-08-2019.pdf 2019-08-09
12 Claims_FER Reply_09-08-2019.pdf 2019-08-09
12 Form2 Title Page_FER Reply_09-08-2019.pdf 2019-08-09
13 Correspondence by Applicant_FER Reply_09-08-2019.pdf 2019-08-09
13 Drawing_FER Reply_09-08-2019.pdf 2019-08-09
14 Correspondence by Applicant_FER Reply_09-08-2019.pdf 2019-08-09
14 Drawing_FER Reply_09-08-2019.pdf 2019-08-09
15 Claims_FER Reply_09-08-2019.pdf 2019-08-09
15 Form2 Title Page_FER Reply_09-08-2019.pdf 2019-08-09
16 Amended Pages Of Specification_FER Reply_09-08-2019.pdf 2019-08-09
16 Marked up Copy of Specification_FER Reply_09-08-2019.pdf 2019-08-09
17 Abstract_FER Reply_09-08-2019.pdf 2019-08-09
17 1955-CHE-2013-FER.pdf 2019-02-12
18 1955-CHE-2013-US(14)-HearingNotice-(HearingDate-20-01-2023).pdf 2022-12-18
18 1955CHE2013 FORM-18 28-03-2014.pdf 2014-03-28
19 1955-CHE-2013 ABSTRACT 01-05-2013.pdf 2013-05-01
19 1955-CHE-2013-Marked Up Copy_Authorization Certificate And Hearing Reply_27-01-2023.pdf 2023-01-27
20 1955-CHE-2013 CLAIMS 01-05-2013.pdf 2013-05-01
20 1955-CHE-2013-Drawing_Hearing Reply_27-01-2023.pdf 2023-01-27
21 1955-CHE-2013 DESCRIPTION (COMPLETE) 01-05-2013.pdf 2013-05-01
21 1955-CHE-2013-Correspondence_Amended Pages Of Specification And Hearing Reply_27-01-2023.pdf 2023-01-27
22 1955-CHE-2013 DRAWINGS 01-05-2013.pdf 2013-05-01
22 1955-CHE-2013-Claims_Hearing Reply_27-01-2023.pdf 2023-01-27
23 1955-CHE-2013 FORM-1 01-05-2013.pdf 2013-05-01
23 1955-CHE-2013-Abstract_Hearing Reply_27-01-2023.pdf 2023-01-27
24 1955-CHE-2013 FORM-2 01-05-2013.pdf 2013-05-01
24 1955-CHE-2013-Amended Pages Of Specification-270123.pdf 2023-02-10
25 1955-CHE-2013-PatentCertificate30-01-2024.pdf 2024-01-30
25 1955-CHE-2013 FORM-3 01-05-2013.pdf 2013-05-01
26 1955-CHE-2013-IntimationOfGrant30-01-2024.pdf 2024-01-30
26 1955-CHE-2013 FORM-5 01-05-2013.pdf 2013-05-01

Search Strategy

1 searchstrategy1955CHE2013_05-02-2019.pdf

ERegister / Renewals